Enclosure 2 - Description of GFE Aircrafts

Unclassified Enclosure 2 – GFE Aircrafts Date FMV Document ID Subject type

2012-12-06

Document number Page

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Enclosure 2 – Description of GFE Aircrafts

1 GFE Aircraft Learjet LR35A ..........................................................................................4

1.1 Learjet LR35A Aircraft Maintenance Program ........................................................4

1.1.1 Comprehensive description of Learjet Maintenance Program (MM-99) ...............4

1.1.2 Modifications that affects the maintenance program ............................................5

1.1.3 Airframe Maintenance Documentation ................................................................5

1.1.4 Engine Maintenance Documentation ...................................................................5

1.1.5 Maintenance Tasks related to changes .................................................................6

1.1.6 Guiding documents issued by the Agency and Aviation Authority for both

Airframe and Engines: ....................................................................................................6

1.2 GFE Aircraft Learjet 35A SE-DHO.........................................................................7

1.2.1 Aircraft Specification ..........................................................................................7

1.2.2 Engines ...............................................................................................................7

1.2.3 Avionics ..............................................................................................................7

1.2.4 Mission System ...................................................................................................8

1.2.5 Mission Cable Harness to Hard Points .................................................................9

1.2.6 Antenna layout .................................................................................................. 10

1.2.7 Inspection due times and dates .......................................................................... 11

1.2.8 Implemented Changes ....................................................................................... 12

1.3 GFE Aircraft Learjet 35A SE-DHP ....................................................................... 28

1.3.1 Aircraft Specification ........................................................................................ 28

1.3.2 Engines ............................................................................................................. 28

1.3.3 Avionics ............................................................................................................ 28

1.3.4 Mission System ................................................................................................. 29

1.3.5 Mission Cable Harness to Hard Points ............................................................... 30

1.3.6 Antenna layout .................................................................................................. 30

1.3.7 Inspektion due times and dates .......................................................................... 31


2 GFE Aircraft Mitsubishi MU-2 ..................................................................................... 47

2.1 Mitsubishi MU-2 Aircraft Maintenance Program .................................................. 47

2.1.1 Comprehensive description of Mitsubishi Maintenance Requirements Manual

(MR-0178-2): ............................................................................................................... 47

2.1.2 Modifications that affects the maintenance program .......................................... 47

2.1.3 Maintenance Documentation ............................................................................. 48

2.1.4 Guiding documents to be used during maintenance: .......................................... 48

2.1.5 Maintenance Tasks related to changes ............................................................... 48

2.1.6 Guiding documents issued by the Agency and Aviation Authority for both

Airframe and Engines: .................................................................................................. 49

2.2 GFE Aircraft Mitsubishi MU-2 SE-GHA .............................................................. 50


2.2.2 Engines ............................................................................................................. 50

2.2.3 Propeller ........................................................................................................... 50

2.2.4 Avionics ............................................................................................................ 50


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2.2.5 Mission System ................................................................................................. 51


2.2.7 Antenna Layout ................................................................................................. 52



2.3 GFE Aircraft Mitsubishi MU-2 SE-GHB .............................................................. 75


2.3.2 Engines ............................................................................................................. 75

2.3.3 Propeller ........................................................................................................... 75

2.3.4 Avionics ............................................................................................................ 75

2.3.5 Mission System ................................................................................................. 76


2.3.7 Antenna Layout ................................................................................................. 77



2.4 GFE Aircraft Mitsubishi MU-2 SE-GHD .............................................................. 99


2.4.2 Engines ............................................................................................................. 99

2.4.3 Propeller ........................................................................................................... 99

2.4.4 Avionics ............................................................................................................ 99

2.4.5 Mission System ............................................................................................... 100

2.4.6 Mission Cable Harness to Hard Points ............................................................. 100

2.4.7 Antenna Layout ............................................................................................... 101

2.4.8 Inspection due times and dates ........................................................................ 102

2.4.9 Implemented Changes ..................................................................................... 103

2.5 GFE Aircraft Mitsubishi MU-2 SE-GHF ............................................................. 123

2.5.1 Aircraft Specification ...................................................................................... 123

2.5.2 Engines ........................................................................................................... 123

2.5.3 Propeller ......................................................................................................... 123

2.5.4 Avionics .......................................................................................................... 123

2.5.5 Mission System ............................................................................................... 124


2.5.7 Antenna Layout ............................................................................................... 125



2.6 GFE Aircraft Mitsubishi MU-2 SE-IOV .............................................................. 147


2.6.2 Engines ........................................................................................................... 147

2.6.3 Propeller ......................................................................................................... 147

2.6.4 Avionics .......................................................................................................... 147

2.6.5 Mission System ............................................................................................... 148


2.6.7 Antenna Layout ............................................................................................... 149



2.7 GFE Aircraft Mitsubishi MU-2 SE-IUA .............................................................. 171


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2.7.2 Engines ........................................................................................................... 171

2.7.3 Propeller ......................................................................................................... 171

2.7.4 Avionics .......................................................................................................... 171

2.7.5 Mission System ............................................................................................... 172


2.7.7 Antenna Layout ............................................................................................... 173




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1 GFE Aircraft Learjet LR35A

1.1 Learjet LR35A Aircraft Maintenance Program

1.1.1 Comprehensive description of Learjet Maintenance Program (MM-99) The maintenance is (according to Learjet Maintenance Manual MM-99) based on 24 Phase

Inspections, accomplished one at a time, in groups or collectively, as scheduled by the aircraft

operator and in accordance with allowable inspection tolerances.

Estimated utilization is 500 Hrs per A/C and year.

Each Phase Inspection is contained within one of four (1 of 4) hourly or calendar driven

inspection intervals, the 300 hour or 12 month A-Phases, 600 hour or 24 month B-Phases,

1200 hour or 48 month C-Phases and 2400 hour or 96 month D-Phases.

Each of the primary inspection intervals (A, B, C, and D) contains six (6) stand-alone Phase

Inspections.

Inspection list according to Learjet maintenance Manual MM-99:

• Phase A2 300 hrs Inspection / Checks.




• Phase A6 300 hrs Inspection / Checks

• Phase B1 600 hrs Inspection / Checks

• Phase B2 600 hrs Inspection / Checks.

• Phase B3 600 hrs Inspection / Checks




• Phase C1 1200 hrs Inspection / Checks.

• Phase C2 1200 hrs Inspection / Checks





• Phase D1 2400 hrs Inspection / Checks.

• Phase D2 2400 hrs Inspection / Checks





• 3000 Landings Inspections.

• Major Landing Inspections.

• 12 Year Airframe Inspections


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• 12000 Hours Airframe Inspections.

• Other Interval Inspections.

• Unscheduled Maintenance Checks.

• MPI Engine Zone Inspection.

• Engine Light Maintenance TFE731-2.

1.1.2 Modifications that affects the maintenance program

• The wings have been modified with hard points to carry ECM pods and outboard

winches.

• The R/H wing tip tank has been modified with tip radome covering antennas for an

inboard ECM system ASTOR.

• To supply the ECM equipment with 3-phase AC, one 3kVA inverter system has been

installed in the inboard aft baggage area. (FAA STC SA125NE).

• Operator Stand is installed in the cabin with equipment to control winches and ECM

units. Set of monitoring equipment as TV-camera, mirrors etc.

• Aft Body Strakes in accordance with AVCON STC ST00432WI (EASA/LBA

TA0112) have been installed.

• Alteration between Dual / Single Mid Fuselage Camera Pods and Structural Plugs in

accordance with AVCON STC SA2479CE (EASA.IM.A.S.01449).

1.1.3 Airframe Maintenance Documentation Maintenance of the airframe is conducted according to the following documentation:

• Learjet Maintenance Manual. MM-99

• Learjet Wiring Manual. WM-99

• Learjet Illustrated Parts Catalogue.

• Learjet Service Bulletins.

• Learjet Airplane Accessory Kit.

• Learjet Airplane Modification Kit.

• Learjet Structural Repair Manual.

• Learjet Non-Destructive Inspection Manual.

• Keith TR-134 System Service Manual. TR-134.

• Saab AB, Technical Directives-Modification, issued by DOA EASA 21J.108.

Continued Airworthiness.

1.1.4 Engine Maintenance Documentation Maintenance of the engines is conducted according to the following documentation:

• Honeywell TFE731 Light Maintenance Manual. 72-02-01

• Honeywell TFE731 Illustrated Pars Catalogue. 72-00-71.

• Honeywell TFE731 Service Bulletin for Service Life Limits of Critical Life Limited

Components. SB TFE731-72-3001.

• Honeywell TFE731 Service Bulletins.

• Honeywell TFE731 Service Information Letters.


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1.1.5 Maintenance Tasks related to changes The following maintenance tasks are not included in the aircraft manufactures’ maintenance

manual. The tasks are included in the operators AMP:

• Structural Plugs in Cabin Annual/300 hrs Inspection/Checks

• Operator’s Consol. Annual/300 hrs Inspection/Checks

• Mission Power Annual/300 hrs Inspection/Checks

• Mission Power 600 hrs Inspection/Checks

• Mission Power 1200 hrs Inspection/Checks

• ACAS II. 24 Months Inspection/Checks

• Special Operational Fatigue Inspection 1200 hrs Inspection/Checks

• Hard Points and ejection unit 300 Hrs Inspection

1.1.6 Guiding documents issued by the Agency and Aviation Authority for both Airframe and Engines:

• FAA Airworthiness Directives.

• Swedish NAA LVD.

• EASA AD.

• EC 2042/2003 Annex II Part-145- AMC. & Guidance Material.

• BCL - C, -D, -M if operating under Swedish regulations

• EASA Series-OPS


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1.2 GFE Aircraft Learjet 35A SE-DHO

1.2.1 Aircraft Specification Type: Serial

Number:

Registration: Airframe

total Hours:

Total

Landing

Cycles:

Date

Reference:

Learjet

35A

195 SE-DHO 13320 8780 2012-11-23

1.2.2 Engines Type: TFE731-2-2B

Serial

Number:

Total Hours

Since New:

Total

Cycles

Since New:

Hours

remaining to

MPI:

Hours

remaining to

CZI:

Left Engine P-74278 11122 7392 928 922

Right Engine P-74583 10648 7406 179 170

1.2.3 Avionics System: Type / Part Number: Note:

Autopilot JET FC 200

Dual VHF-COM Collins VHF-22C

HF-COM Collins 718U-5

ICS & Audio System DB System

Dual VHF-NAV Collins VIR-30A

GPS Garmin GPS 165 TSO

Dual DME Collins DME40

ADF 1 Bendix/King KDF-805

XPDR 1 & 2 Collins TDR94D Mode S

EHS

TCAS II Collins TCAS-4000

Dual TCAS II VSI/RA/TA Indicator Collins TVI-920

TAWS / EGPWS Honeywell MK VIII

RDR ALT Collins ALT-55B

Weather Radar Honeywell Primus 400

MFD Display Honeywell MFRD

ELT Kanad ELT 406-AF-H

Dual Mach Airspeed indicator IDC 2680003-2

Altimeter incl. encoder LH IDC 518-16007-187

Altimeter RH IDC 23932-053

Altitude Report & Alerting System IDC 23989-011

Air Data Display Unit 9D-80130-32

Dual Flight Director Indicator Collins 329B-7R-2


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Dual VG-Gyro JET VG-206(XX)

Standby Altitude Gyro JET AI 804

Dual Horizontal Situation Indicator Collins 331A-6R

Dual RMI Collins 332C-10

Dual DG-Gyro JET DN-101D

RVSM

FDR Sundstrand 980-4100-FWUS

CVR Fairchild 93-A100-83

1.2.4 Mission System System: Description:

Fixed general installations

FR31 VHF/UHF COM Radio

AN/ARC 182 VHF/UHF COM Radio

GPS MAP System

JET SI-3003B Inverter 115/200VAC 400Hz 3 phase

KGS SPS-3052B Inverter 230VAC 50Hz

Laser Prism

Wing Pylon

NATO 14” Alcon Ejector Unit LH and RH Wing Pylon

EW system

ASTOR Fixed installed system

ADRIAN C & S Pod mounted system

U95-N Pod mounted system

U95-D2 Pod mounted system

U95 Sorc Pod mounted system

A100 Pod mounted system

Missile Threat Simulator

DARTS Pod mounted system

GMS Pod mounted system

Chaff Dispenser

BOX 3 Pod mounted system

Target Towing

MTR 101 Outboard pod mounted winch

AS200 MDI (Miss Distance Indicator)

TLX Height keeping target

Precisions GPS Pos System

TAPS


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1.2.5 Mission Cable Harness to Hard Points Used for Mission

System:

LH NATO Hard point: RH NATO Hard point: Note:

Adrian C & S, U95-N,

U95-D2, U95 Sorc,

A100, DARTS, GMS,

BOX 3 and MTR 101

General Signal Harness General Signal Harness Two pair shielded

AWG 20 x 25

MTR 101 MTR 101 Harness MTR 101 Harness Two pair shielded

AWG 20 x 3

AWG 16 x 4 +

shield

U95-N, U95-D2, U95

Sorc, A100 and GMS

MIL-STD-1553B Data

Bus

MIL-STD-1553B Data

Bus

Twinax x 8

U95-N, U95-D2, U95

Sorc, A100, DARTS,

GMS and BOX 3

AC Power

115/200VAC 400 Hz 3-

Phase 3 x 10 A

AC Power 115/200VAC

400 Hz 3-Phase 3 x 10 A

AWG 12 x 10 +

shield

Adrian C & S, GMS

and BOX 3

DC Power 28 VDC 150

A

DC Power 28 VDC 150

A

AWG 4 x 4

MTR 101 Coaxial 2 x 75 Ω Coaxial 2 x 75 Ω

Adrian C & S Coaxial 3 x 50 Ω Coaxial 3 x 50 Ω

Recognition Light Recognition Light

Cable

Recognition Light Cable AWG 16 x 4 +

shield


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1.2.6 Antenna layout


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1.2.7 Inspection due times and dates Status date November 23

rd 2012.

Description Maint. Ref C/Out date C/Out Hrs Due Hrs Due date Due Landings

Aircraft SE-DHO

Phase A 300 hour insp. AMP 2012-07-16 13290 13590,3 2013-09-10

Phase B 600 hour insp. AMP 2011-03-05 13043 13643,3 2013-04-05

Phase C 1200 hour insp. AMP 2009-11-01 12849 14049,1 2013-10-31

Phase D 2400 hour insp. AMP 2009-08-18 12789 15189,6 2017-08-16

Special operational fatigue inspect AMP 2009-01-23 12620 13820,8

12000 Hrs Inspection AMP 2001-08-29 11269 17269,1

45 days insp. AMP 2012-10-19 13303 2012-12-03

6 Month Inspection AMP 2012-07-17 13290 2013-03-11

2 Year Inspection AMP 2011-06-17 13129 2013-07-20

12 Year Airframe inspection AMP 2001-08-28 2013-08-25 13503

MPI engine zone inspecition LH AMP 2009-10-22 12849 14249,1

MPI engine zone inspecition RH AMP 2005-04-12 12053 13453,6

300 Hrs Inspection AMP 2011-10-11 13182 13500

1200 Hrs Inspection AMP 2007-05-15 12440 13640

3000 Landing Inspection AMP 1996-01-24 9000

6000 Major Landing Gear Inspection AMP 1988-10-11 10745

Operator's Console 300h/1y insp. AMP 2012-04-23 13248 13548,8 2013-04-23

ACAS 2 (TCAS) 24month insp. AMP 2011-06-29 13129 2013-07-13

Mission equipment 300 hour insp. AMP 2012-07-19 13290 13590,3

Engine S/N P-74278 Remaining

Engine 150 hrs insp. AMP 13431,82 111,34



Engine Compressor Zone Insp. AMP 14243,3 922,82

Engine Major Periodic Inspection AMP 14249,1 928,62




Engine 800 hrs insp. AMP 13696 375,52




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1.2.8 Implemented Changes

Abbreviations:

Abbr. Issued by Explanation

AAK Learjet Aircraft Accessory Kit

AD EASA, FAA Airwortness Directive

AMK Learjet Aircraft Mod Kit

AW Learjet Accessory Wire

LVA LFV Luftvärdighetsanvisning

LVD LFV Luftvärdighetsdirektiv

SB Keith, Learjet, Nyge Service Bullentin

SIL Rockwell Service information letter

SSB Nyge and Garmin Sofware SB

SSK Learjet Special Spares Kit

STC Avcon, Flight Int., Keith,

EASA

Supplement Type Certificate

TDM Nyge Tekniskt Direktiv Materiel


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Status date November 23rd

2012.

SB/AD etc Reference

Rev Subject Document reference Eff. date Rev Compliance Status Remarks

AVCON, Avcon Industries, Inc.

AVCON STC SA00432WI

R Install. Avcon Fins 31-Mar-2005 R 01-Jul-2005

AVCON STC SA2479CE

A Install. Plug of Dual Hatches 30-Jun-2005 A 01-Jul-2005

AVCON STC ST00564WI

AFM suppl. increase T/O weight........ 25-Aug-1997 29-Jun-2005

AVCON STC ST00611WI

C Increase Takeoff Weight to 19600 pounds

11-Mar-2005 C 01-Jul-2005

AVCON STC ST00612WI

B Increase Wing/Tip Zero Fuel Weight 28-Nov-1997 B 01-Jul-2005

AVCON STC ST00613WI

C Increase Landing Weight to 16000 pounds

11-Mar-2005 C 01-Jul-2005

EASA, European Aviation Safety Agency

EASA AD 2006-0265

Incorrect transponder altitude 30-Aug-2006 18-Aug-2009

EASA AD 2008-0159

Improve EHS Operation HONEYWELL SB MST 67A-34-56 HONEYWELL SSBMST 67A-SW5 Rev 1

25-Aug-2008 01-Dec-2010 N/A N/A by transponder P/N installed

EASA AD 2009-0097

IR Mode S Transponder -Check/Modification

DHC SB 8-34-243 Rev A EASA AD 2010-0067 ROCKWELL SIL07-1

29-Apr-2009 IR 18-Aug-2009 PCW Are in compliance with EASA AD2009-0097 Ref TDM03-17 DWG MF1030064-1 Rev.C

EASA AD 2009-0173

1 Mode S Transponder Mod/Repl 30-Sep-2010 1 08-Dec-2010 N/A due to ADC p/n

EASA AD 2009-0251-E

Portable Fire Extinguishers-Ident/Repl

25-Nov-2009 07-May-2010 N/A N/A by current P/N installed

EASA AD 2009-0262

Halon 1211 Fire Extinguishers Id/Repl

EASA AD 2009-0278 FFE ASB26-115 Rev C

15-Dec-2009 07-May-2010 N/A N/A by current P/N installed

EASA AD 2009-0278


EASA AD 2009-0262 22-Dec-2009 07-May-2010 N/A N/A by current P/N installed


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EASA AD 2010-0003

R1 Mode S Transponder -Check/Modification

11-Jan-2010 R1 10-Mar-2010 N/A due to p/n

EASA AD 2010-0204

IR Mode S Transponder -Mod/Repl 06-Oct-2010 IR 08-Dec-2010 N/A by ADC p/n installed

EASA AD 2012-0037

KIDDE GRAVINER HAND OPERATTED FIRE EXTINGUISHER

10-Sep-2012

FAA, U.S, Federal Aviation Administration

FAA, U.S AD 2000-24-19

Donning oxygen masks 22-Nov-2000 20-Feb-2003 Complied with by insert of AFM Change 12

FAA, U.S AD 2001-07-11

Goodyear Flight Eagle Tire Tread Separat

LEARJET AW 32-021 01-May-2001 17-May-2001 N/A by s/n on tire

FAA, U.S AD 2001-15-17

Prevent erroneous altitude interpretatio

20-Aug-2001 12-Feb-2009 N/A due to p/n

FAA, U.S AD 2004-03-08

To prev. structural damage to eng.pylons

LEARJET SB 51-03 LEARJET SB 51-04 Rev 5

08-Mar-2004 09-Mar-2004 SB 51-04 previous carried out.

FAA, U.S AD 2005-13-36

Detailed inspection of aileron cable. 09-Aug-2005 01-Nov-2005

FAA, U.S AD 2005-16-09

Inspection of Tip Tank Flapper Valves Supersedes AD 95-25-03

LEARJET SB 28-10 13-Sep-2005 14-Sep-2005 Flapper p/n 2323006-802 previously installed. No further action req.

FAA, U.S AD 2007-04-18

Modify Standby Fuel Pump switches LEARJET SB 28-11 Rev 5

23-Mar-2007 15-Mar-2007 Previusly complied with. Ref. Learjet SB 28-11

FAA, U.S AD 2007-17-17

Unsealed gaps in engine firewall 02-Oct-2007 11-Sep-2007 Previously carried out, ref. SB 54-03

FAA, U.S AD 2008-02-19

HP-Turbine Disc replacement. 19-Feb-2008 06-Feb-2008 N/A due to engine model.

FAA, U.S AD 2008-19-12

Remove from service ITT Duct 08-Aug-2012

FAA US AD 74-08-09

3 Transport category airplanes equipped with lavatories

11-May-2012

FAA, U.S AD 78-16-03

To precl. a fail. of the Refr. Cond. Fan Issued 1978-08-17

LEARJET SB 21-03 11-Dec-2000 20-Jan-1984

FAA, U.S AD 79-08-01

1 Aeronca thrust Reversers Suppl to AFM

19-Apr-1982 1 13-Feb-2009 N/A Aeronca Thrust Reversers not installed

FAA, U.S AD 80-06-02

Starter assisted airstart 24-Mar-1980 03-Dec-1993

FAA, U.S AD 80-07-09

Cabin Main Entrance Upper Door LEARJET AMK79-09 01-May-1980 25-Jun-1980

FAA, U.S AD 80-17-11

Airspeed Limitation Placard LEARJET SB 11-03 Rev A

28-Aug-1980 19-Aug-1987


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FAA, U.S AD 80-18-08

To Prevent loss of Emergency electrical Power............

28-Aug-1980 01-Jan-2003 N/A N/A due to Component p/n

FAA, U.S AD 80-19-09

1 Motive Flow Valve LEARJET AMK80-07 11-Dec-1980 1 05-Nov-1980

FAA, U.S AD 80-19-11

1 AFM insert LFV LVD1635 Rev A 20-May-1985 1 09-Feb-2006 Checked. Previously complied with.

FAA, U.S AD 81-04-06

Cockpit Voice Recorder A100 series 01-Apr-1981 12-Feb-2009 N/A due to model & s/n

FAA, U.S AD 81-13-07

To ensure oper. without fuel starvation

LFV LVA1748 25-Jun-1981 10-Aug-1981

FAA, U.S AD 82-01-05

2 Stall Warning Accelerometer Check LEARJET SB 27-12 Rev B LFV LVA1912

10-Apr-1986 2 30-May-2007 Överförd till A1 phase insp. Ref. Learjet Chpt.5 rev.74 och FAA AMOC från 2005-03-24

FAA, U.S AD 83-08-03

Insp.RH Engine Hydraulic Pressure Line for Interference.

LEARJET SB 29-01 Rev 1

03-May-1983 12-Apr-1983

FAA, U.S AD 84-19-06

To prevent Aileron/Trim Tab Flutter due to failure of the trim tab ctrl system

22-Oct-1984 01-Oct-2009 PCW

FAA, U.S AD 84-20-06

Inspect LH Hydraulic Lines for Interfere superseded by 86-22-05

LEARJET SB 29-02 20-Feb-1987

FAA, U.S AD 85-16-04

Airplane Lateral Control Characteristics

FAA, U.S AD 96-19-13 LEARJET AMK83-05 LFV LVD2034

06-Sep-1985 06-Feb-2002 N/A due to config. (STC SA766NW never been installed).

FAA, U.S AD 85-22-10

Collins HSI & FD indicators 31-Dec-1985 15-Jun-2009 N/A by p/n & s/n

FAA, U.S AD 86-05-05

1 Relocation of Battery Vent Inlet Fitting

LEARJET SB 24-10 LFV LVD2046

19-Jan-1988 1 10-Dec-1985

FAA, U.S AD 86-22-05

To prevent of flap operation.......... LEARJET AMK86-04 10-Nov-1986 20-Feb-1987

FAA, U.S AD 87-02-06

Insp. of Fwd. Eng.Mounts for Cracks LEARJET SB 71-03 Rev 1

06-Feb-1987 17-Jan-2005 Para.A: see Phase A3 300 hour insp. Para.B: see A/C status RAL

FAA, U.S AD 87-04-06

Autopilot FC-530 Limitations 09-Mar-1987 12-Feb-2009 N/A due to A/P model

FAA, U.S AD 87-06-09

Inspection of Mechanical Prod. C/B's 27-Apr-1987 01-Oct-2009 PCW Ref. Jet East Inc. 25 july 1988 (gammal aircraft logbook)

FAA, U.S AD 89-12-01

Inspection of Drag Chute Riser LEARJET SB 25-07 Rev A

03-Jul-1989 01-Oct-2009

FAA, U.S AD 90-09-10

Replace Texas Instr. Circuit Breakers 30-May-1990 01-Oct-2009 N/A due to type of C/B not installed in aircraft Ref. Learjet PC.

FAA, U.S AD 91-03-08

Deactivation of Forward Cabinet and Overhead Fluoriscent Light Circuits

LEARJET SB 33-05 Rev A

12-Feb-1991 22-Sep-2009 Post mod SB 33-06A


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FAA, U.S AD 92-19-12

SYSTEM TUBE (W-IN 30D) LEARJET AMK90-05 17-Nov-1992 17-Jun-1993

FAA, U.S AD 94-21-06

Safety belt LFV LVD2588 25-Nov-1994 01-Oct-2009 N/A due to p/n

FAA, U.S AD 95-19-04

1 Omega Navigation System 27-Mar-2000 1 03-Dec-2010 AD note cancelled

FAA, U.S AD 95-20-03

Insp.of Cabin Pressurization Outflow....

LEARJET SB 21-19 02-Nov-1995 24-Jan-1996

FAA, U.S AD 95-22-01

IR ALC Series 66 fluorescent lamps 07-Aug-2012

FAA, U.S AD 95-25-03

Inspection of Tip Tank Flapper Valves

LEARJET SB 28-10 27-Dec-1995 24-Jan-1996

FAA, U.S AD 96-19-13

Raisbeck Group STC SA766NW FAA, U.S AD 85-16-04 LEARJET AMK83-05

22-Oct-1996 09-Feb-2006 N/A due to config. (STC SA766NW never been installed).

FAA US AD 97-05-03

1 GNS XLS and GNS XL system 01-Nov-2011

FAA, U.S AD 98-06-28

Electrical Arcing and Fire Hazard LEARJET SB 21-24 Rev 1

24-Apr-1998 15-Sep-2009 N/A due to s/n

FAA, U.S AD 98-25-10

1 Inspection of seat restraint system LFV LVD2929 Rev 2 14-Jan-2000 1 01-Oct-2009 N/A due to manufacturing year

FAA, U.S AD 99-08-21

Oxygens Masks 02-Jun-1999 30-Sep-2009 N/A due to different cure date

FAA, U.S AD 99-23-19

Replacement or Spoiler Actuator LEARJET SB 27-36 28-Oct-1999 12-Feb-2009 N/A due to s/n

FLIGHT INT, Flight international inc.

FLIGHT INT STC SA1604SO

Hard points 26-nov-99 17-nov-88

KEITH, Keith Products, Inc.

KEITH SB 163 B Load Shed Installation 19-Nov-1999 15-May-2007

KEITH SB 166 A Belt Guard Installation 08-Oct-2001 15-May-2007

KEITH STC ST09366SC

Install. of Electric-Driven Vapor A/C 12-Aug-1997 21-Jul-1999


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LEARJET, Bombardier, LEARJET

LEARJET AAK 76-03

WING ICE L. 30-Jun-1976 10-Nov-1988

LEARJET AAK 78-03

A MLG OLEO ST PISTON 30-Jun-1978 A 10-Dec-1985

LEARJET AAK 79-02

PITOT HEAT IND. 30-Jun-1979 25-Jul-1988

LEARJET AAK 79-04

CONICAL FAN SPINNER 30-Jun-1979 10-Nov-1988

LEARJET AAK 80-02

INCREASE T.O. WEIGHT 30-Jun-1980 10-Dec-1985

LEARJET AAK 80-03

INCREASE LAND.WEIGHT 30-Jun-1980 10-Dec-1985

LEARJET AAK 81-01

1 Starter Contactor 30-Jun-2008 1 16-Sep-2008 PCW

LEARJET AAK 82-02

1 Install. Cabin Temp.Contr.Syst.filters 01-Oct-1982 1 22-Jan-2003 Final complied w/o C04708

LEARJET AAK 85-08

GS ANTENNA 30-Jun-1985 10-Dec-1985

LEARJET AAK 86-02

1 Inst. of LDG Actuator Down Lock Switch

22-Sep-2008 1 04-Nov-2008 Checked PCW.

LEARJET AAK 89-03

Installation of Doublers at Frame 6. 08-Jan-1990 29-Aug-2001 Installation doubler at frame #6 on R/H side

LEARJET AAK 89-04

D Inst. of Doublers at Frame 7 11-Aug-1995 D 29-Aug-2001

LEARJET AAK 89-14

25 DG.FLAP LIMIT SWITCH 30-Jun-1989 02-May-1990

LEARJET AAK 90-12

1 Inst. of Batting at Wing Spar 1 Splice 22-Sep-2008 1 04-Nov-2008 Checked PCW.

LEARJET AAK 90-16

IR Overhead Fluorescent Light. Wiring Prov.

30-Jan-1991 IR 22-Sep-2009

LEARJET AAK 91-05

1 Inst of Defog Temperature Sensors 16-Feb-2009 1 05-Jun-2009 N/A Due to Electric Windshield not installed

LEARJET AMK 78-02

2 DOOR HANDLE 30-Jun-1978 06-Feb-1991 N/A due to s/n of aircraft.

LEARJET AMK 78-08

A GENERATOR DRIVE SPLINES DRIVE SHAFT

30-Jun-1978 A 25-Jun-1980

LEARJET AMK 78-12

A ENGINE BLEED AIR PLUMBING 30-Jun-1978 A 26-Jun-1979


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LEARJET AMK 78-13

A ESS.BUS 04-Jun-2007 A 11-Sep-2007 Previously carried out, ref. AMK 78-13

LEARJET AMK 79-06

EMERG.PRES. VALVE 30-Jun-1979 22-Oct-1979

LEARJET AMK 79-07

GENERATOR DRIVE SPLINES 30-Jun-1979 25-Jun-1980

LEARJET AMK 79-09

CAB.DOOR MECHANISM (AD800709) (AD800709)

FAA, U.S AD 80-07-09 LFV LVA1613

30-Jun-1979 25-Jun-1980

LEARJET AMK 79-10

ENGINE FUEL TUBE 30-Jun-1979 25-Jun-1980

LEARJET AMK 80-06

A ENG.MOUNT (AD801711) (AD801711)

30-Jun-1980 A 27-Feb-1981

LEARJET AMK 80-07

MOTIVE FLOW VALVE (AD801909) (AD801909)

FAA, U.S AD 80-19-09 Rev 1 LFV LVA1625 Rev A

30-Jun-1980 05-Nov-1980

LEARJET AMK 80-17

1 Installation of Current Limiter Warning

28-Jun-2010 A 23-Jan-2009 Starter engage lamps, moved to opt. position

LEARJET AMK 81-17

HOR.STAB. HINGE PIN 30-Jun-1981 22-Jun-1982

LEARJET AMK 83-03

AILERON TRIM TAB BALANCE WEIGHT (AD84190 (AD84190

30-Jun-1983 01-Oct-2009 PCW

LEARJET AMK 83-05

WING STALL STRIP (AD851604) (AD851604)

FAA, U.S AD 85-16-04 FAA, U.S AD 96-19-13

30-Jun-1983 20-Feb-1987 N/A due to config. (STC SA766NW never been installed).

LEARJET AMK 85-01

A POWER DIST. 30-Jun-1985 A 24-Jan-1996

LEARJET AMK 86-04

WING FLAP SECTOR (AD862205) (AD862205)

FAA, U.S AD 86-22-05 30-Jun-1986 20-Feb-1987

LEARJET AMK 90-04

A Replacement of Parallelling Control Box

01-Aug-1992 26-Jan-1993

LEARJET AMK 90-05

SYSTEM TUBE (AD921912) (AD921912)

FAA, U.S AD 92-19-12 09-Oct-1991 05-Feb-1993

LEARJET AMK 91-2A

Windshield Anti-Ice Thermostat Replacem. Learjet SIL 30-005

12-Aug-1998 15-Nov-1999

LEARJET AW 32-021


FAA, U.S AD 2001-07-11 05-Feb-2001 17-May-2001 N/A by s/n on tire.

LEARJET SB 00-01

Inspection/Replacement of cables 27-Feb-2001 10-Apr-2001 Kontr.i status

LEARJET SB 05-01

FIRE EXT. BOTTLE (HYDROST.) 18-Nov-1992 21-Jun-1993

LEARJET SB 11-03

A AIRSPEED LIMIT PLACARDS AD841906

FAA, U.S AD 80-17-11 18-Sep-1980 A 19-Aug-1987


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LEARJET SB 11-04

WASTE DISP.REC. PLACARDS AD740809

18-Dec-1981 23-Apr-1982 N/A due to model and s/n.

LEARJET SB 11-05

CREW SEAT BELT PLACARDS 31-Aug-1983 20-Oct-1980

LEARJET SB 11-06

BATTERY PLACARDS 21-Jul-1987 19-Aug-1987 N/A due to SB32-04 is carried out.

LEARJET SB 11-07

ID PLATE (O) 06-Nov-1992 01-Jan-1994

LEARJET SB 11-10

Repl.of Fuel Servicing Placards 17-Dec-2001 10-Dec-2003

LEARJET SB 21-03

CONDENSER FAN ASSY. AD781603

FAA, U.S AD 78-16-03 12-Jul-1978 20-Jan-1984

LEARJET SB 21-04

Inst. of Refrigeration Syst.Warn.Placard

22-Feb-1979 09-Feb-1979

LEARJET SB 21-05

CABIN PRES. SAFETY VALVE 18-Dec-1979 25-Feb-1980

LEARJET SB 21-06

Insp.of Air Distr.Sleeves & Clamps-Tailc

23-Sep-1980 27-Feb-1981

LEARJET SB 21-07

CABIN PRES. SAFETY VALVE (CHANGED) Garrett SB 5-2290

28-Oct-1980 12-Apr-1991

LEARJET SB 21-09

Insp.Cabin Press. Control Module for PN

12-Sep-1983 20-Jan-1984

LEARJET SB 21-12

Insp. of Pneumatic Duct Temp. Limiter

26-Sep-1989 10-Nov-1990

LEARJET SB 21-14

1 OUTFLOW VALVE SAFETY VALVE (R)

03-Jan-1995 1 24-Jan-1996 Superseded by SB 21-19.

LEARJET SB 21-15

2 Repl. of Refrig.Syst. Press Switch 22-Jul-2005 2 11-Oct-2005 N/A to Keith R34.

LEARJET SB 21-16

Mod. of Aux Cabin Heater Relay Assy

16-May-1994 13-Apr-2006

LEARJET SB 21-18

3 Imp.W-shield Aux.Defog & Aux.Crew Heat

11-Aug-2008 3 04-Nov-2008 N/A N/A due to AAK86-1 not incorporated

LEARJET SB 21-19

Insp.of Cabin Press.Outflow & Safety Vlv 130406-21-A4011 R2,102850-21-A4021 R2

FAA, U.S AD 95-20-03 03-Jan-1995 24-Jan-1996

LEARJET SB 21-20

Repl. Cabin Press. Outflow valve Assy

14-Jul-1995 16-Sep-1999

LEARJET SB 21-22

1 Inst.of Cabin Air Syst. Electr.Connector

15-Aug-2003 1 03-Nov-2003 N/A due to s/n of aircraft.

LEARJET SB 21-24

1 Repl.of Aux.Cabin Heater Wiring FAA, U.S AD 98-06-28 13-Aug-1996 1 15-Sep-2009 N/A due to s/n


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LEARJET SB 21-25

3 Inst.of Improved Refrigeration Comp.Asse

12-Nov-2007 2 06-Feb-2008 N/A Due to Keith Aircondition System TR-134 Installed

LEARJET SB 21-26

5 Mod.of Auxiliary Cabin Heather 16-May-2007 5 05-Mar-2012

LEARJET SB 22-03

Repl.of Yaw Damper Servo Sector Bolts

02-Feb-1979 03-Feb-1979

LEARJET SB 22-04

C Mod. of Mach Trim Computer J.E.T SB 501-1132-9E, -10B, -11

25-Mar-1980 C 20-Feb-1980

LEARJET SB 22-05

Mod.of FC-530/-535 Autopilot Computer

05-Jan-1987 12-Apr-1991 N/A N/A due to A/P model

LEARJET SB 22-07

3 Inst.of Autopilot Accelerometer Monitor

11-Jun-2007 2 29-May-2007 N/A AAK 83-2 not complied with.

LEARJET SB 23-03

2 Increased FOD Protection-Installation of Antenna Protection.

09-Jul-2001 2 11-Jan-2006 Previous revision carried out.

LEARJET SB 24-06

Insp.of Battery Vents for Obstruction 29-Sep-1980 21-Oct-1980

LEARJET SB 24-07

Current Limiter Box Moisture Proofing 15-Jan-1981 12-Apr-1991

LEARJET SB 24-08

Insp.of No.4 Gauge Electrical Cables 11-May-1982 26-Jan-1983

LEARJET SB 24-09

Insp.Fuses for Proper Prot.Covering & PN

19-Apr-1983 22-Jul-1983

LEARJET SB 24-10

Reloc.of Battery Vent Inlet Fitting AD860505

FAA, U.S AD 86-05-05 Rev 1

18-jul-85 10-Dec-1985

LEARJET SB 24-11

Add.of Ret.for Gen.Warn.Ctrl Box.Connect

01-Nov-1990 12-Apr-1991

LEARJET SB 24-15

1 Inst.of Concorde Sealed Lead-Acid Batt.

24-Mar-2008 1 04-Sep-2008

LEARJET SB 25-03

Insp.of Drag Chute Mechanism Bolt 10-Nov-1980 15-Jan-1981

LEARJET SB 25-04

A Insp.of Drag Chute Mech.for Proper Clear

11-Nov-1981 A 23-Nov-1986

LEARJET SB 25-06

Insp.Drag Chute Canister Lid Latch Screw

19-Feb-1987 12-Feb-1987

LEARJET SB 25-07

A Insp.of Drag Chute Riser FAA, U.S AD 89-12-01 22-Mar-1989 A 01-Oct-2009

LEARJET SB 26-02

A Verif.& Ident.of Eng.Fire Ext.Bottl.Wire

30-Apr-1991 A 17-Jun-1991

LEARJET SB 26-04

1 Engine Fire Element Insp./repl. 11-Aug-2008 1 04-Nov-2008 N/A N/A by s/n on elements

LEARJET SB 27-03

A Repl.of Primary Control Syst.Stop Bolts

12-Sep-1975 A 19-Aug-1997 Checked. Previously complied with.


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LEARJET SB 27-09

Insp.of Wing Flap Actuators 19-Dec-1978 20-May-1975

LEARJET SB 27-10

Rework of Pilot/Copil.Ctrl Wheel Trim ..

19-Apr-1979 17-Aug-1979

LEARJET SB 27-11

Insp.of Aileron for Drain Holes 06-Nov-1979 01-Mar-1980

LEARJET SB 27-12

B Stall Warn.Accelerometer Op.Check FAA, U.S AD 82-01-05 Rev 2 LFV LVA1912

25-Sep-1981 B 30-May-2007 Överförd till A1 phase insp. Ref. Learjet Chpt.5 rev.74 och FAA AMOC från 2005-03-24

LEARJET SB 27-14

Insp.of Welds on Rudder Pedal Supp.Assy

08-Sep-1983 20-Jan-1984

LEARJET SB 27-16

Insp.Flap Attach.Fittings for Cracks 27-May-1986 05-Sep-1986

LEARJET SB 27-24

Insp.of Ail.& Rudder Ctrl Cable Assy 08-Nov-1993 01-Jan-1994

LEARJET SB 27-33

Removal of Sealant from Aileron Rib 27-May-1997 19-Aug-1997

LEARJET SB 27-35

4 Inst.of Secondary Locking Feature 15-Aug-2003 4 03-Nov-2003 Previous rev. carried out.

LEARJET SB 27-36

Replacement of Spolier Actuator FAA, U.S AD 99-23-19 14-Dec-1998 12-Feb-2009 N/A due to s/n

LEARJET SB 27-40

6 Insp/Inst. of Flap Structure Components

16-Aug-2010 6 10-Nov-2011 PCW Previous revision carried out

LEARJET SB 27-43

Recalibration rosemount 19-Jan-2005 17-Mar-2005 N/A due to STC ST00321WI-D not complied with.

LEARJET SB 27-45

1 Insp. Spoiler panels 02-Apr-2012

LEARJET SB 28-02 INAKTIV

Insp.of Tip Tank Elect.Conduit for Damag

20-Feb-1976 12-Apr-1991


Op.check of Fuel Jettison Valves 14-Feb-1980 23-Apr-1980

LEARJET SB 28-06

Insp.of Rec.for Field Rep.of Mot.Flow Vl

21-Aug-1980 09-Dec-1980

LEARJET SB 28-08

Insp.of Motive Flow Vlv Shroud Cover 27-Aug-1990 02-Nov-1990

LEARJET SB 28-10


FAA, U.S AD 2005-16-09 FAA, U.S AD 95-25-03

06-Oct-1995 14-Sep-2005 Flapper p/n 2323006-802 previously installed. No further action req.

LEARJET SB 28-11

5 Inst.of Standby Fuel Pump Annunciators

FAA, U.S AD 2007-04-18 28-Sep-2009 5 26-Feb-2010 Rev. 1-4 PCW. AFM cheched for Change 14

LEARJET SB 28-14

2 Repl.of Tip Tank Flapper Valves 09-May-2001 2 29-Aug-2001


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LEARJET SB 28-17

1 Inst.of Fuel Panel Overlay Blank. Plate

14-Jan-2004 1 30-Aug-2007 Cover installed

LEARJET SB 28-18

Insp./Repl. of Fuel Filter Elements 24-Aug-2009 30-Oct-2009 N/A due to filter p/n

LEARJET SB 29-01

1 Insp.RH Eng.Hydr.Press.Line for Interfer

FAA, U.S AD 83-08-03 10-Sep-1996 1 01-Nov-2005 N/A due to installation of reducingvalve 3000-1500 psi

LEARJET SB 29-02

Insp.LH Eng.Hydr.Lines for Interference

FAA, U.S AD 84-20-06 15-Jun-1983 23-Aug-1983

LEARJET SB 29-03

Insp.Hydr.Tube Assy & Wiring for Interf.

14-Jan-1985 18-Apr-1985

LEARJET SB 29-05

Repl.of Hydr.Reservoir Sight Glass Assy

07-Oct-1992 01-Jan-1994

LEARJET SB 30-01

Windshield Anti-Ice Timer Op. Check 19-Jan-1983 28-Feb-1983

LEARJET SB 30-10

1 Repl. of Wing Anti-Ice Transverse Duct

12-Feb-1999 1 04-Aug-2000

LEARJET SB 30-11

3 Inst.of High Current Capacity Wire 05-May-2008 3 04-Sep-2008 PCW

LEARJET SB 31-01

Repl.of Oil Press.Annunciator Cap Assy

26-Oct-1992 01-Jan-1994

LEARJET SB 32-03

Insp.of LG Brake & Torque Link for Inter

25-Aug-1981 12-Apr-1991

LEARJET SB 32-04

Repl.of LG Hydraulic Selector Valve 23-Jan-1989 06-Nov-1990

LEARJET SB 32-07

1 Inst.of MLG Lower Torque Arms 10-Nov-1995 1 13-Jan-2004

LEARJET SB 32-18

Inst.of Main Landing Gear Wheel Screens

19-Jan-1999 15-Mar-1999 N/A. Affected Wheel Assy not installed.

LEARJET SB 32-20

Repl.of Landing Gear Shuttle Valve Bolt

09-Mar-2000 30-Jun-2000 Found N/A to Part Number.

LEARJET SB 32-21

Repl.of Brake Valve Adjustment Screw

01-May-2000 29-Aug-2001

LEARJET SB 32-23

1 Mod landing gear squat switch wiring 09-Apr-2007 1 29-May-2007 Previously carried out

LEARJET SB 32-26

Insp/Repl of the Nose Gear Wheel Assy

18-Jan-2010 10-May-2010 N/A by s/n

LEARJET SB 33-03

Insp.& Mod. of LH Fwd Cabinet Light Assy

24-Apr-1985 12-Apr-1991 N/A N/A due to interior config.

LEARJET SB 33-05

A Deactiv.of Fwd Cabinet & Overhead Light.

FAA, U.S AD 91-03-08 / AD901406

21-Dec-1990 A 12-Aug-1991

LEARJET SB 33-06

A Activ.of Fwd Cabinet & Overhead Fluore..

12-Apr-1991 A 22-Sep-2009


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LEARJET SB 34-04

Insp.of Static Ports 11-Jun-1982 21-Oct-1982

LEARJET SB 35-04

Replacarding Oxygen Bottle Shutoff Valve

27-Feb-2004 20-Sep-2004 N/A N/A by p/n on oxygen regulator

LEARJET SB 36-02

A Insp.& Repl.of Eng.Bleed Air Flex Tube..

25-May-1978 A 12-Apr-1991 N/A N/A by s/n on aircraft

LEARJET SB 36-03

Repl Air Bottle & Weight-Balance Change

14-Dec-2009 11-Mar-2010 Due to weighing after installation of bottle p/n 6600194-6

LEARJET SB 51-01

Insp.Baggage Comp.Struct. for Corrosion AD 84-12-03

18-Jul-1985 10-Dec-1985

LEARJET SB 51-03

Insp.of Forward Engine Beam Shear Web.

FAA, U.S AD 2004-03-08 01-Feb-2001 06-Sep-2001 N/A N/A due to SB 51-04 performed.

LEARJET SB 51-04

5 Rep.of Forward Engine Beam Shear Web

FAA, U.S AD 2004-03-08 12-Oct-2009 5 11-Mar-2010 No rework required

LEARJET SB 51-4

3 20-Jan-2005 No rework req.

LEARJET SB 52-04

Mod.of Access Door Lock Assemblies

16-Apr-1979 12-Apr-1991 Found N/A. No locks installed.

LEARJET SB 52-05

Insp.of Cabin Int.Liner-Areas Of Emerg..

04-Nov-1980 12-Apr-1991

LEARJET SB 52-06

Mod.of Lwr Cabin Door Hook Mechanism

18-Dec-1992 01-Jan-1994

LEARJET SB 52-07

Repl.of Lwr Cabin Door Cable & Handle As

15-Sep-1993 06-Feb-1995

LEARJET SB 52-10

1 Repl.of Upper Cabin Door Torsion Bar Arm

03-Jun-1999 1 20-Sep-1999 N/A. 24 inch door not installed.

LEARJET SB 53-07

Inspect for Tailcone Drains 18-Dec-1992 01-Jan-1994

LEARJET SB 53-08

Inst.of Nutplates on Circ.Br.Panel Suppo

14-Feb-1994 06-Feb-1995

LEARJET SB 53-10

1 Repl.of LowerStinger & Ventral Fin Skin

17-Mar-2008 1 14-May-2008 N/A Due to Avcon Fins STC ST00432WI

LEARJET SB 53-11

3 Mod.of Tailcone Ballast Weight Installat

01-Jun-2009 3 28-Jan-2010 N/A Not incorporated.

LEARJET SB 53-13

Insp. Intern. baggage comp. floor splice

16-Jan-2006 08-Mar-2006 N/A Due to S/N

LEARJET SB 54-01

Insp.for Silicon Firesleeve-Start&Gen Ca

11-Jun-1982 06-Oct-1982

LEARJET SB 54-03

Insp/Firewall Sealing Modification 16-Mar-2001 02-Nov-2005 R/H side carried out

LEARJET SB 54-04

Insp/Repl.of Upper and Lower Pylon Skins

08-Aug-2001 22-Mar-2002 N/A by s/n on aircraft.


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LEARJET SB 55-01

Insp.Horiz.Stab.Hinge Assy for Cracks

16-Aug-1991 16-Aug-1991 N/A No Thrust Reversers installed.

LEARJET SB 55-04

2 Inst.of Doublers on Horiz.Stabili.Skin 23-Feb-2009 2 10-Jun-2009 PCW

LEARJET SB 55-05

Imp.of Horiz.Stabilizer Actuator Access

16-Jan-1998 30-Sep-1998

LEARJET SB 55-06

Mod.of Navigation Light Wiring Conduit

30-Aug-2004 13-May-2005

LEARJET SB 71-02

Eng.Firewall Sealing at Feed-Thru Condui

13-May-1982 15-Jul-1982

LEARJET SB 76-01

B Insp.of Eng. I.T.T. Cable Connectors 07-Nov-1983 B 22-Jul-1983

LEARJET SB A27-42

Insp/Repl.of Aileron Ctrl Cables 23-Dec-2002 12-Dec-2002 Cables N/A by cal.time.

LEARJET SB A30-03

ALCOHOL ANTI-ICE SYSTEM (W-IN 10H)

18-Dec-1992 26-Jan-1993

LEARJET SB A32-15

1 Insp.of Landing Gear Actuator Pistons

21-Apr-1997 1 17-Apr-1998

LEARJET SSK 980

Evaporator Assy. 10-Feb-1989 20-Jul-1994

LEARJET SSK 981

Repl. of Spoiler Act. Support Bracket 19-Dec-1986 04-Aug-2000 Carried out on R/H side, kit 2692006-4.

LEARJET SSK 993

2 Repl. of Landing Gear Wheel Bearings

21-Jan-1991 2 14-Oct-1997 see w/o C00671 for 2 wheels

LFV, Luftfartsverket LFV

LVA 1613 Modifiering av övre kabindörr LEARJET AMK79-09 27-May-1980 25-Jun-1980

LFV LVA 1625 A Till,gg i flyghandbok. T,thetskontroll FAA, U.S AD 80-19-09 Rev 1 LEARJET AMK80-07

23-Jun-1980 A 05-Nov-1980

LFV LVA 1748 Revision av Flyghandbok. Br,nslem,ngd

FAA, U.S AD 81-13-07 24-Aug-1981 10-Aug-1981

LFV LVA 1912 Periodisk kontroll av Stallvarning. FAA, U.S AD 82-01-05 Rev 2 LEARJET SB 27-12 Rev B

10-Nov-1983 30-May-2007 Överförd till A1 phase insp. Ref. Learjet Chpt.5 rev.74 och FAA AMOC från 2005-03-24

LFV LVD 1635 A Revision Flyghandbok/kontr. A/P & mod.

FAA, U.S AD 80-19-11 Rev 1

15-Jul-1985 A 28-Sep-2009 PCW Ref. FAA AD 80-19-11 R1

LFV LVD 2034 Reducering av MMO FAA, U.S AD 85-16-04 30-Aug-1985 06-Feb-2002 N/A due to config. (STC SA766NW never been installed).


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LFV LVD 2046 Kontroll av batterihållare FAA, U.S AD 86-05-05 Rev 1

25-nov-85 10-Dec-1985

LFV LVD 2352 Shoulder Harness Inst. FAA AC 43-13 CHPT 9 23-May-1991 17-Jun-1991 checked OK.

LFV LVD 2588 Byte av säkerhetsbälten FAA AD 94-21-06

FAA, U.S AD 94-21-06 05-Jan-1995 01-Oct-2009 N/A due to p/n

LFV LVD 2853 Periodisk funktionskontroll av nödutgång

23-Mar-1998 13-Aug-2010

LFV LVD 2929 2 Kontroll av bältens låsfunktion AD 98-25-10

FAA, U.S AD 98-25-10 Rev 1

13-Jan-2000 2 01-Oct-2009 N/A due to manufacturing year

LFV LVD 3148 Modif. Transponder kontrollpanel 17-Aug-2001 12-Feb-2009 N/A due to p/n

NYGE, Saab Aerotech Aircraft Services

NYGE SB 08-06-34-03 A

EGPWS System Provision for Inhibit Unit)

30-Nov-2009 A 08-Feb-2010

NYGE SSB DR-MGPC-YELL

A 29-Nov-2006

NYGE TDM 12-22

A L35A Move mission inverter A 10-Sep-2012

NYGE TDM 12.23

Installation laser prismor L35 A 10-Sep-2012

NYGE TDM 02-25

Installation Underving-kanaler 16-Oct-2002 12-Dec-2003 LFV app.No: M21/02 revision 1.

NYGE TDM 02-26

Box 3 Installation 01-Nov-2002 03-Dec-2003 Approved in accordance with EASA 2004-11267 and with LFV AFMS S04/89 R2.

NYGE TDM 02-28

Utv. Framtagning mod.balkar LR-35 18-Nov-2002 12-Dec-2003

NYGE TDM 03-03

B Operators Console L35A 02-Apr-2007 B 26-Feb-2008 only updated to rev.B

NYGE TDM 03-07

Alkan Fairings (mod.) 27-Feb-2003 12-Dec-2003 Approved by EASA no. 235 in accordance with LFV Mod. Cert. No. M29/03.

NYGE TDM 03-17

ACAS Installation 06-May-2003 28-Oct-2004 Approved i.a.w. EASA Doc. No: STC S.A.00255

NYGE TDM 03-19

Mission Inverter Modif. 20-Nov-2003 05-Dec-2003 Approved in accordance with LFV M37/03 and EASA 1985.

NYGE TDM 03-23

U95 Installation L35A 10-Sep-2003 D 08-Nov-2005 Rev.D updated


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NYGE TDM 04-03

D Astor L35A 16-Jan-2004 D 21-Nov-2012 Effektindikering/Ground test

NYGE TDM 04-06

C Darts System L35A 05-Dec-2006 01-Jan-2006 Approved in accordance with DOA 21J.108,04-06.

NYGE TDM 05-06

Removal of Reflector System 30-May-2005 11-Nov-2005 Approved i.a.w. DOA 21J.108,05-06

NYGE TDM 05-15

Install. Jumpseat Intercom 18-Jul-2005 08-Dec-2005 Approved in accordance with DOA 21J.108,05-15.

NYGE TDM 05-17

GMS anpassning i nya OP-racken 26-Aug-2005 08-Dec-2005 Approved in accordance with DOA 21J.108,05-17.

NYGE TDM 05-19

Install. GPS Map and GP&C Transponder

08-Sep-2005 11-Nov-2005 Approved in accordance with DOA 21J.108,05-19.

NYGE TDM 05-20

Install. Mission Equip. new OP-Console

13-Sep-2005 11-Nov-2005 Approved in accordance with DOA 21J.108,05-20.

NYGE TDM 05-26

Install. Cabin Side Wall Cable Channel

20-Oct-2005 11-Nov-2005 Approved in accordance with DOA 21J.108,05-26.

NYGE TDM 05-34

Install. Structural Plug FAA STC SA2479CE

11-Nov-2005 11-Nov-2005 Approved in accordance with DOA 21J.108,05-34.

NYGE TDM 06-22

Re-mod. Hydraulic system 05-May-2006 15-May-2007

NYGE TDM 06-33

Robot 15 Radar Altimeter (Nav Demo Pod)

05-Jul-2006 26-Oct-2006

NYGE TDM 06-34

Meteor Proximity Fuse 05-Jul-2006 26-Oct-2006

NYGE TDM 06-36

A A100 (to carry on L35A) 23-Apr-2007 A 25-Feb-2008

NYGE TDM 08-02

C Enhanced Surveillance L35A 09-Mar-2010 C 18-Aug-2009 Original compliance to rev A of TDM. TDM rev B and C does not affect previous compliance.

NYGE TDM 08-06

C EGPWS MK.8 & Mission Inhibit System

05-Mar-2010 C 30-Oct-2008 Original compliance with rev A. Rev B and C does not affect previous compliance.

NYGE TDM 08-07

E LR35A GPS-Map Display 12-Apr-2010 E 10-Sep-2012 Compliance was IAW TDM rev B. Previous compliance not affected by rev D.

NYGE TDM 08-09

C Install termination resistors D 01-Sep-2012

NYGE TDM 08-13

A Barlast DARTS L35A 10-Mar-2008 A 10-Mar-2008

NYGE TDM 08-17

C ELT 406 L35A 04-Jul-2008 C 03-May-2010 Original compliance with TDM rev A. Rev B and C does not affect previous complaiance.


2012-12-06


27(195)

NYGE TDM 08-26

A Mission Antenna Adapter 28-Oct-2008 A 15-Dec-2008

NYGE TDM 09-01

C LR35A U-95 SORC Lite 24-Sep-2009 C 30-Sep-2009 Original compliance i.a.w rev B

NYGE TDM 09-30

E LR35A Removable Hard Disk Drives 30-Apr-2010 E 04-July-2012

NYGE TDM 10-04

A Overload Sensing Control 02-Jun-2010 A 14-Oct-2010 Initial complaiance was I.A.W TDM rev 2

NYGE TDM 10-27

A LR35A U95-D2 22-Apr-2010 A 15-Jun-2010

NYGE TDM 95-01

Installation Intercom 10-Jan-1995 24-Jan-1995

NYGE TDM 95-02

Modifiering Transponder-system 10-Jan-1995 24-Jan-1995

NYGE TDM 96-01

Miss-rack,GPS-antenn,CVR,inverter m.m.

12-Feb-1996 15-Mar-1996

NYGE TDM 97-01

TAPS 20-Feb-1997 01-Jan-1998

NYGE TDM 97-09

Kontrollprogram SE-DHO 26-Nov-1997 01-Jan-1998

NYGE TDM 98-06

Astor L35A 09-Mar-1998 10-Feb-1998 Approved in accordance with LFV M20/99.

NYGE TDM 98-12

Installation BRNAV L35A 26-Jun-1998 16-Apr-1998 Approved in accordance with S-CAA Approval reference LS 2005-7326.

ROCKWELL, Rockwell Collins U.K.Ltd

ROCKWELL SIL 07-1

Reply Inhibition On The Ground EASA AD 2009-0097 Rev IR

25-May-2007 18-Aug-2009 PCW Are in compliance with EASA AD2009-0097 Ref TDM03-17 DWG MF1030064-1 Rev.C


2012-12-06


28(195)

1.3 GFE Aircraft Learjet 35A SE-DHP


Number:


total Hours:

Total

Landing

Cycles:

Date

Reference:

Learjet

35A

075 SE-DHP 12549 8437 2012-11-23

1.3.2 Engines Type: TFE731-2-2B

Serial

Number:

Total Hours

Since New:

Total

Cycles

Since New:

Hours

remaining

to MPI:

Hours

remaining

to CZI:

Left Engine P-74542 14889 11860 549 561

Right Engine P-74277 10913 7322 1051 3851


Autopilot JET FC 200

Dual VHF-COM Collins VHF-22C

HF-COM Collins 718U-5

ICS & Audio System DB System

Dual VHF-NAV Collins VIR-30A

GPS Garmin GPS 165 TSO

Dual DME Collins DME40

ADF 1 & 2 Bendix/King KDF-806

XPDR 1 & 2 Collins TDR94D Mode S

EHS

TCAS II Collins TCAS-4000

TCAS II VSI/RA/TA Indicator LH /

RH

Collins TVI-920

TAWS / EGPWS Honeywell MK VI

RDR ALT Collins ALT-55B

Weather Radar Honeywell Primus 400

MFD Display Honeywell MFRD


Dual Mach Airspeed indicator IDC 2680003-2

Altimeter incl. encoder LH IDC 28007-017

Altimeter RH IDC 23932-053

Altitude Report & Alerting System IDC 23989-011

Air Data Display Unit 9D-80130-32

Flight Director Indicator LH Collins 329B-7R-2

Vertial Gyro Indicator RH JET 5-4000-08


2012-12-06


29(195)

Dual VG-Gyro JET VG-206EL

Standby Altitude Gyro JET AI 804

Horizontal Situation Indicator LH Collins 331A-6R

Horizontal Situation Indicator RH Collins 331A-3G

Dual RMI Collins 332C-10

Dual DG-Gyro JET DN-101D

RVSM

FDR Sundstrand 980-4100-FWUS

CVR Fairchild 93-A100-83



FR31 VHF/UHF COM Radio

AN/ARC 182 VHF/UHF COM Radio

GPS MAP System


KGS SPS-3052B Inverter 230VAC 50Hz

Laser Prism

Wing Pylon


EW system


ADRIAN C & S Pod mounted system

U95-N Pod mounted system

U95-D2 Pod mounted system

U95 Sorc Pod mounted system

A100 Pod mounted system


DARTS Pod mounted system

GMS Pod mounted system

Chaff Dispenser

BOX 3 Pod mounted system

Target Towing

MTR 101 Outboard pod mounted winch


TLX Height keeping target


TAPS


2012-12-06


30(195)


System:


Adrian C & S, U95-N, U95-

D2, U95 Sorc, A100, DARTS,

GMS, BOX 3 and MTR 101

General Signal Harness General Signal Harness Two pair shielded

AWG 20 x 25

MTR 101 MTR 101 Harness MTR 101 Harness Two pair shielded

AWG 20 x 3

AWG 16 x 4 +

shield U95-N, U95-D2, U95

Sorc, A100 and GMS MIL-STD-1553B Data

Bus

MIL-STD-1553B Data

Bus

Twinax x 8

U95-N, U95-D2, U95 Sorc,

A100, DARTS and GMS AC Power

115/200VAC 400 Hz 3-

Phase 3 x 10 A

AC Power 115/200VAC

400 Hz 3-Phase 3 x 10 A

AWG 12 x 10 +

shield

Adrian C & S, GMS and BOX

3 DC Power 28 VDC 150

A

DC Power 28 VDC 150

A

AWG 4 x 4

MTR 101 Coaxial 2 x 75 Ω Coaxial 2 x 75 Ω

Adrian C & S Coaxial 3 x 50 Ω Coaxial 3 x 50 Ω

Recognition Light Recognition Light

Cable

Recognition Light Cable AWG 16 x 4 +

shield

1.3.6 Antenna layout


2012-12-06


31(195)

1.3.7 Inspektion due times and dates Status date November 23

rd 2012.

Description Maint. RefC/Out date C/Out Hrs Due Hrs Due date Due Landings

Aircraft SE-DHP

Phase A 300 hour insp. AMP 2012-01-09 12407 12707 2013-02-09

Phase B 600 hour insp. AMP 2012-01-09 12407 13007 2014-02-09

Phase C 1200 hour insp. AMP 2010-11-05 12288 13488 2014-11-04

Phase D 2400 hour insp. AMP 2010-12-01 12288 14688 2018-11-29

Special operational fatigue inspect AMP 2009-02-26 11911 13111,3

12000 Hrs Inspection AMP 2001-03-26 10287,00 16287

45 days insp. AMP 2012-11-16 12547 2012-12-31

6 Month Inspection AMP 2012-08-06 12509 2013-02-06


12 Year Airframe inspection AMP 2001-03-25 2013-03-22 13042

MPI engine zone inspecition LH AMP 2007-04-17 11653 13053,5

MPI engine zone inspecition RH AMP 2010-03-04 12186 13586,7



3000 Landing Inspection AMP

6000 Major Landing Gear Inspection AMP 1998-08-19 12000

Operator's Console 300h/1y insp. AMP 2011-11-24 12400 12707 2013-02-09

ACAS 2 (TCAS) 24month insp. AMP 2011-11-24 12400 2013-11-23

Mission equipment 300 hour insp. AMP 2012-01-17 12407 12707,8














2012-12-06


32(195)

1.3.8 Implemented Changes Status date November 23rd 2012. For abbreversions see chapter 1.2.8

SB/AD etc

Reference


AVCON, Avcon

Industries, Inc

AVCON STC SA00432WI

R Install. Avcon Fins 31-mar-05 R 12-jul-06

AVCON STC

SA2479CE

A Install. Plug of Dual Hatches 30-jun-05 A 12-jul-06

AVCON STC

ST00564WI

AFM suppl. increase T/O weight........ 25-aug-97 13-jul-06

AVCON STC

ST00611WI

C Increase Takeoff Weight to 19600

pounds

11-mar-05 C 12-jul-06

AVCON STC

ST00612WI

B Increase Wing/Tip Zero Fuel Weight 28-nov-97 B 12-jul-06

AVCON STC

ST00613WI

C Increase Landing Weight to 16000

pounds

11-mar-05 C 12-jul-06

EASA, European

Aviation Safety

Agency

EASA AD 2006-0265

Incorrect transponder altitude 30-Aug-2006

13-Nov-2009

EASA AD 2008-0159

Improve EHS Operation HONEYWELL SB MST 67A-34-56 HONEYWELL SSBMST 67A-SW5 Rev 1

25-Aug-2008

01-Dec-2010 N/A transponder P/N installed

EASA AD 2009-0097

IR Mode S Transponder -Check/Modification

DHC SB 8-34-243 Rev A EASA AD 2010-0067 ROCKWELL SIL07-1

29-Apr-2009

IR 28-Jul-2009

EASA AD 2009-0173

1 Mode S Transponder Mod/Repl 30-Sep-2010

1 08-Dec-2010 N/A due to ADC p/n


2012-12-06


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EASA AD 2009-

0251-E

Portable Fire Extinguishers-

Ident/Repl

25-Nov-

2009

07-May-

2010

N/A N/A by current P/N installed

EASA AD 2009-

0262

Halon 1211 Fire Extinguishers Id/Repl EASA AD 2009-0278 FFE ASB26-

115 Rev C

15-Dec-

2009

07-May-

2010


EASA AD 2009-

0278

Halon 1211 Fire Extinguishers Id/Repl EASA AD 2009-0262 22-Dec-

2009

07-May-

2010


EASA AD 2010-0003


11-Jan-2010

R1 10-Mar-2010

N/A due to p/n

EASA AD 2010-

0204

IR Mode S Transponder -Mod/Repl 06-Oct-

2010

IR 08-Dec-2010 N/A by ADC p/n installed

EASA AD 2012-

0237

KIDDE GRAVINER HAND OPERATTED

FIRE EXTINGUISHER

06-sep-2012

EASA STC

EASA.IM.A.S.0144

9

Install. of Dual Openable Hatches 20-feb-06 23-nov-06

FAA, U.S, Federal

Aviation

Administration

FAA, U.S AD 2000-24-19

Donning oxygen masks 22-nov-00 26-feb-03 Complied with by insert of AFM change 12

FAA, U.S AD 2001-07-11


LEARJET AW 32-021 01-May-2001

17-May-2001 N/A by s/n on tire

FAA, U.S AD 2001-

15-17

Prevent erroneous altitude

interpretatio

20-aug-01 12-feb-09 N/A due to p/n

FAA, U.S AD 2004-

03-08

To prev. structural damage to

eng.pylons

LEARJET SB 51-03 LEARJET SB 51-04

Rev 5

08-mar-04 09-mar-04 SB 51-04 previous carried out.

FAA, U.S AD 2005-

13-36

Detailed inspection of aileron cable. 09-aug-05 19-sep-05 Checked OK.

FAA, U.S AD 2005-

16-09


Supersedes AD 95-25-03

LEARJET SB 28-10 13-sep-05 14-sep-05 Flapper p/n 2323006-802 previously installed. No

further action req.

FAA, U.S AD 2007-

04-18

Modify Standby Fuel Pump "switches" LEARJET SB 28-11 Rev 5 23-mar-07 15-mar-07 Previusly complied with. Ref. Learjet SB 28-11

FAA, U.S AD 2007-

17-17

Unsealed gaps in engine firewall 02-Oct-

2007

11-sep-07 Previously carried out, ref. SB 54-03

FAA, U.S AD 2008-02-19

HP-Turbine Disc replacement. 19-feb-08 06-feb-08 N/A due to engine model.

FAA US AD 74-08-09

3 Transport categoryairplanes equipped with lavatories

11-May-2012


2012-12-06


34(195)

FAA, U.S AD 76-18-

07

Connection of Inverter to correct Bus LEARJET SB 24-03 11-dec-00 11-dec-00 This AD is carried out 1976-09-29

FAA, U.S AD 78-16-

03

To precl. a fail. of the Refr. Cond. Fan

Issued 1978-08-17

LEARJET SB 21-03 11-dec-00 11-dec-00 This AD is carried out 1978-07-30

FAA, U.S AD 79-08-

01

1 Aeronca thrust Reversers Suppl to

AFM

19-apr-82 1 13-feb-09 N/A Aeronca Thrust Reversers not installed

FAA, U.S AD 80-06-02

Starter assisted airstart 24-mar-80 03-dec-93

FAA, U.S AD 80-07-

09

Cabin Main Entrance Upper Door LEARJET AMK79-09 01-May-

1980

17-nov-80

FAA, U.S AD 80-17-

11

Airspeed Limitation Placard LEARJET SB 11-03 Rev A 28-aug-80 23-sep-80

FAA, U.S AD 80-18-

08

To Prevent loss of Emergency

electrical Power............

28-aug-80 01-jan-03 N/A due to Component p/n

FAA, U.S AD 80-19-

09

1 Motive Flow Valve LEARJET AMK80-07 LFV LVA1625

Rev A

11-dec-80 1 24-dec-80

FAA, U.S AD 80-19-

11

1 AFM insert LFV LVD1635 Rev A 20-May-

1985

1 09-feb-06 Checked. Previously complied with.

FAA, U.S AD 81-04-

06

Cockpit Voice Recorder A100 series 01-apr-81 12-feb-09 N/A due to model & s/n

FAA, U.S AD 81-13-

07

To ensure oper. without fuel

starvation

LFV LVA1748 25-jun-81 10-aug-81

FAA, U.S AD 82-01-

05

2 Stall Warning Accelerometer Check LEARJET SB 27-12 Rev B LFV

LVA1912

10-apr-86 2 12-jun-06 Överförd till A1 phase insp. Ref. Learjet Chpt.5

rev.74 och FAA AMOC från 2005-03-24

FAA, U.S AD 83-08-

03

Insp.RH Engine Hydraulic Pressure

Line for Interference.

LEARJET SB 29-01 Rev 1 03-May-

1983

19-dec-08

FAA, U.S AD 84-19-

06

To prevent Aileron/Trim Tab Flutter

due to failure of the trim tab ctrl

system

22-Oct-

1984

14-jun-85

FAA, U.S AD 84-20-

06

Inspect LH Hydraulic Lines for

Interfere superseded by 86-22-05

LEARJET SB 29-02 03-nov-86

FAA, U.S AD 85-16-

04

Airplane Lateral Control

Characteristics

FAA, U.S AD 96-19-13 LEARJET

AMK83-05 LFV LVD2034

06-sep-85 22-jan-86 N/A due to config. (STC SA766NW never been installed).

FAA, U.S AD 85-22-

10

Collins HSI & FD indicators 31-dec-85 15-jun-09 N/A by p/n & s/n

FAA, U.S AD 86-05-

05

1 Relocation of Battery Vent Inlet Fitting LEARJET SB 24-10 LFV LVD2046 19-jan-88 1 18-jun-86

FAA, U.S AD 86-22-

05

To prevent of flap operation.......... LEARJET AMK86-04 10-nov-86 03-nov-86


2012-12-06


35(195)

FAA, U.S AD 87-02-

06

Insp. of Fwd. Eng.Mounts for Cracks LEARJET SB 71-03 Rev 1 06-feb-87 17-jan-05 Para.A: see Phase A3 300 hour insp. Para.B: see A/C

status RAL

FAA, U.S AD 87-04-

06

Autopilot FC-530 Limitations 09-mar-87 12-feb-09 N/A due to A/P model

FAA, U.S AD 89-12-

01

Inspection of Drag Chute Riser LEARJET SB 25-07 Rev A 03-jul-89 07-dec-10 N/A N/A by Riser P/N installed

FAA, U.S AD 91-03-08

Deactivation of Forward Cabinet and Overhead Fluoriscent Light Circuits

LEARJET SB 33-05 Rev A 12-feb-91 19-dec-08

FAA, U.S AD 92-19-

12

SYSTEM TUBE (W-IN 30D) LEARJET AMK90-05 17-nov-92 15-feb-93

FAA, U.S AD 95-19-

04

1 Omega Navigation System 27-mar-00 1 03-dec-10 N/A AD note cancelled

FAA, U.S AD 95-20-

03

Insp.of Cabin Pressurization

Outflow....

LEARJET SB 21-19 02-nov-95 02-dec-95

FAA, U.S AD 95-22-

01

ALC Series 66 fluorescent lamps 07-Aug-2012

FAA, U.S AD 95-25-

03

Inspection of Tip Tank Flapper Valves LEARJET SB 28-10 27-dec-95 14-feb-96

FAA, U.S AD 96-19-

13

Raisbeck Group STC SA766NW FAA, U.S AD 85-16-04 LEARJET

AMK83-05

22-Oct-

1996

22-jan-86 N/A due to config. (STC SA766NW never been installed).

FAA US AD 97-05-

03

1 GNS XLS and GNS XL system 1-Nov-2011

FAA, U.S AD 98-06-

28

Electrical Arcing and Fire Hazard LEARJET SB 21-24 Rev 1 24-apr-98 09-dec-08 N/A due to s/n

FAA, U.S AD 98-25-

10

1 Inspection of seat restraint system LFV LVD2929 Rev 2 14-jan-00 1 03-dec-10 N/A Affected seat belts not installed

FAA, U.S AD 99-08-

21

Oxygens Masks 02-jun-99 19-dec-08 N/A due to different cure date

FAA, U.S AD 99-23-

19

Replacement or Spoiler Actuator LEARJET SB 27-36 28-Oct-

1999

09-dec-08 N/A due to s/n

FLIGHT INT, Flight

international inc

FLIGHT INT STC

SA1604SO

Hard points 26-nov-99 22-May-1989

KEITH, Keith

Products, Inc


2012-12-06


36(195)

KEITH SB 163 B Load Shed Installation 19-nov-99 B 17-apr-07

KEITH SB 166 A Belt Guard Installation 08-Oct-

2001

A 17-apr-07

KEITH STC

ST09366SC

Install. of Electric-Driven Vapor A/C 12-aug-97 06-aug-99

LEARJET,

Bombardier,

LEARJET

LEARJET AAK 71-13 F Gravel Runway Operations Kit 10-sep-99 F 27-mar-01

LEARJET AAK 76-03 WING ICE L. 30-jun-76 11-May-1989

LEARJET AAK 79-02 PITOT HEAT IND. 30-jun-79 03-jul-81

LEARJET AAK 79-04 CONICAL FAN SPINNER 30-jun-79 22-apr-89

LEARJET AAK 80-02 INCREASE T.O. WEIGHT 30-jun-80 15-nov-84

LEARJET AAK 80-03 INCREASE LAND.WEIGHT 30-jun-80 02-dec-88

LEARJET AAK 81-01 1 Starter Contactor 30-jun-08 1 16-sep-08 PCW

LEARJET AAK 82-02 1 Install. Cabin Temp.Contr.Syst.filters 01-Oct-1982

1 08-mar-06 N/A N/A by s/n

LEARJET AAK 83-06 VERT.STAB. ACCESS 30-jun-83 29-jul-84

LEARJET AAK 83-08 Inst.of Comp.to allow variable Pitch Trim Settings at takeoff

08-mar-85 28-nov-01 Checked. Previously complied with.

LEARJET AAK 84-03 A WINDSHIELD HEAT 30-jun-84 A 12-mar-85

LEARJET AAK 86-02 1 Inst. of LDG Actuator Down Lock

Switch

22-sep-08 1 04-nov-08 Checked PCW.

LEARJET AAK 89-04 D Inst. of Doublers at Frame 7 11-aug-95 D 27-mar-01

LEARJET AAK 89-14 25 DG.FLAP LIMIT SWITCH 30-jun-89 02-May-1990

LEARJET AAK 90-12 1 Inst. of Batting at Wing Spar 1 Splice 22-sep-08 1 04-nov-08 Checked PCW.

LEARJET AAK 90-16 IR Overhead Fluorescent Light. Wiring Prov.

30-jan-91 IR 10-mar-09

LEARJET AAK 91-05 1 Inst of Defog Temperature Sensors 16-feb-09 1 05-jun-09 N/A Due to Electric Windshield not installed

LEARJET AMK 76- A WING SKIN FASTENERS 30-jun-76 A 14-dec-79


2012-12-06


37(195)

02

LEARJET AMK 76-

07

1 CABIN AIR CONTR.VALVE 30-jun-76 24-dec-77

LEARJET AMK 76-

09

A OIL PRES. TRANSM. 30-jun-76 A 24-dec-77

LEARJET AMK 77-

01

AIL.CABLE PULLEY 30-jun-77 24-dec-77

LEARJET AMK 77-

03

ENGINE BLEED AIR VALVE 30-jun-77 24-dec-77

LEARJET AMK 77-

06

A WING BOLTS 30-jun-77 A 24-dec-77

LEARJET AMK 77-08

ESS.BUS C/B PANEL 30-jun-77 24-dec-77

LEARJET AMK 78-04

ENGINE BLEED AIR DUCT 30-jun-78 23-feb-86

LEARJET AMK 78-06

A ENGINE BLEED AIR TUBE 30-jun-78 A 08-nov-79

LEARJET AMK 78-08

A GENERATOR DRIVE SPLINES DRIVE SHAFT

30-jun-78 A 19-jun-85

LEARJET AMK 78-12

A ENGINE BLEED AIR PLUMBING 30-jun-78 A 15-jan-80

LEARJET AMK 78-13

A ESS.BUS 04-jun-07 A 11-sep-07 Previously carried out, ref. AMK 78-13

LEARJET AMK 79-09

CAB.DOOR MECHANISM (AD800709) (AD800709)

FAA, U.S AD 80-07-09 LFV LVA1613 30-jun-79 17-nov-80

LEARJET AMK 79-10

ENGINE FUEL TUBE 30-jun-79 12-jul-80

LEARJET AMK 79-11

AILERON DRAIN 30-jun-79 17-nov-80

LEARJET AMK 80-

01

B RUDDER PEDAL 30-jun-80 B 03-aug-81

LEARJET AMK 80-

06

A ENG.MOUNT (AD801711) (AD801711) 30-jun-80 A 15-apr-81

LEARJET AMK 80-

07

MOTIVE FLOW VALVE (AD801909)

(AD801909)

FAA, U.S AD 80-19-09 Rev 1 LFV

LVA1625 Rev A

30-jun-80 24-dec-80

LEARJET AMK 80-

17

1 Installation of Current Limiter

Warning

28-jun-10 A 04-jul-08 Starter engage lamps, moved to opt. position

LEARJET AMK 81-

17

HOR.STAB. HINGE PIN 30-jun-81 23-mar-86


2012-12-06


38(195)

LEARJET AMK 83-

03

AILERON TRIM TAB BALANCE WEIGHT

(AD84190 (AD84190

30-jun-83 14-jun-85

LEARJET AMK 83-

05

WING STALL STRIP (AD851604)

(AD851604)

FAA, U.S AD 85-16-04 FAA, U.S AD

96-19-13

30-jun-83 22-jan-86 N/A due to config. (STC SA766NW never been installed).

LEARJET AMK 84-

08

SPOILER SYSTEM 30-jun-84 23-mar-86

LEARJET AMK 85-01

A POWER DIST. 30-jun-85 A 23-mar-86

LEARJET AMK 86-

04

WING FLAP SECTOR (AD862205)

(AD862205)

FAA, U.S AD 86-22-05 30-jun-86 03-nov-86

LEARJET AMK 90-

05

SYSTEM TUBE (AD921912)

(AD921912)

FAA, U.S AD 92-19-12 09-Oct-

1991

25-jan-93

LEARJET AW 32-

021

Goodyear Flight Eagle Tire Tread

Separat

FAA, U.S AD 2001-07-11 05-feb-01 17-May-2001 N/A by s/n on tire.

LEARJET SB 00-01 Inspection/Replacement of cables 27-feb-01 26-mar-01

LEARJET SB 05-01 FIRE EXT. BOTTLE (HYDROST.) 18-nov-92 18-nov-92

LEARJET SB 11-02 AIRSPEED LIMIT PLACARDS 06-dec-76 02-jan-77

LEARJET SB 11-03 A AIRSPEED LIMIT PLACARDS AD841906 FAA, U.S AD 80-17-11 18-sep-80 A 23-sep-80

LEARJET SB 11-04 WASTE DISP.REC. PLACARDS

AD740809

18-dec-81 25-jul-91 N/A due to model and s/n.

LEARJET SB 11-05 CREW SEAT BELT PLACARDS 31-aug-83 23-Oct-1983

LEARJET SB 11-06 BATTERY PLACARDS 21-jul-87 25-jul-91 N/A due to SB32-04 is carried out.

LEARJET SB 11-07 ID PLATE (O) 06-nov-92 23-jul-93

LEARJET SB 11-10 Repl.of Fuel Servicing Placards 17-dec-01 06-feb-04

LEARJET SB 21-02 Cabin Air Distribution 02-May-

1977

25-jul-91 N/A. Optional.

LEARJET SB 21-03 CONDENSER FAN ASSY. AD781603 FAA, U.S AD 78-16-03 12-jul-78 30-jul-78

LEARJET SB 21-04 Inst. of Refrigeration

Syst.Warn.Placard

22-feb-79 23-May-1979

LEARJET SB 21-05 CABIN PRES. SAFETY VALVE 18-dec-79 05-May-1980

LEARJET SB 21-06 Insp.of Air Distr.Sleeves & Clamps-

Tailc

23-sep-80 16-nov-80

LEARJET SB 21-07 CABIN PRES. SAFETY VALVE

(CHANGED) Garrett SB 5-2290

28-Oct-

1980

29-jan-81


2012-12-06


39(195)

LEARJET SB 21-14 1 OUTFLOW VALVE SAFETY VALVE (R) 03-jan-95 1 22-dec-95 Superseded by SB 21-19.

LEARJET SB 21-15 2 Repl. of Refrig.Syst. Press Switch 22-jul-05 2 11-Oct-2005 N/A to Keith R34.

LEARJET SB 21-18 3 Imp.W-shield Aux.Defog & Aux.Crew Heat

11-aug-08 3 04-nov-08 N/A N/A due to AAK86-1 not incorporated

LEARJET SB 21-19 Insp.of Cabin Press.Outflow & Safety Vlv 130406-21-A4011 R2,102850-21-A4021 R2

FAA, U.S AD 95-20-03 03-jan-95 22-dec-95

LEARJET SB 21-24 1 Repl.of Aux.Cabin Heater Wiring FAA, U.S AD 98-06-28 13-aug-96 1 09-dec-08 N/A due to s/n

LEARJET SB 21-25 3 Inst.of Improved Refrigeration

Comp.Asse

12-nov-07 2 06-feb-08 N/A Due to Keith Aircondition System TR-134 Installed

LEARJET SB 21-26 5 Mod.of Auxiliary Cabin Heather 16-May-

2007

5 05-Mar-2012

LEARJET SB 22-02 Sec.Yaw Damper Servo Cable Clamp Bolt

06-sep-78 10-mar-78

LEARJET SB 22-03 Repl.of Yaw Damper Servo Sector Bolts

02-feb-79 03-jun-79

LEARJET SB 22-04 C Mod. of Mach Trim Computer J.E.T SB 501-1132-9E, -10B, -11

25-mar-80 C 01-sep-91 N/A

LEARJET SB 22-05 Mod.of FC-530/-535 Autopilot Computer

05-jan-87 25-jul-91 N/A N/A due to A/P model

LEARJET SB 22-07 3 Inst.of Autopilot Accelerometer Monitor

11-jun-07 2 29-May-2007 N/A AAK 83-2 not complied with.

LEARJET SB 23-03 2 Increased FOD Protection-Installation of Antenna Protection.

09-jul-01 2 11-jan-06 Previous revision carried out.

LEARJET SB 24-03 AC Inverter Excitation & Control

Check

FAA, U.S AD 76-18-07 09-aug-76 29-sep-76

LEARJET SB 24-04 A Reloc.of AC

Second.Inv.Ground.Connection

01-jun-77 A 24-dec-77

LEARJET SB 24-05 Repl.of Generator Bearings Bendix SB

R-358 & Suppl No.1

02-May-

1978

27-jul-78

LEARJET SB 24-06 Insp.of Battery Vents for Obstruction 29-sep-80 25-jul-91 N/A Found not applicable due to incorporation of SB 24-

15.

LEARJET SB 24-07 Current Limiter Box Moisture Proofing 15-jan-81 25-jul-91

LEARJET SB 24-08 Insp.of No.4 Gauge Electrical Cables 11-May-

1982

25-jul-91

LEARJET SB 24-09 Insp.Fuses for Proper Prot.Covering &

PN

19-apr-83 25-jul-91


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LEARJET SB 24-10 Reloc.of Battery Vent Inlet Fitting

AD860505

FAA, U.S AD 86-05-05 Rev 1 18-Jul-

1985

18-jun-86

LEARJET SB 24-11 Add.of Ret.for Gen.Warn.Ctrl

Box.Connect

01-nov-90 25-jul-91

LEARJET SB 24-15 1 Inst.of Concorde Sealed Lead-Acid

Batt.

24-mar-08 1 04-sep-08 PCW

LEARJET SB 25-03 Insp.of Drag Chute Mechanism Bolt 10-nov-80 09-jun-81

LEARJET SB 25-04 A Insp.of Drag Chute Mech.for Proper

Clear

11-nov-81 A 15-aug-82

LEARJET SB 25-06 Insp.Drag Chute Canister Lid Latch

Screw

19-feb-87 25-jul-91

LEARJET SB 26-02 A Verif.& Ident.of Eng.Fire Ext.Bottl.Wire

30-apr-91 A 25-jul-91

LEARJET SB 26-03 2 Repl. of Fire extinguishing Bottle Ass. 20-aug-07 2 21-jan-08 Carried out at L/H side

LEARJET SB 26-04 1 Engine Fire Element Insp./repl. 11-aug-08 1 04-nov-08 N/A N/A by s/n on elements

LEARJET SB 27-05 Stall Warn.Computer Plug &

Receptacle ID

13-sep-76 31-dec-76

LEARJET SB 27-06 Insp.of Alt.Pressure Switch Wiring 06-May-

1977

27-dec-77

LEARJET SB 27-07 Mod.of Spoileron Computer Assembly

J.E.T SB 501-1133-4

01-Oct-

1977

12-mar-85

LEARJET SB 27-08 Wiring of Pilot & Copilot Cntrl Wheel.. 24-May-

1978

13-dec-81

LEARJET SB 27-09 Insp.of Wing Flap Actuators 19-dec-78 25-jul-91

LEARJET SB 27-10 Rework of Pilot/Copil.Ctrl Wheel Trim

..

19-apr-79 01-jul-80

LEARJET SB 27-11 Insp.of Aileron for Drain Holes 06-nov-79 27-dec-79

LEARJET SB 27-12 B Stall Warn.Accelerometer Op.Check FAA, U.S AD 82-01-05 Rev 2 LFV

LVA1912

25-sep-81 B 12-jun-06 Överförd till A1 phase insp. Ref. Learjet Chpt.5

rev.74 och FAA AMOC från 2005-03-24

LEARJET SB 27-14 Insp.of Welds on Rudder Pedal

Supp.Assy

08-sep-83 27-mar-84

LEARJET SB 27-16 Insp.Flap Attach.Fittings for Cracks 27-May-

1986

03-nov-86

LEARJET SB 27-24 Insp.of Ail.& Rudder Ctrl Cable Assy Ter

08-nov-93 01-dec-93

LEARJET SB 27-33 Removal of Sealant from Aileron Rib 27-May-1997

19-feb-98


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LEARJET SB 27-35 4 Inst.of Secondary Locking Feature 15-aug-03 4 03-nov-03 Previous rev. carried out.

LEARJET SB 27-36 Replacement of Spolier Actuator FAA, U.S AD 99-23-19 14-dec-98 09-dec-08 N/A due to s/n

LEARJET SB 27-40 6 Insp/Inst. of Flap Structure Components

16-aug-10 6 10-Nov-2011 PCW Previous revision carried out

LEARJET SB 27-43 Recalibration rosemount 19-jan-05 17-mar-05 N/A due to STC ST00321WI-D not complied with.

LEARJET SB 27-45 1 Insp. Spoiler panels 29-Mar-2012


Insp.of Tip Tank Elect.Conduit for Damag

20-feb-76 03-jan-77

LEARJET SB 28-04 Reloc.of Fuel Probes on Wing Tank Access

01-nov-77 20-sep-79

LEARJET SB 28-05

INAKTIV

Op.check of Fuel Jettison Valves 14-feb-80 07-sep-80

LEARJET SB 28-06 Insp.of Rec.for Field Rep.of Mot.Flow

Vl

21-aug-80 24-sep-80

LEARJET SB 28-08 Insp.of Motive Flow Vlv Shroud Cover 27-aug-90 09-jan-91

LEARJET SB 28-10 Inspection of Tip Tank Flapper Valves FAA, U.S AD 2005-16-09 FAA, U.S AD 95-25-03

06-Oct-1995

14-sep-05 Flapper p/n 2323006-802 previously installed. No further action req.

LEARJET SB 28-11 5 Inst.of Standby Fuel Pump Annunciators

FAA, U.S AD 2007-04-18 28-sep-09 5 26-feb-10 Rev. 1-4 PCW. AFM cheched for Change 14

LEARJET SB 28-14 2 Repl.of Tip Tank Flapper Valves 09-May-2001

2 31-aug-01 SB previuos installed.

LEARJET SB 28-18 Insp./Repl. of Fuel Filter Elements 24-aug-09 30-Oct-2009 N/A due to filter p/n

LEARJET SB 29-01 1 Insp.RH Eng.Hydr.Press.Line for Interfer

FAA, U.S AD 83-08-03 10-sep-96 1 19-dec-08 due to remod. hyd.syst.

LEARJET SB 29-02 Insp.LH Eng.Hydr.Lines for Interference

FAA, U.S AD 84-20-06 15-jun-83 14-aug-83

LEARJET SB 29-05 Repl.of Hydr.Reservoir Sight Glass Assy

07-Oct-1992

23-jul-93 N/A

LEARJET SB 30-10 1 Repl. of Wing Anti-Ice Transverse Duct 12-feb-99 1 08-dec-99

LEARJET SB 30-11 3 Inst.of High Current Capacity Wire 05-May-2008

3 04-sep-08 PCW

LEARJET SB 31-01 Repl.of Oil Press.Annunciator Cap Assy

26-Oct-1992

01-dec-93

LEARJET SB 32-03 Insp.of LG Brake & Torque Link for Inter

25-aug-81 25-jul-91


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LEARJET SB 32-04 Repl.of LG Hydraulic Selector Valve 23-jan-89 09-jan-91

LEARJET SB 32-07 1 Inst.of MLG Lower Torque Arms 10-nov-95 1 31-Oct-2003

LEARJET SB 32-18 Inst.of Main Landing Gear Wheel Screens

19-jan-99 15-mar-99 N/A. Affected Wheel Assy not installed.

LEARJET SB 32-20 Repl.of Landing Gear Shuttle Valve 09-mar-00 30-jun-00 N/A Found N/A to Part Number.

LEARJET SB 32-21 Repl.of Brake Valve Adjustment Screw 01-May-2000

26-mar-01

LEARJET SB 32-23 1 Mod landing gear squat switch wiring 09-apr-07 1 29-May-2007 N/A Previously carried out

LEARJET SB 32-26 Insp/Repl of the Nose Gear Wheel Assy

18-jan-10 10-May-2010 N/A by s/n

LEARJET SB 32-27 IR Sealant on Anti-Skid Solnoid 14-Jun-2011

LEARJET SB 33-01 Add.of Drain Holes in Tip Tank Nose Cone

03-jan-77 11-feb-77

LEARJET SB 33-03 Insp.& Mod. of LH Fwd Cabinet Light Assy

24-apr-85 25-jul-91 N/A N/A due to interior config.

LEARJET SB 33-05 A Deactiv.of Fwd Cabinet & Overhead Light. AD901406

FAA, U.S AD 91-03-08 21-dec-90 A 19-dec-08

LEARJET SB 33-06 A Activ.of Fwd Cabinet & Overhead Fluore..

12-apr-91 A 26-feb-09

LEARJET SB 34-04 Insp.of Static Ports 11-jun-82 25-jul-91

LEARJET SB 35-01 Insp.of Oxygen Mask Microphone Jack Wiri

09-sep-77 25-jul-91

LEARJET SB 35-04 Replacarding Oxygen Bottle Shutoff Valve

27-feb-04 04-aug-04 Placards installed.

LEARJET SB 36-02 A Insp.& Repl.of Eng.Bleed Air Flex Tube..

25-May-1978

A 01-sep-91

LEARJET SB 36-03 Repl Air Bottle & Weight-Balance Change

14-dec-09 11-mar-10 Due to weighing after installation of bottle p/n 6600194-6

LEARJET SB 51-01 Insp.Baggage Comp.Struct. for

Corrosion AD 84-12-03

18-jul-85 06-sep-85

LEARJET SB 51-03 Insp.of Forward Engine Beam Shear

Web.

FAA, U.S AD 2004-03-08 01-feb-01 1200H 06-sep-01 N/A N/A due to SB 51-04 performed.

LEARJET SB 51-04 5 Rep.of Forward Engine Beam Shear

Web

FAA, U.S AD 2004-03-08 12-Oct-

2009

5 11-mar-10 No rework required

LEARJET SB 51-4 3 20-jan-05 No rework req.


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LEARJET SB 52-02 Adj.of Lwr Cabin Door Hok Act.Toggle

Sw.

09-aug-77 14-jun-85

LEARJET SB 52-04 Mod.of Access Door Lock Assemblies 16-apr-79 25-jul-91 N/A Found N/A. No locks installed.

LEARJET SB 52-05 Insp.of Cabin Int.Liner-Areas Of

Emerg..

04-nov-80 25-jul-91

LEARJET SB 52-06 Mod.of Lwr Cabin Door Hook

Mechanism

18-dec-92 01-dec-93

LEARJET SB 52-10 1 Repl.of Upper Cabin Door Torsion Bar

Arm

03-jun-99 1 20-sep-99 N/A. 24 inch door not installed.

LEARJET SB 53-01 Inst.of Rivets at Fwd Eng.Beam &

Frame24

27-apr-77 01-sep-91 N/A

LEARJET SB 53-07 Inspect for Tailcone Drains 18-dec-92 01-dec-93

LEARJET SB 53-08 Inst.of Nutplates on Circ.Br.Panel

Suppo

14-feb-94 15-dec-94

LEARJET SB 53-10 1 Repl.of LowerStinger & Ventral Fin

Skin

17-mar-08 1 14-May-2008 N/A Due to Avcon Fins STC ST00432WI

LEARJET SB 53-11 3 Mod.of Tailcone Ballast Weight

Installat

01-jun-09 3 08-jan-10 Ballast not/never installed

LEARJET SB 53-13 Insp. Intern. baggage comp. floor splice

16-jan-06 08-mar-06 N/A Due to S/N

LEARJET SB 54-01 Insp.for Silicon Firesleeve-Start&Gen Ca

11-jun-82 25-jul-91

LEARJET SB 54-03 Insp/Firewall Sealing Modification 16-mar-01 17-apr-07 L/H side carried out

LEARJET SB 54-04 Insp/Repl.of Upper and Lower Pylon Skins

08-aug-01 22-mar-02 N/A by s/n on aircraft.

LEARJET SB 55-01 Insp.Horiz.Stab.Hinge Assy for Cracks 16-aug-91 16-aug-91 N/A No Thrust Reversers installed.

LEARJET SB 55-04 2 Inst.of Doublers on Horiz.Stabili.Skin 23-feb-09 2 10-jun-09 PCW

LEARJET SB 55-05 Imp.of Horiz.Stabilizer Actuator

Access

16-jan-98 30-Oct-1998

LEARJET SB 55-06 Mod.of Navigation Light Wiring

Conduit

30-aug-04 30-nov-04

LEARJET SB 71-01 Insp.for Interf.between LH Eng Starter

&

08-sep-76 02-jan-77

LEARJET SB 71-02 Eng.Firewall Sealing at Feed-Thru Condui

13-May-1982

25-jul-91

LEARJET SB 71-03 1 Insp.of Fwd Eng.Mounts for Cracks FAA, U.S AD 87-02-06 10-feb-95 1 27-jan-97


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LEARJET SB 71-05 2 Repl.of Fwd Eng.Mount Bolts 18-jun-93 2 10-jan-95 Bolt replaced L/H side w/o C00454 1997-01-21.

LEARJET SB 76-01 B Insp.of Eng. I.T.T. Cable Connectors 07-nov-83 B 27-sep-84

LEARJET SB 80-02 A Repl.of Starter Rly Cover & Magnetic Cor Bendix SB R-352A, R-355

04-mar-77 A 18-sep-79

LEARJET SB A27-42 Insp/Repl.of Aileron Ctrl Cables 23-dec-02 11-jan-03 1ea: cable effective by cal.time, inspected OK.

LEARJET SB A32-15 1 Insp.of Landing Gear Actuator Pistons 21-apr-97 1 19-feb-98

LEARJET SSK 981 Repl. of Spoiler Act. Support Bracket 19-dec-86 27-mar-01

LEARJET SSK 993 2 Repl. of Landing Gear Wheel Bearings 21-jan-91 2 08-jan-98

LFV,

Luftfartsverket

LFV LVA 1613 Modifiering av övre kabindörr LEARJET AMK79-09 27-May-

1980

17-nov-80

LFV LVA 1625 A Till,gg i flyghandbok. T,thetskontroll FAA, U.S AD 80-19-09 Rev 1

LEARJET AMK80-07

23-jun-80 A 24-dec-80

LFV LVA 1748 Revision av Flyghandbok.

Br,nslem,ngd

FAA, U.S AD 81-13-07 24-aug-81 10-aug-81

LFV LVA 1912 Periodisk kontroll av Stallvarning. FAA, U.S AD 82-01-05 Rev 2 LEARJET SB 27-12 Rev B

10-nov-83 12-jun-06 Överförd till A1 phase insp. Ref. Learjet Chpt.5 rev.74 och FAA AMOC från 2005-03-24

LFV LVD 1635 A Revision Flyghandbok/kontr. A/P & mod.

FAA, U.S AD 80-19-11 Rev 1 15-jul-85 A 28-sep-09 PCW Ref. FAA AD 80-19-11 R1

LFV LVD 2034 Reducering av MMO FAA, U.S AD 85-16-04 30-aug-85 22-jan-86 N/A due to config. (STC SA766NW never been installed).

LFV LVD 2046 Kontroll av batterihållare FAA, U.S AD 86-05-05 Rev 1 25-

Nov-1985

18-jun-86

LFV LVD 2352 Shoulder Harness Inst. FAA AC 43-13

CHPT 9

23-May-

1991

25-jul-91 checked OK.

LFV LVD 2853 Periodisk funktionskontroll av

nödutgång

23-mar-98 02-dec-10

LFV LVD 3148 Modif. Transponder kontrollpanel 17-aug-01 12-feb-09 N/A due to p/n

NYGE, Saab

Aerotech Aircraft

Services

NYGE SB 08-06-34- A EGPWS System Provision for Inhibit 30-nov-09 A 04-mar-10


2012-12-06


45(195)

03 Unit)

NYGE TDM 02-20 GMS Prototyp 27-aug-02 05-jun-04 utf. i samband med Kapsel-mod.

NYGE TDM 02-25 Installation Underving-kanaler 16-Oct-2002

10-nov-03 LFV app.No: M21/02 revision 1.

NYGE TDM 02-26 Box 3 Installation 01-nov-02 29-sep-03 Approved in accordance with EASA 2004-11267 and with LFV AFMS S04/89 R2.

NYGE TDM 02-28 Utv. Framtagning mod.balkar LR-35 18-nov-02 10-nov-03

NYGE TDM 03-03 B Operators Console L35A 02-apr-07 B 26-feb-08 only updated to rev.B

NYGE TDM 03-07 Alkan Fairings (mod.) 27-feb-03 10-nov-03 Approved by EASA no. 235 in accordance with LFV Mod. Cert. No. M29/03.

NYGE TDM 03-17 ACAS Installation 06-May-

2003

30-nov-04 Approved i.a.w. EASA Doc. No: STC S.A.00255.

NYGE TDM 03-19 Mission Inverter Modif. 20-nov-03 05-nov-03 Approved in accordance with LFV M37/03 and EASA

1985.

NYGE TDM 03-23 U95 Installation L35A 10-sep-03 D 10-mar-06 Rev.D updated

NYGE TDM 04-03 D Astor L35A 16-jan-04 D 21-Nov-2012

NYGE TDM 04-06 C Darts System L35A 05-dec-06 01-jan-06 Approved in accordance with DOA 21J.108.04-06.

NYGE TDM 05-06 Removal of Reflector System 30-May-2005

02-jun-06 Approved i.a.w. DOA 21J.108.05-06

NYGE TDM 05-15 Install. Jumpseat Intercom 18-jul-05 23-nov-06 Approved in accordance with DOA 21J.108.05-15A

NYGE TDM 05-19 Install. GPS Map and GP&C

Transponder

08-sep-05 23-nov-06 Approved in accordance with DOA

NYGE TDM 05-20 Install. Mission Equip. new OP-

Console

13-sep-05 23-nov-06 Approved in accordance with DOA 21J.108.05-20A

NYGE TDM 05-26 Install. Cabin Side Wall Cable Channel 20-Oct-

2005

23-nov-06 Approved in accordance with DOA 21J.108.05-26A

NYGE TDM 06-22 Re-mod. Hydraulic system 05-May-

2006

07-nov-06

NYGE TDM 06-36 A A100 (to carry on L35A) 23-apr-07 A 25-feb-08

NYGE TDM 08-02 C Enhanced Surveillance L35A 09-mar-10 C 28-jul-09 Original compliance to rev A of TDM. TDM rev B and C does not affect previous compliance.

NYGE TDM 08-06 C EGPWS MK.8 & Mission Inhibit System 05-mar-10 C 04-jul-08 Original compliance with rev A. Rev B and C does not affect previous compliance.

NYGE TDM 08-07 E LR35A GPS-Map Display 12-apr-10 E 28-Aug-2012 Compliance was IAW TDM rev A. Previous compliance not affected by rev D.


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NYGE TDM 08-09 C Install Termination resistor C 01-09-2012

NYGE TDM 08-13 A Barlast DARTS L35A 10-mar-08 A 10-mar-08

NYGE TDM 08-17 C ELT 406 L35A 04-jul-08 C 04-jul-08 Original compliance with TDM rev A. Rev B and C does not affect previous complaiance.

NYGE TDM 08-26 A Mission Antenna Adapter 28-Oct-2008

A 22-dec-08

NYGE TDM 09-30 E LR35A Removable Hard Disk Drives 30-apr-10 E 04-July-2012 Original compliance was i.a.w TDM rev A. Rev B

does not affect previous installation.

NYGE TDM 10-04 B Overload Sensing Control 02-jun-10 B 28-Sep-2012

NYGE TDM 10-27 A LR35A U95-D2 22-apr-10 A 15-jun-10

NYGE TDM 10-31 A Overload Sensing Control Provisions 01-jul-10 A 06-jul-10

NYGE TDM 12-22 A L35A Move mission inverter A 28-Sep-2012

NYGE TDM 12-23 A Installation laser prismor L35 A 28-Sep-2012

NYGE TDM 95-01 Installation Intercom 10-jan-95 16-jan-95

NYGE TDM 95-03 Modifiering Transponder-system 06-feb-95 16-jan-95

NYGE TDM 96-04 Miss-rack,GPS-antenn,CVR,inverter m.m.

12-feb-96 15-mar-96

NYGE TDM 97-01 TAPS 20-feb-97 01-jan-98

NYGE TDM 98-06 Astor L35A 09-mar-98 27-apr-98

NYGE TDM 98-12 Installation BRNAV L35A 26-jun-98 31-May-1998

NYGE TDM 98-13 Kontrollprogram SE-DHP 26-jun-98 15-aug-98

ROCKWELL,

Rockwell Collins

U.K.Ltd

ROCKWELL SIL 07-1

Reply Inhibition On The Ground EASA AD 2009-0097 Rev IR 25-May-2007

28-jul-09


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2 GFE Aircraft Mitsubishi MU-2

2.1 Mitsubishi MU-2 Aircraft Maintenance Program

2.1.1 Comprehensive description of Mitsubishi Maintenance Requirements Manual (MR-0178-2):

The maintenance is (according to Mitsubishi Maintenance Requirements Manual MR-0178-

2.) divided into 100 hours intervals between each periodic inspection.

Some inspections have both flight time and calendar time limitations; they must be complied

with when the first limitation becomes due. For maintenance planning purpose, a "Window

For Compliance" can be established for each inspection. An inspection accomplished within

the window, will be considered as if it was completed at the flight time or calendar time due.

It is not allowed to accumulate the time between inspections.

Inspection list according to Mitsubishi Maintenance Requirements manual MR-0178-2:

• 100 Hrs/12 Month



• 1000 Hrs

• 1200 Hrs

• 1800 Hrs

• 2000 Hrs

• 1 Year

• 2 Year

• 10 Year

• Detailed and General Engine Inspection

2.1.2 Modifications that affects the maintenance program If no individual reg. numbers are mentioned, the information applies for all six individuals.

• The fuselage is modified with a hatch, which enables deployment and changing Soft

Sleeve Targets during the flight.

• An inboard hydraulic driven winch - Air Target MBV-7 Mk II - is installed. (SE-

GHD, SE-IOV and SE-IUA).

• An aircraft hydraulic system, which consists of a hydraulic oil tank installed in the

centre wing leading edge, an engine driven hydraulic pump installed on the left engine

and a shut off valve installed in the left wing leading edge, has been installed in order

to supply the inboard winch with necessary hydraulic power for operation. (SE-GHD,

SE-IOV and SE-IUA).

• One retractable launcher arm for sleeve targets is installed under the fuselage. (SE-

GHD, SE-IOV and SE-IUA).

• A set of Laser Reflector Prisms is installed on the fuselage. (SE-GHD, SE-IOV and

SE-IUA)


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• The wings have been modified with hard points to carry external under-wing stores

• The nose radome and wing tip tanks have been modified with radome covering

antennas for the inboard ECM-system ASTOR. (SE-GHA, SE-GHB and SE-GHF).

• To supply the ECM equipment, a 3-face AC, 3kVA inverter system has been installed

in the inboard aft baggage area.

• An operator console is installed in the cabin with equipment to operate the winch and

ECM units, including a set of surveillance equipment as TV-camera, mirrors etc.

• On airplanes modified with ECM System, the R/H steering wheel is removed by

installation of operator’s work station. (SE-GHA, SE-GHB, SE-GHD and SE-GHF).

• AMOC Approval: EASA.A.AMOC.01276. Exemption from installation of

Rosemount ice-detector in accordance with JCAB TCD4529-97 and MHI SB217.

2.1.3 Maintenance Documentation Maintenance of the aircraft is conducted according to the following documentation:

• Mitsubishi Maintenance Requirement Manual MR-0178-2

• Honeywell MM 72-01-32 applicable to TPE331-6-252M

• Honeywell SB TPE331-72-0404 applicable to TPE331-6-252M

• Honeywell SB TPE331-72-0019

• Hartzell SL 61-61Y

2.1.4 Guiding documents to be used during maintenance:

• Mitsubishi Maintenance Manual YET 68035



• Mitsubishi Illustrated Parts Catalogue YET 68036B

• Mitsubishi Illustrated Parts Catalogue YET 72092A

• Mitsubishi Illustrated Parts Catalogue YET 74134A

• Mitsubishi Structural Repair Manual YET 72035A

• Mitsubishi Airplane Flight Manual

• Mitsubishi Pilot Operating Manual

• Mitsubishi Service Bulletins, -Recommendations, -Letters

• Honeywell TPE331 Service Bulletins. -Recommendations. –Letters

• Saab AB TVO

• Saab AB TDM

2.1.5 Maintenance Tasks related to changes The following maintenance tasks are not included in the aircraft manufactures’ maintenance

manual. The tasks need to be included in the operators AMP:

• Launcher Arm 3 months inspection

• Launcher Arm 100 hours inspection

• Provisions for Special Mission. 1 year inspection

• Special Operational Fatigue Inspection 1000 hours


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2.1.6 Guiding documents issued by the Agency and Aviation Authority for both Airframe and Engines:

• Requirements in BCL-M4.3

• FAA Airworthiness Directives

• JCAB Airworthiness Directives

• EASA Airworthiness Directives

• LVD Swedish Airworthiness Directives.


2012-12-06


50(195)

2.2 GFE Aircraft Mitsubishi MU-2 SE-GHA


Number:


total Hours:

Total

Landing

Cycles:

Date

Reference:

MU-2B-20 283 SE-GHA 10586 5954 2012-11-23

2.2.2 Engines Type: Honeywell TPE331-6-252M

Serial

Number:

Total Hours

Since New:

Total

Cycles

Since New:

Hours remaining to

overhaul/HSI/GBl:

Left Engine P27094 8140 10755 3330/923/2723

Right Engine P20322 3718 4975 1693/1073/2873

2.2.3 Propeller Type Number: Serial Number: Overhaul Due Date:

Left Propeller HC-B3TN-5E BVA 6125 2014-12-16

Right Propeller HC-B3TN-5E BVA 6718 2015-11-15


Autopilot & Flight Director Century IV

COM/NAV/GPS 1 Garmin GNS 530


Audiopanel Bendix/King KMA-24H-70

MKR Bendix/King KR-21

DME Bendix/King KDM-706

ADF Bendix/King KDF-806

XPDR 1 Garmin GTX 330D Mode S EHS

XPDR 2 Garmin GTX 330 *) Mode S EHS

RDR ALT Bendix/King KRA-10A


Airspeed Indicator LH / RH Aerosonic 20040-161 / 20040-

0186

Altimeter LH United Instr. Inc. 5934 PAD-1

Altimeter incl. encoder RH United Instr. Inc. 5035P-P40

Altitude Reporter Narco AR 850

Altitude Alerter Aero Mechanism AM 275C

Vertical Speed Indicator LH Aerosonic RC-60-MS-10-3

Attitude Gyro & Flight Director Ind. Century 52C77


2012-12-06


51(195)

LH

Attitude Gyro Ind. RH AIM 504-0006-914

Turn & Bank Ind. LH R.C Allen A5930-02

Horizontal Situation Indicator LH Bendix/King KPI-553A

DG-Gyro Sperry C-14A

Directional Gyro RMI Ind. LH AIM 254-1D

CDI Indicator Garmin GI-106A

*) XPDR 2 without diversity configuration



VHF/UHF COM 1 & 2 FR31

GPS MAP


Laser Prism

MIL-STD-1553 Bus LH Wing Pylon

Wing Pylon


EW system


ADRIAN Pod mounted system LH and RH Wing

Pylon

U95 N Pod mounted system LH Wing Pylon

A100 Pod mounted system LH Wing Pylon


DARTS Pod mounted system LH Wing Pylon

Chaff Dispenser

BOX 3 Pod mounted system LH and RH Wing

Pylon


System:


Adrian C & S, U95-N, A100,

DARTS and BOX 3 General Signal Harness AWG22 shielded x 44

General Signal Harness AWG22 shielded x 50

U95-N and A100 MIL-STD-1553B Data

Bus

Triax Cable x 1

U95-N, A100 and DARTS AC Power

115/200VAC 400 Hz 3-

Phase 3 x 10 A

AWG 12 x 4

twisted

AWG 16 x 2

AWG 20 x 2 Adrian C & S and BOX 3 DC Power 28 VDC 200

A

DC Power 28 VDC 200

A

AWG 2 x 2


2012-12-06


52(195)

Adrian C & S Coax Cable 1 x 50 Ω Coax Cable 1 x 50 Ω Prepared installation Ethernet LAN Cable

2.2.7 Antenna Layout


2012-12-06


53(195)


rd 2012.

Description Maint. Ref C/Out date C/Out Hrs Due Hrs Due date

Aircraft SE-GHA

Vingstudie MU-2 AMP 2011-09-19 10470,92 11500

100 Hour Inspection AMP 2012-09-14 10568,72 10670,92 2013-09-14



1000 Hour Inspection AMP 2011-09-19 10470,92 11500

1200 Hour Inspection AMP 2012-09-25 10568,72 11768,72

1800 Hour Inspection AMP 2005-02-04 9700 11500


1 Year Inspection AMP 2012-09-18 10568,72 2013-10-04




Engine Assembly (Overhaul) AMP 12280,1 1693,72

Engine Hot Section Inspection AMP 11660,1 1073,72

Engine Gearbox Inspection AMP 13460,1 2873,72

Engine S/N P-27094




Propeller L/H O/H AMP 2009-12-17 13394,52 2014-12-16

Propeller R/H O/H AMP 2010-11-16 13382,5 2015-11-15


2012-12-06


54(195)

2.2.9 Implemented Changes Abbreviations:

Abbr. Issued by Explanation

AAK Learjet Aircraft Accessory Kit

AD EASA, FAA, Finnish CA,

JCAB

Airwortness Directive

AMK Learjet Aircraft Mod Kit

AW Learjet Accessory Wire

LVA LFV Luftvärdighetsanvisning

LVD LFV Luftvärdighetsdirektiv

MSB Mitsubishi Mitsubishi. SB

MSR Mitsubishi Mitsubishi SR

SA Hartzell Service advisory

SB Keith, Learjet, Nyge,

Century, Garrett, MAI,

Hartzell, Mitsubishi,

Narco

Service Bullentin

SI Hartzell Service information

SIB EASA Service information bullentin

SIL Rockwell Service information letter

SL Mitsubishi Service Letter

SN Mitsubishi Service news

SR Mitsubishi Service recomendation

SSB Nyge and Garmin Sofware SB

SSK Learjet Special Spares Kit

STC Avcon, Flight Int., Keith, Supplement Type Certificate


2012-12-06


55(195)

Mitsubishi

TDM Nyge Tekniskt Direktiv Materiel

TVO Nyge Teknisk Verkstad Order

Status date November 23rd

2012. SB/AD etc

Reference


CENTURY, Century Flight

Systems Inc.

CENTURY SB CSB-2005-01

Check for frayed Bridle Cable 21-feb-05 16-nov-10

EASA, European Aviation Safety Agency

EASA AD 2006-0265

Incorrect transponder altitude 30-aug-06 27-nov-09

EASA AD 2009-0251-E

Portable Fire Extinguishers-Ident/Repl

25-nov-09 07-May-2010

N/A by current P/N installed

EASA AD 2009-0262


EASA AD 2009-0278 FFE ASB26-115 Rev C 15-dec-09 07-May-2010


EASA AD 2009-0278


EASA AD 2009-0262 22-dec-09 07-May-2010


EASA AD 2010-0003


11-jan-10 R1 10-mar-10 N/A due to model

EASA AD 2012-0037

KIDDE GRAVINER HAND OPERATTED FIRE EXTINGUISHER

04-Oct-2012

EASA SIB 2008-

58R1

Channel Spacing Switching GARMIN SSB0844 Rev IR GARMIN

SSB0845 Rev IR

17-dec-08 21-sep-10 N/A by SSB 0845 incorporated

EASA SIB 2009-14 Upgrade to main unit/GPS software 24-jun-09 28-sep-09 N/A due to model


FAA, U.S AD 2000-09-15 FAA, U.S AD

2000-02-25

1 Flight in Icing Condition AFM De-icing

FINNISH AD M 2435/97 FINNISH AD M 2786/00 MAI SB 086/74-002 Rev A MAI

SB 093/22-009 MAI SB 096/30-004

07-jul-00 1 22-nov-01 Action not required due to s/n. N/A Due to paragraph b.


2012-12-06


56(195)

MITSUBISHI SB 226 Rev E MITSUBISHI SB

231 Rev B MITSUBISHI SB 232 Rev A

FAA, U.S AD 2003-

17-04

Windshield check FINNISH AD M 3076 LFV LVD2678 MAI SB

087/56-001 Rev B MITSUBISHI SB 224 Rev C

01-Oct-

2003

16-nov-10

FAA, U.S AD 2003-22-07

1 Forecast Icing Conditions FINNISH AD T5007/03 JCAB AD TCD-4753A-2004 MAI SN 071/00-006 Rev D MITSUBISHI SN 117 Rev D

16-apr-04 1 17-May-2004

inserted in AFM limitations

FAA, U.S AD 2005-14-12

Prop. mounting bolt insp. HARTZELL SB 61-279 ALERT Rev 4 29-jul-05 14-sep-05 Propellerbolts previously checked u/a

FAA, U.S AD 2005-18-20

Prop de-icer "FASTprop" 14-Oct-2005

12-Oct-2005

N/A Due to boots p/n

FAA, U.S AD 2006-13-15

Safety evaluation wing barrel nuts) MAI SB 103/57-004 Rev A MITSUBISHI SB 241 Rev A

11-aug-06 18-mar-03 c/o in conjunction with vingstudie

FAA, U.S AD 2006-15-07

Safety evaluation (feathering linkage)

MAI SB 090/76-003 MITSUBISHI SB 229 24-aug-06 24-aug-06 se Mitsubishi SB 229

FAA, U.S AD 2006-17-01

Detect & correct torque transducers MAI SB 095/77-002 MITSUBISHI SB 233 Rev B

22-sep-06 21-sep-06 PCW see MSB 233A

FAA, U.S AD 2006-

17-05

Adjust flight idle fuel flow setting MITSUBISHI SB 234 22-sep-06 16-nov-10

FAA, U.S AD 2007-

17-09

Reduce max deflect elev nose-down

trim

MITSUBISHI SB 216 MITSUBISHI SB 228 25-sep-07 11-sep-07 Previously carried out i.a.w. mentioned SB's.

FAA, U.S AD 71-

14-01

Fuel Tank Fungus Coating Peeling 01-May-1972 01-jan-96 N/A by s/n

FAA, U.S AD 74-

11-01

Windshield Outer Panes LFV LVA829 Rev A MITSUBISHI SB 163 Rev

B

30-jan-78 05-May-

1974

FAA, U.S AD 75-

16-13

Main Wing Flap JCAB AD TCD-1094A-76 LFV LVA1011 Rev

A MITSUBISHI SB 167 Rev D

05-aug-75 18-jan-77 Revision C PCW by Swedair.

FAA, U.S AD 75-16-20

Propeller Pitch Control Lever JCAB AD TCD-1188-75 LFV LVA1012 MITSUBISHI SB 168 Rev A

12-aug-75 20-jan-88

FAA, U.S AD 78-03-05

Cowling Latches JCAB AD TCD-1202-75 LFV LVA1014 Rev A MITSUBISHI SB 171 Rev B MITSUBISHI SB

180 Rev A

23-feb-78 18-jan-88

FAA, U.S AD 81-

06-01

1 Engine Aft Nacelles 01-apr-81 1 22-nov-97 Previously complied with

FAA, U.S AD 81-

25-04

1 Engine's Electrical wiring SB 036/71-

003A, SB 043/71-005

21-jan-82 1 02-dec-10 N/A N/A by model

FAA, U.S AD 82-

08-02

Electrical Wiring Inspection 15-apr-82 18-mar-82


2012-12-06


57(195)

FAA, U.S AD 83-

08-01

2 To preclude prop. attach bolt

failures

FINNISH AD M 1168/83 Rev 1 FINNISH AD

T5114/05 HARTZELL SI 140A Rev 9

28-apr-82 2 20-May-

2005

Ref. MU2B MM chap 13.4 when using bolts P/N B-

3339 only

FAA US AD 83-09-

02

Strobe Light Assemblies 16-Mar-

2012

FAA, U.S AD 84-

12-04

Torque of Air Tube Coupling Nuts SB

047/30-001, SB 196A

MAI SB 047/30-001 Rev A MITSUBISHI SB

196 Rev A

28-jun-84 31-jul-84

FAA, U.S AD 84-25-02

Elevator TrimTab Bracket Insp/Repl. SB 031/27-005 R1, SB 176E

MAI SB 031/27-005 Rev 1 MITSUBISHI SB 176 Rev E

18-dec-84 18-apr-85

FAA, U.S AD 86-

15-03

NLG Strut Assembley LFV LVA1546 MITSUBISHI SB 181 PART 2

Rev B

13-aug-86 15-jul-04 Found SB 181 part 2 PCW.

FAA, U.S AD 86-

20-01

To assure anti-ice capability of pitot

SB

LFV LVD2015 Rev B 06-Oct-

1986

07-feb-00

FAA, U.S AD 86-

26-02

To prevent engine flameout in an

iceing SB 74-0003, SR 040/74-001

GARRETT SB 74-0003 Rev 6 MAI SR

040/74-001 MITSUBISHI SB 226 Rev E

MITSUBISHI SR 066

31-dec-87 09-mar-09 see applicable engine for c/o

FAA, U.S AD 87-

04-03

Addit. Seal and Flap Flexible Shaft

Insp SB 051/27-007, SB 198

MAI SB 051/27-007 MITSUBISHI SB 198 07-mar-87 14-jun-85

FAA, U.S AD 87-12-02

Generator Shield Jumper Wires MITSUBISHI SB 201 Rev A 03-jul-87 17-May-1990

FAA, U.S AD 88-13-01

Bendix Autopilot Disengagement SB 066/22-006

LFV LVD2190 MAI SB 066/22-006 Rev A MITSUBISHI SB 206

11-jul-98 06-jun-89 N/A N/A due to Autopilot model

FAA, U.S AD 88-21-01

1 To minimize confusion in autopilot/manua SB 066/22-006

LFV LVD2206 MAI SB 066/22-006 Rev A 28-jan-89 1 25-Jan-2012

FAA, U.S AD 88-

23-01

To prevent flap control failure SB

067/27-008, SB 189B

LFV LVD2202 MAI SB 067/27-008 Rev A 04-dec-88 15-feb-95

FAA, U.S AD 93-

07-11

ELECTRIC TRIM SYSTEM SB 079/27-

010

LFV LVD2477 MAI SB 079/27-010 01-jun-93 27-mar-09 N/A by s/n

FAA, U.S AD 94-

04-16

Elevator trim tab mod. LFV LVD2537 MITSUBISHI SB 216 11-apr-94 31-mar-93

FAA, U.S AD 94-

11-04

Change of Flight Idle Blade Angel SB

016/61-001


FAA, U.S AD 96-

25-02

Cap. of the icing protection system FINNISH AD M 2423/97 JCAB AD TCD-

4552-96 LFV LVD2749

27-dec-96 13-feb-02

FAA, U.S AD 97-

04-13

Vent Check Valve Assy LFV LVD2769 16-apr-97 05-May-

1997

N/A N/A due to s/n.

FAA, U.S AD 97-

20-14 CNL

Icing related incidents/accidents 17-Oct-

1997

02-dec-98

FAA, U.S AD 97-

25-02

To prevent loss of airplane

ctrl/overspe

FINNISH AD M 2524/98 21-jan-98 03-dec-10 N/A AD superseeded by AD 2010-10-17


2012-12-06


58(195)

FAA, U.S AD 98-

20-39

Forward fitting bolt of wingtip tank

SB

LFV LVD2688 19-Oct-

1998

29-nov-96

FINNISH, Finnish Civil

Aviation Adm.

FINNISH AD M

1177/83

Kontroll av rören till strobe-kablarna MITSUBISHI SB 174 PART 1 Rev C 07-jul-83 16-nov-10

FINNISH AD M

2609/98

Justering av br,nslefl"de MHI SB

097/73-001, TCD-4890-98

JCAB AD TCD-4890-98 MAI SB 097/73-001 12-nov-99 16-nov-10

FINNISH AD M

3076

Kontroll av vindrutor och fönster FAA, U.S AD 2003-17-04 21-aug-03 16-nov-10

GARMIN, Garmin

GARMIN SSB 0844 Software Version 5.04 EASA SIB2008-58R1 19-May-

2010

A 14-nov-08

GARMIN SSB

0845

Software Version 6.04 EASA SIB2008-58R1 19-May-

2010

O 14-nov-08

GARRETT, AlliedSignal

Aerospace

GARRETT SB 74-

0003

6 Replace Ignition Unit AD 74-0003 FAA, U.S AD 86-26-02 25-mar-94 6 09-mar-09 see applicable engine for c/o

HARTZELL,

Hartzell Propeller

Inc.

HARTZELL SB 61-256

Propeller mounting bolt inspection MITSUBISHI SL 053/72-003 , MITSUBISHI SL 080

08-feb-02 06-jun-02

HARTZELL SB 61-279 ALERT

4 Prop. mounting bolt insp. FAA, U.S AD 2005-14-12 , MITSUBISHI SL 085

04-Oct-2005

4 14-nov-05 Propellerbolts previously checked u/a

HARTZELL SB A61-313

3 Counterweight Slug Bolt Inspection EASA SIB2008-88 , FAA, U.S AD 2009-10-14

15-jul-09 3 21-sep-10 N/A by SSB 0845 incorporated

HARTZELL SI 140A 9 Installation of Mounting Bolt FAA, U.S AD 83-08-01 Rev 2 , LFV LVA1424 Rev A

30-mar-05 9 13-mar-08 see previously revision

JCAB, Japan Civil Aviation


2012-12-06


59(195)

Bureau

JCAB AD TCD-0642-70

JCAB AD TCD-0518-68

AFM revision regarding fuel spec.

Rivet holes elevator hinge fitting

LFV LVA439 MITSUBISHI SB 112 Rev C 07-feb-70 18-jan-88

JCAB AD TCD-

0643-70

Adjustment of fuelquantitygauge LFV LVA438 MITSUBISHI SB 114 07-feb-70 15-Jul-2004

26-Mar-2009

N/A N/A by s/n. by s/n

JCAB AD TCD-0652-70

Insp. of NLG bolts LFV LVA456 MITSUBISHI SB 119 25-mar-70 26-mar-09 N/A by model

JCAB AD TCD-0653-70

Engine Nacelle Tail Area-Modification of

25-mar-70 26-mar-09 N/A by model

JCAB AD TCD-0660-70

Replacement of bearing in nosegearstrut

LFV LVA457 MITSUBISHI SB 123 01-May-1970

26-mar-09 N/A by s/n

JCAB AD TCD-

0730-1-72

Insp. and painting of maintanks LFV LVA543 Rev B MITSUBISHI SB 143 Rev

B

25-mar-72 14-jul-04 N/A N/A by s/n.

JCAB AD TCD-

0730-2-86

Insp. and painting of maintanks MITSUBISHI SB 143 Rev B 10-dec-86 26-mar-09 N/A by s/n

JCAB AD TCD-

0859-72

Mod. of electrical system LFV LVA645 MITSUBISHI SB 156 04-sep-72 09-Oct-

1972

N/A N/A due to s/n.

JCAB AD TCD-

0866-72

NLG gearbox and structure LFV LVA664 MITSUBISHI SB 155 09-Oct-

1972

31-dec-72 N/A N/A due to s/n.

JCAB AD TCD-

0947A-74

Kontr. & mod. av klaffdrivning LFV LVA828 Rev A MITSUBISHI SB 162 Rev

A

12-nov-74 18-jan-88 N/A N/A due to s/n.

JCAB AD TCD-0948A-1-78

Inspection of Windshields MITSUBISHI SB 163 Rev B 22-dec-78 26-mar-09

JCAB AD TCD-0948A-74

Inspektion av frontrutor LFV LVA829 Rev A MITSUBISHI SB 163 Rev B

07-Oct-1974

05-May-1974


Insp./repl. of elevator trim tab rod LFV LVA886 Rev A MITSUBISHI SB 176 Rev E

06-Oct-1976

18-apr-85

JCAB AD TCD-1001B-2-84

Replacement of Elevator Trim Tab Bracket

FINNISH AD M 1080/82 LFV LVD1971 MITSUBISHI SB 176 Rev E

12-dec-84 18-apr-85


Insp. of wingflap controlsystem FAA, U.S AD 75-16-13 LFV LVA1011 Rev A MITSUBISHI SB 167 Rev D

06-sep-76 18-jan-77 Revision C PCW by Swedair.

JCAB AD TCD-1188-75

Insp. of propeller controllever inst. FAA, U.S AD 75-16-20 LFV LVA1012 MITSUBISHI SB 168 Rev A

06-May-1975

20-jan-88

JCAB AD TCD-1202-75

Engine Cowling Latches FAA, U.S AD 78-03-05 LFV LVA1014 Rev A MITSUBISHI SB 171 Rev B MITSUBISHI SB 180 Rev A

20-sep-75 15-jul-04 Found SB 171 and SB 180 PCW.

JCAB AD TCD-1209-75

Insp/mod of NLG shimmydamper locking

LFV LVA1013 MITSUBISHI SB 169 Rev B 16-jun-75 10-jul-75


2012-12-06


60(195)

JCAB AD TCD-

1235-75

Insp./repl. of MLG fwd door

emerg.cables

LFV LVA1083 MITSUBISHI SB 170 Rev A 19-sep-75 18-jan-88 N/A N/A due to model.

JCAB AD TCD-

1272-75

Supp.,MLG Forward D. Actuating

Mech.-I&M

MITSUBISHI SB 172 14-nov-75 26-mar-09 N/A by model

JCAB AD TCD-

1284-1-76

Prevent failure of MLG. dragstrut MITSUBISHI SB 173 Rev A 31-mar-76 24-nov-09 PCW Ref. SB 173

JCAB AD TCD-1328-76

Fire hazard in rear baggage compartment

01-jul-76 26-mar-09 N/A by s/n

JCAB AD TCD-

1353-76

Barrel Nut, Inner/Outer Wing Conn.-

Repl.

MITSUBISHI SB 175 16-aug-76 01-sep-09 N/A by s/n

JCAB AD TCD-

1370-76

Inspect strobelight conduit in

Tiptank

LFV LVA1196 18-Oct-

1976

18-jan-88 Part.1

JCAB AD TCD-

1370A-81


Tiptank supersed TCD-1370-76

MITSUBISHI SB 174 PART 1 Rev C 05-nov-81 16-nov-10

JCAB AD TCD-

1379-1-80

Insp. rear eng. cowling reg.

heatdamage

LFV LVA1197 Rev A MITSUBISHI SB 177

Rev B

06-feb-02 22-nov-77 Previously complied with

JCAB AD TCD-

1520A-77

Latch link engine nacelle door MITSUBISHI SB 180 Rev A 12-dec-77 24-mar-09 ref. SB 180

JCAB AD TCD-

1768-1-85

Fatigue failure of the NLG strut assy. LFV LVA1546 MITSUBISHI SB 181 PART 12-jul-85 15-jul-04 PCW Found SB 181 part 2 PCW.

JCAB AD TCD-

1817-79

Modification of

bagagecompartment

LFV LVA1583 MITSUBISHI SB 182 05-feb-02 11-feb-80 N/A N/A due to s/n.

JCAB AD TCD-

2048-81

Insp. firewarning & emerg.power

circuit

LFV LVA1740 MITSUBISHI SB 187 Rev B 05-feb-02 27-May-

1985

N/A N/A due to s/n.

JCAB AD TCD-

2070-81

Inspect NLG downlock mechanism LFV LVA1753 MITSUBISHI SB 188 05-feb-02 12-Oct-

1981

JCAB AD TCD-

2113-82

Insp./replace engine electrical

harness

LFV LVA1788 MITSUBISHI SB 191 06-feb-02 18-mar-82

JCAB AD TCD-

2252-2-88

Flap system torquetubes supersed

TCD-2252-1-87

01-feb-89 24-mar-09 PCW

JCAB AD TCD-

2252-83

Flapcontrolsystem torquetubes LFV LVA1873 MITSUBISHI SB 189 Rev C 04-feb-83 15-feb-95

JCAB AD TCD-

2263-83

NLG. bracket attaching to drag strut 13-aug-83 24-mar-09 N/A by model

JCAB AD TCD-2342-1-84

Engine inlet anti-ice tubing. Torq./lock

MITSUBISHI SB 196 Rev A 05-jun-84 10-mar-09 PCW

JCAB AD TCD-2342-84


LFV LVA1942 MITSUBISHI SB 196 Rev A 06-feb-02 31-jul-84


Pitot Tube Wiring LFV LVD2015 Rev B MITSUBISHI SR 053A 16-jun-87 15-jul-04 SB PCW.


2012-12-06


61(195)

JCAB AD TCD-

2451-1-87

Add. seal/Tq. insp of flap flex. shaft 01-May-

1987

09-mar-09 PCW see TCD-2451-85

JCAB AD TCD-

2451-85

Add. seal/Tq. insp of flap flex. shaft

Superseeded by TCD-2451-1-87

LFV LVD2037 MITSUBISHI SB 198 30-sep-85 14-jun-85

JCAB AD TCD-

2545-1-88

Generator System LFV LVD2191 MITSUBISHI SB 201 Rev A 01-jul-88 17-May-

1990


Auto-ignition System FINNISH AD M 2435/97 LFV LVD2761 MITSUBISHI SB 226 Rev E

01-feb-97 22-nov-01

JCAB AD TCD-

2856-1-97

Bendix M4C Autopilot System MITSUBISHI SB 206 05-nov-97 16-nov-09 N/A due to Autopilot model

JCAB AD TCD-

3378-90

Insp./mod. of rudder trimtab

leadingedge

LFV LVD2338 MITSUBISHI SB 211 28-mar-91 14-jul-04 N/A N/A by s/n.

JCAB AD TCD-

3393A-96

Anti ice/De-ice system FINNISH AD M 2364/96 LFV LVD2347 Rev

1 MITSUBISHI SB 212 Rev A

25-May-

1996

16-nov-10

JCAB AD TCD-

3464-91

Unintentional engagement of

A/P......

17-jun-91 24-mar-09 N/A by model

JCAB AD TCD-

3740A-98

Mod.of Autopilote pitchtrimsystem

MSB 216, 228 LVD 2898

FINNISH AD M 2581/98 LFV LVD2450 LFV

LVD2898 MITSUBISHI SB 216 MITSUBISHI SB 228

17-aug-98 27-Oct-

1998

JCAB AD TCD-3901-93

Tiptank inst FINNISH AD M 2110/93 LFV LVD2512 MITSUBISHI SB 221

10-sep-93 21-feb-94


Inspection of landing gear lower pin FINNISH AD M 2238/95 LFV LVD2592 MITSUBISHI SB 219 Rev A

28-nov-94 24-mar-95

JCAB AD TCD-

3942-94

Change lockingpin ldg LFV LVD2538 MITSUBISHI SB 219 Rev A 01-feb-94 08-mar-95

JCAB AD TCD-

4310-96

Fwd. Fitting Bolt FINNISH AD M 2351/96 LFV LVD2688

MITSUBISHI SB 225

01-apr-96 29-nov-96

JCAB AD TCD-

4311-95

Windshield/window insp. FINNISH AD M 2331/96 LFV LVD2678

MITSUBISHI SB 224 Rev C

01-nov-95 16-nov-10

JCAB AD TCD-

4379-96

Feathering Valve/Linkage insp. FINNISH AD M 2352/96 LFV LVD2689

MITSUBISHI SB 229

01-apr-96 30-jul-96

JCAB AD TCD-

4552-96

Icing Limitation FAA, U.S AD 96-25-02 LFV LVD2749 27-dec-96 13-feb-02

JCAB AD TCD-

4625-97

Mod.of Trimsystem/AFM Revision FINNISH AD M 2460/97 UPPHÄVD MAI SB

093/22-009

14-jul-97 04-Oct-

2001

JCAB AD TCD-

4625A-2001

Mod of trim system/AFM revision LFV LVD3122 MITSUBISHI SB 231 Rev B

NYGE TDM01-45

16-mar-01 13-mar-09 PCW Ref AMOC LFV Appr M15/01, TDM 01-45

JCAB AD TCD-

4626-97

De-ice system Modification FINNISH AD M 2461/97 LFV LVD2800

MITSUBISHI SB 232 Rev A

01-May-

1997

14-jul-04 PCW


2012-12-06


62(195)

JCAB AD TCD-

4684-97

Mod. of Bearing box Ldg. Act. FINNISH AD M 2495/97 LFV LVD2819

MITSUBISHI SB 230

01-jun-97 25-mar-99

JCAB AD TCD-

4753-98

Ändring av flyghandbok LVD

2922,FAA AD 97-20-14, MHI SN 117A

FINNISH AD M 2518/98 LFV LVD2922

MITSUBISHI SN 117 Rev D

18-feb-98 02-dec-98 FAA AD utförd.


Icing-related incidents VIDEO FAA, U.S AD 2003-22-07 Rev 1 24-feb-04 17-May-2004


JCAB AD TCD-

4838-98

Inspection of landing gear power

train


MITSUBISHI SB 235

04-aug-98 24-mar-09 N/A by model

JCAB AD TCD-

4889-2-2007

Inappropriate calib. of eng. trq-

meter

MITSUBISHI SB 233 Rev B 21-jun-07 11-sep-07 Previously carried out, ref. SB 233A.

JCAB AD TCD-

4889-98

Insp. of Engine Torque Indication

System LFV 2924, MU SB 233


MITSUBISHI SB 233 Rev B

05-nov-98 14-jul-04 PCW

JCAB AD TCD-

4890-98

Check of flight idle FF LVD 2925, MU

SB 234


MITSUBISHI SB 234

04-nov-98 16-nov-10

JCAB AD TCD-

5030-99

Inspect the fuselage frame LFV LVD2988 MITSUBISHI SB 209 Rev B 17-May-

1999

24-mar-09 N/A by model

JCAB AD TCD-5432-2000

AFM revision LFV LVD3112 27-nov-00 12-feb-02


To prevent loss of airplane control LFV LVD3123 16-mar-01 12-feb-02


Inspection of Tip Tank Brackets LFV LVD3166 MITSUBISHI SB 236 12-sep-01 04-Oct-2001

JCAB AD TCD-

5864-2001

Flap Drive Train Inspection LFV LVD3212 MITSUBISHI SB 237 27-dec-01 17-jan-02

JCAB AD TCD-

6127-2003

Pneumatic Line insp. LFV LVD3322 MITSUBISHI SB 239 17-mar-03 04-nov-03

JCAB AD TCD-

7030-2006

Inspection of Wing Attachment

Hardware

MITSUBISHI SB 241 Rev A 27-dec-06 17-jan-07 c/o in conjunction with wingstudie

LFV,

Luftfartsverket

LFV LVA 1011 A Kontroll av vingklaffarnas manöversystem

FAA, U.S AD 75-16-13 JCAB AD TCD-1094A-76 MITSUBISHI SB 167 Rev D

05-feb-02 A 18-jan-77 Revision C PCW by Swedair.

LFV LVA 1012 Kontroll av propellerreglagets montering

FAA, U.S AD 75-16-20 JCAB AD TCD-1188-75 MITSUBISHI SB 168 Rev A

05-feb-02 20-jan-88

LFV LVA 1013 Kontr. och mod. av låsning på nosställ

JCAB AD TCD-1209-75 MITSUBISHI SB 169 Rev B

05-feb-02 10-jul-75


2012-12-06


63(195)

LFV LVA 1014 A Kontr. & byte av motorinkl.

låsanordning

FAA, U.S AD 78-03-05 JCAB AD TCD-1202-

75 MITSUBISHI SB 171 Rev B MITSUBISHI SB 180 Rev A

05-feb-02 A 18-jan-88

LFV LVA 1083 Insp. & utbyte av lina för nödöppning

JCAB AD TCD-1235-75 MITSUBISHI SB 170 Rev A

05-feb-02 18-jan-88 N/A N/A due to s/n.

LFV LVA 1196 Isolering av strobe light från bränsle JCAB AD TCD-1370-76 MITSUBISHI SB 174 PART 1 Rev C

06-feb-02 16-nov-10

LFV LVA 1197 A Förhindr. av värmeskador på

bak.motorpl.

JCAB AD TCD-1379-1-80 MITSUBISHI SB

177 Rev B

06-feb-02 A 22-nov-77 Previously complied with

LFV LVA 1238 Kontr. & byte av infästningsdet.

trimrod

06-feb-02 21-apr-09 N/A by s/n

LFV LVA 1546 Sprickundersökning av nosställ FAA, U.S AD 86-15-03 JCAB AD TCD-1768-

1-85 MITSUBISHI SB 181 PART 2 Rev B

06-feb-02 18-jan-88

LFV LVA 1583 Modifiering av bagageutrymme JCAB AD TCD-1817-79 MITSUBISHI SB 182 05-feb-02 11-feb-80 N/A N/A due to s/n.

LFV LVA 1740 Kontr.av brandvarnings-och

n"dstr"mskret

JCAB AD TCD-2048-81 MITSUBISHI SB 187

Rev B

05-feb-02 31-aug-09 N/A by s/n

LFV LVA 1753 Kontroll av låsmekanism i nosställ JCAB AD TCD-2070-81 MITSUBISHI SB 188 05-feb-02 12-Oct-

1981

LFV LVA 1788 Kontroll/Utbyte av elledningar på

motor

JCAB AD TCD-2113-82 MITSUBISHI SB 191 06-feb-02 18-mar-82

LFV LVA 1873 Insp./utbyte av infäst.till torsionsrör JCAB AD TCD-2252-83 MITSUBISHI SB 189

Rev C

06-feb-02 15-feb-95

LFV LVA 1942 Momentdragning/låsn.av koppl.i varmlufts


06-feb-02 31-jul-84

LFV LVA 438 Justering av bränslemängdsmätare JCAB AD TCD-0643-70 MITSUBISHI SB 114 05-feb-02 15-jul-04 N/A N/A by s/n.

LFV LVA 439 Rev. av flyghandbok betr.

bränslespec.


Rev C

05-feb-02 18-jan-88

LFV LVA 456 Inspektion av bultar i nossst,ll JCAB AD TCD-0652-70 MITSUBISHI SB 119 05-feb-02 26-mar-09 N/A by model

LFV LVA 457 Utbyte av lager i nosst,llets

st"td,mp.

JCAB AD TCD-0660-70 MITSUBISHI SB 123 05-feb-02 26-mar-09 N/A by s/n

LFV LVA 543 B Insp. och målning av integraltankar JCAB AD TCD-0730-1-72 05-feb-02 B 14-jul-04 N/A N/A by s/n.

LFV LVA 645 Modifiering av el-system JCAB AD TCD-0859-72 MITSUBISHI SB 156 05-feb-02 16-nov-09 N/A by s/n

LFV LVA 664 Nosställsväxellåda och struktur JCAB AD TCD-0866-72 05-feb-02 31-aug-09 N/A by s/n

LFV LVA 828 A Kontr. & mod. av klaffdrivning JCAB AD TCD-0947A-74 MITSUBISHI SB 162 Rev A

05-feb-02 A 18-jan-88 N/A N/A due to s/n.

LFV LVA 829 A Inspektion av frontrutor FAA, U.S AD 74-11-01 FAA, U.S AD 75-03- 05-feb-02 A 05-May-


2012-12-06


64(195)

06 JCAB AD TCD-0948A-74 MITSUBISHI SB

163 Rev B

1974

LFV LVA 886 A Kontroll/byte av

höjdtrimroderarmar

JCAB AD TCD-1001A-76 05-feb-02 A 18-apr-85

LFV LVD 1238 Kontr./byte infästn.det.

höjdtrimroder

15-apr-77 31-aug-09 N/A by s/n

LFV LVD 1971 Elevator Trim Tab MU2 SB 176E JCAB AD TCD-1001B-2-84 MITSUBISHI SB 176 Rev E

18-jan-85 18-apr-85

LFV LVD 2015 B Pitot Tube Wiring MAI SR 020/34-

005 Rev A, MHI SR 53

FAA, U.S AD 86-20-01 JCAB AD TCD-

2450A-87 MAI SR 020/34-005

MITSUBISHI SR 053A

24-May-

1985

B 06-mar-86

LFV LVD 2037 Flap Flexible Shaft MU2 SB 198 JCAB AD TCD-2451-85 MITSUBISHI SB 198 30-sep-85 14-jun-85

LFV LVD 2069 Altimeter 25-mar-86 18-jan-88 N/A N/A by p/n & s/n

LFV LVD 2113 Modif. & revision Handbook MHI SR 006B, MAI SR 040/74-001RA

26-jan-87 11-sep-87

LFV LVD 2190 Autopilot Switch MU2 SB 066/22-006 och SB 206

FAA, U.S AD 88-13-01 MAI SB 066/22-006 Rev A MITSUBISHI SB 206

19-aug-88 17-May-1990

N/A Bendix A/P ej installerad

LFV LVD 2191 Generator System MU2 SB 201A JCAB AD TCD-2545-1-88 MITSUBISHI SB 201 Rev A

19-aug-88 25-Oct-1988

LFV LVD 2202 Kontr. av koppl. för tors.rör till klaff FAA, U.S AD 88-23-01 JCAB AD TCD-2252-

1-87 MAI SB 067/27-008 Rev A MITSUBISHI SB 189 Rev C

08-dec-88 15-feb-95

LFV LVD 2206 Modifiering av Autopilot FAA, U.S AD 88-21-01 Rev 1 08-dec-88 12-feb-02

LFV LVD 2338 Kont./Mod.av sidorodrets

trimroderframka Mitsubishi MHI SB

211

JCAB AD TCD-3378-90 MITSUBISHI SB 211 28-mar-91 14-jul-04 N/A N/A by s/n.

LFV LVD 2347 1 Control Deice-system Mitsubishi SB

212A

JCAB AD TCD-3393A-96 MITSUBISHI SB

212 Rev A

29-May-

1996

1 16-nov-10


CHPT 9

23-May-

1991

05-jun-91 checked OK.

LFV LVD 2450 Elevator Trim Tab Installation MU SB

216


216

03-dec-92 31-mar-93

LFV LVD 2477 Electric Trim System AD930711, MU

SB 079/27-0-010

FAA, U.S AD 93-07-11 MAI SB 079/27-010 03-jun-93 27-mar-09 N/A by s/n

LFV LVD 2512 TIP TANK INST. (NXT 100H) JCAB AD TCD-3901-93 MITSUBISHI SB 221 02-dec-93 21-feb-94

LFV LVD 2537 Reducering av Höjdrodrets trimområde. FAA AD 94-04-16, SB

FAA, U.S AD 94-04-16 MITSUBISHI SB 216 07-apr-94 31-mar-93


2012-12-06


65(195)

216

LFV LVD 2538 Byte Låspinne i landställets nödutf.

SB 219


Rev A

07-apr-94 24-mar-95

LFV LVD 2551 Adj.of Ground Idle FAA AD 94-11-04 FAA, U.S AD 94-11-04 22-jun-94 27-mar-09 N/A by s/n

LFV LVD 2592 Insp/Repl. of Lock-pin in L/G gearbox TCD-3942-1-94, MSB 219A

JCAB AD TCD-3942-1-94 MITSUBISHI SB 219 Rev A

09-feb-95 24-mar-95

LFV LVD 2678 Kontr. av vindrutor och fönster MHI

SB 224 Rev A


4311-95 MITSUBISHI SB 224 Rev C

12-mar-96 16-nov-10

LFV LVD 2688 Kontr/byte av infästn.bult för

tiptank MU-2 SB 225


96 MITSUBISHI SB 225

09-May-

1996

29-nov-96

LFV LVD 2689 Kontroll av linkage för prop.flöjning

MU-2 SB 229

JCAB AD TCD-4379-96 MITSUBISHI SB 229 09-May-

1996

30-jul-96

LFV LVD 2732 Inspection/ Replacement of Prop

Hub. FAA AD 96-18-14, Hz SB 136H

FAA, U.S AD 96-18-14 HARTZELL SB 61-

261 Rev 1

27-sep-96 09-mar-98 Prop. utbytt mot BVA

LFV LVD 2749 Revision av flyghandbok AFM TCD-

4552-96


96

21-jan-97 13-feb-02

LFV LVD 2761 Installation av autoignition system

TCD-2679A-97


226 Rev E

14-feb-97 19-mar-99

LFV LVD 2769 Demont.av backventil i bränslesystemets MU-2 SB 130A

FAA, U.S AD 97-04-13 MITSUBISHI SB 130 Rev A

18-mar-97 05-May-1997

N/A due to s/n.

LFV LVD 2800 Mod. av De-ice Monitoring System Mitsubishi SB 232, TCD-4626-97


28-aug-97 08-May-1998

LFV LVD 2819 Mod.av lagerboxar för landställssystem Mitsubishi SB 230

JCAB AD TCD-4684-97 MITSUBISHI SB 230 18-nov-97 09-mar-98


23-mar-98 16-nov-10

LFV LVD 2897 Kontroll av landst,llets drivsystem TCD-4838-98, SB 235

JCAB AD TCD-4838-98 MITSUBISHI SB 235 02-aug-98 24-mar-09 N/A by model

LFV LVD 2898 Mod. av autopilotens höjdtrimsystem TCD-3740A-98, SB 216, 228

JCAB AD TCD-3740A-98 MITSUBISHI SB 216 MITSUBISHI SB 228

27-aug-98 27-Oct-1998

LFV LVD 2922 Änd.av Flyghandbok-Extra krav på typutbi TCD-4753-98, MHI SN 117A

JCAB AD TCD-4753-98 MITSUBISHI SN 117 Rev D

12-nov-98 02-dec-98 FAA AD utförd.

LFV LVD 2924 Kontr/Just av motorernas Torque indikeri MHI SB 233, TCD-4889-98


01-dec-98 19-mar-99

LFV LVD 2925 Kontr/just av mot bränsleflöde Flight Id MHI SB 234

JCAB AD TCD-4890-98 MITSUBISHI SB 234 01-dec-98 08-apr-10

LFV LVD 2988 Sprickkontroll av kroppsspant JCAB AD TCD-5030-99 MITSUBISHI SB 209 18-jun-99 24-mar-09 N/A by model


2012-12-06


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Rev B

LFV LVD 3112 Revision av flyghandbok JCAB AD TCD-5432-2000 30-jan-01 12-feb-02

LFV LVD 3122 Modifiering av autopilotsystemet JCAB AD TCD-4625A-2001 MAI SB 093/22-009 MITSUBISHI SB 231 Rev B NYGE TDM01-45

02-apr-01 04-Oct-2001

Ref AMOC LFV Appr M15/01, TDM 01-45

LFV LVD 3123 Ändring av flyghandbok JCAB AD TCD-5547-2001 02-apr-01 12-feb-02

LFV LVD 3166 Sprickkontroll av infästning till ving-

spetstank

JCAB AD TCD-5747-2001 MITSUBISHI SB

236

20-sep-01 04-Oct-

2001

LFV LVD 3212 Kontroll av vridaxel till vingklaff. JCAB AD TCD-5864-2001 MAI SB 099/27-


09-jan-02 17-jan-02

LFV LVD 3322 Kontroll av tryckluftsledningar JCAB AD TCD-6127-2003 MITSUBISHI SB

239

21-mar-03 04-nov-03

MAI, Mitsubishi Aircraft

International

MAI SB 047/30-001

A Torque of Bleed Air Tube Coupling Nuts AD 84-12-04,SB 196A


19-jul-84 A 31-jul-84

MAI SB 051/27-007

Add.Seal and Flap Flexible Shaft Torque AD 87-04-03, SB 198

FAA, U.S AD 87-04-03 01-feb-85 14-jun-85

MAI SB 067/27-008

A Insp/Repl. of Flap Control System Torque AD 88-23-01, SB 189B

FAA, U.S AD 88-23-01 LFV LVD2202 29-mar-95 A 15-feb-95

MAI SB 069/24-006

Split Radio Bus Inspection and Rework

MAI SB 066/22-006 Rev A 17-nov-88 06-jun-89 N/A N/A due to Aircraft s/n

MAI SB 086/74-002

A Auto-Ignition System Installation FAA, U.S AD 2000-09-15 Rev 1 FINNISH AD M 2435/97 MITSUBISHI SB 226 Rev E

05-Oct-2000

A 22-nov-01 Action not required due to s/n.

MAI SB 089/57-

002

A Insp/Repl. of Bolts for Wing Tip Tank FAA, U.S AD 98-20-39 05-nov-96 A 29-nov-96 N/A N/A due to s/n.

MAI SN 110/00-

017A

Power Lever Position Warning 25-feb-09 09-nov-09 SB 240 considered

MAI SN 111/77-

004

Torque Indicating System Shift

Potential

20-nov-08 11-mar-09 SB 233 considered

MAI SR 020/34-

005

Anti Ice Capability AD 86-20-01, SR

053A

FAA, U.S AD 86-20-01 LFV LVD2015 Rev B

MITSUBISHI SR 053A

06-Oct-

1986

07-feb-00 N/A N/A due to s/n.

MITSUBISHI, Mitsubishi Heavy Industries Ltd

MITSUBISHI MSR B **RECOVERED RECORD** 11-sep-87


2012-12-06


67(195)

066

MITSUBISHI SB

066

Bendix M4D 18-dec-87 17-May-

1990

N/A

MITSUBISHI SB

076/22-008

M-4() Autop.Engage Switch Guard

Install.

11-apr-91 12-apr-95 N/A

MITSUBISHI SB

112

C Anti-Ice Additive in Fuel -Usage of JCAB AD TCD-0642-70 LFV LVA439 09-Oct-

1971

C 18-jan-88

MITSUBISHI SB

114

Fuel Quantity Indicator

Readjustmnet

JCAB AD TCD-0643-70 LFV LVA438 01-jan-70 15-jul-04 N/A N/A by s/n.

MITSUBISHI SB

119

The Bolt and Bolt Hole Diam. of

Nose L.G

JCAB AD TCD-0652-70 LFV LVA456 10-mar-70 26-mar-09 N/A by model

MITSUBISHI SB 123

Bearing,Oleo Strut,Nose L.G. -Repl. of

JCAB AD TCD-0660-70 LFV LVA457 01-apr-70 26-mar-09 N/A by s/n

MITSUBISHI SB 124

Scissors Switch,Nose L.G. -Install. of 31-aug-70 18-jan-88 N/A

MITSUBISHI SB 128

B Tip Tank Air Pressure Modification 28-jun-94 B 05-nov-09 N/A by model & s/n

MITSUBISHI SB 143

B Top Coating, Wing Integral Main F.T.-SIo

JCAB AD TCD-0730-1-72 JCAB AD TCD-0730-2-86

05-jan-72 B 14-jul-04 N/A N/A by s/n.

MITSUBISHI SB 162

A Flex. Shafts, Flap Control Sys.-Insp. of (AD750201)

JCAB AD TCD-0947A-74 LFV LVA828 Rev A 03-Oct-1974

A 18-jan-88 N/A

MITSUBISHI SB 163

B Insp. of Outer Pane, Front Winds. & Inst

FAA, U.S AD 74-11-01 JCAB AD TCD-0948A-1-78 JCAB AD TCD-0948A-74 LFV LVA829 Rev A

16-nov-78 05-May-1974

MITSUBISHI SB 165

A Lubr. Interval,Wheel Bearing,Main & Nose

24-jul-80 19-jan-88 N/A

MITSUBISHI SB 166

Wing Flap 24-jul-80 18-jan-88 N/A

MITSUBISHI SB 167

D Flap M.Jack Screw-Insp. of and/or Main G

FAA, U.S AD 75-16-13 JCAB AD TCD-1094A-76 LFV LVA1011 Rev A

24-jul-80 D 18-jan-77 Revision C PCW by Swedair.

MITSUBISHI SB 168

A Propeller Pitch Control Lever-Insp. of (AD761620)

FAA, U.S AD 75-16-20 JCAB AD TCD-1188-75 LFV LVA1012

24-jul-80 A 20-jan-88

MITSUBISHI SB 169

B Shimmy Damper-Insp. and Modification of

JCAB AD TCD-1209-75 LFV LVA1013 24-jul-80 B 05-nov-09 PCW

MITSUBISHI SB 170

A MLG Forward Door Em.Op. Cable-Insp. & Re (AD762204)

JCAB AD TCD-1235-75 LFV LVA1083 24-mar-77 A 18-jan-88 N/A N/A due to s/n

MITSUBISHI SB 171

B Latches,Eng. Nacelle Upper D.-Insp.& Mod (AD780305)

FAA, U.S AD 78-03-05 JCAB AD TCD-1202-75 LFV LVA1014 Rev A

17-nov-77 B 18-jan-88


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MITSUBISHI SB

173

A Drag Strut, Main L.G.-Modification

of

JCAB AD TCD-1284-1-76 24-jul-80 12-feb-76

MITSUBISHI SB

174 PART 1

C Tip Tank Conduit Tube-Insp.of,and

Rew.of (AD830902)

FINNISH AD M 1177/83 JCAB AD TCD-

1370A-81 LFV LVA1196

02-Oct-

1981

C 16-nov-10

MITSUBISHI SB

175


Repl.

JCAB AD TCD-1353-76 26-jun-76 01-sep-09 N/A

MITSUBISHI SB 176

E Elevator Trim Tab Bracket-Repl. of LVD1971, AD 84-25-02, SB 031/27-

005R1

FAA, U.S AD 84-25-02 FINNISH AD M 1080/82 JCAB AD TCD-1001A-76 JCAB AD

TCD-1001B-2-84 LFV LVD1971

26-sep-84 E 18-apr-85

MITSUBISHI SB

177

B Mod. of Engine Nacelle Tail Area

(AD810601)

JCAB AD TCD-1379-1-80 LFV LVA1197 Rev

A

11-sep-80 B 22-nov-77 Previously complied with

MITSUBISHI SB

179

Rodd Assem., Engine Nacelle Upper

D.-R&M

27-May-

1977

25-Oct-

1988

MITSUBISHI SB

180

A Link, Engine Nacelle Upper D.-Repl.

of (AD780305)


75 JCAB AD TCD-1520A-77 LFV LVA1014 Rev A

17-nov-77 A 20-apr-78

MITSUBISHI SB 181 PART 2

B Insp. and Repl. of Nose L.G. Strut Assem (AD801812)

FAA, U.S AD 86-15-03 JCAB AD TCD-1768-1-85 LFV LVA1546

08-apr-85 B 18-jan-88

MITSUBISHI SB

182

Add. of Ceiling Cover, Rear Bagg.

Comp.

JCAB AD TCD-1817-79 LFV LVA1583 16-nov-79 16-nov-79 N/A N/A due to s/n.

MITSUBISHI SB

184

Turnbuckle, Control Cables -Repl. of 04-apr-80 05-feb-88

MITSUBISHI SB

188

Down Lock Mech., Nose L.G.-Insp. of JCAB AD TCD-2070-81 LFV LVA1753 13-jul-81 12-Oct-

1981

MITSUBISHI SB

189

C Flap Control Torque Tube AD 88-23-

01, SB 067/27-008


2252-1-87 JCAB AD TCD-2252-83 LFV LVA1873 LFV LVD2202

28-jun-94 C 15-feb-95

MITSUBISHI SB 190

A Trav. Nut Repl. of L.G. Mech. Stop Assem

28-jun-94 06-dec-83

MITSUBISHI SB

191

Engine El. Wire-Insp. and

Replacement of (AD820802)

JCAB AD TCD-2113-82 LFV LVA1788 21-dec-81 18-mar-82

MITSUBISHI SB

193

B Landing Gear Warning Horn

Syst.Modif.

15-jun-94 B 04-dec-00 Rev A är utförd.

MITSUBISHI SB

194

Master Cauting Light Visibility-Impr.

of

23-aug-82 23-mar-83

MITSUBISHI SB

196

A Ret. of coupling nut on the bleed air

tu AD 84-12-04, SB 047/30-001


1-84 JCAB AD TCD-2342-84 LFV LVA1942 MAI SB 047/30-001 Rev A

12-apr-84 A 31-jul-84

MITSUBISHI SB 198

Add. Seal & Torque Insp. of Flap Flex.Sh LVD2037, AD 87-04-03, SB

FAA, U.S AD 87-04-03 JCAB AD TCD-2451-85 LFV LVD2037

13-feb-85 14-jun-85


2012-12-06


69(195)

051/27-007

MITSUBISHI SB

199

A Engine Lubricating Tubing Insp. &

Protec

24-jun-94 A 06-nov-09 PCW

MITSUBISHI SB

200

B Insp of Nose Ldg Gear Drag Strut

Link

24-jun-94 A 25-Oct-

1988

MITSUBISHI SB

201

A Generator Circuit Wires Insp. and

Mod.


1-88 LFV LVD2191

02-mar-88 A 17-May-

1990

MITSUBISHI SB

204

Speed Placard Change 03-mar-87 05-feb-88

MITSUBISHI SB

206

Bendix Autop.Disengagement

Method Stand.


1-97 LFV LVD2190

13-Oct-

1987

31-jan-89 N/A N/A due to Autopilot model

MITSUBISHI SB 207

Rudder T.T. & Elevator T.T. Insp. & Rep.

20-May-1988

27-nov-09

MITSUBISHI SB 209

B Fuselage inspection JCAB AD TCD-5030-99 LFV LVD2988 19-apr-99 B 24-mar-09 N/A by model

MITSUBISHI SB 210

A Engine Ignition Unit Replacement 12-nov-96 06-mar-98

MITSUBISHI SB 211

Rudder Trim Tab Modification (LVD 2338)

JCAB AD TCD-3378-90 LFV LVD2338 20-nov-90 14-jul-04 N/A

MITSUBISHI SB 212

A Insp of Anti-ice/Deice Systems (LVD 2347),

JCAB AD TCD-3393A-96 LFV LVD2347 Rev 1

25-apr-96 A 16-nov-10

MITSUBISHI SB 214

Engine Control Rod Inspection 06-dec-91 31-mar-93

MITSUBISHI SB 215

Removel of Prop. Governor Speed Signal

23-Oct-1991

31-jan-92 N/A N/A due to -1 engine

MITSUBISHI SB 216

Elevator Trim Tab Installation (LVD 2450

FAA, U.S AD 2007-17-09 FAA, U.S AD 94-04-16 JCAB AD TCD-3740A-98 LFV LVD2450 LFV LVD2537 LFV LVD2898

11-sep-92 31-mar-93

MITSUBISHI SB 218

A Propeller Feathering Linkage Inspection

17-jan-94 A 21-feb-94

MITSUBISHI SB 219

A Emergency Gear Down G.box Lower Pin Repl

JCAB AD TCD-3942-1-94 JCAB AD TCD-3942-94 LFV LVD2538 LFV LVD2592

24-Oct-1994

A 24-mar-95

MITSUBISHI SB 221

Tip Tank Conduit Tube Insp. and Rep.

JCAB AD TCD-3901-93 LFV LVD2512 10-aug-93 21-feb-94

MITSUBISHI SB 222

Fuselage Waterproof Modification SR 019

28-jun-94 19-mar-99

MITSUBISHI SB 223

Pitot/Static System Improvement SR 064

MITSUBISHI SR 053A MITSUBISHI SR 064 28-jun-94 07-feb-00


2012-12-06


70(195)

MITSUBISHI SB

224

C Acrylic Windsheild/Window glass

Insp. UHB

FAA, U.S AD 2003-17-04 FINNISH AD M

3076 JCAB AD TCD-4311-95 LFV LVD2678

30-apr-98 C 16-nov-10

MITSUBISHI SB

225

Forward fitting bult of wingtip tank

LVD 2688


2351/96 JCAB AD TCD-4310-96 LFV LVD2688

29-sep-95 29-nov-96

MITSUBISHI SB 226

E Auto-Ignition System Installation LVD 2761 (2113), AD TCD-2679A-97

FAA, U.S AD 2000-09-15 Rev 1 FAA, U.S AD 86-26-02 FINNISH AD M 2435/97 FINNISH AD M 2786/00 JCAB AD TCD-

2679A-97 LFV LVD2761 MAI SB 086/74-002 Rev A

18-sep-01 E 22-nov-01 PCW

MITSUBISHI SB 227

Rudder Torque Tube Modification 20-dec-96 09-mar-98

MITSUBISHI SB 228

Elevator Trim Indicator Modification LFV 2898

FAA, U.S AD 2007-17-09 FINNISH AD M 2581/98 JCAB AD TCD-3740A-98 LFV LVD2898

13-jul-98 27-Oct-1998

MITSUBISHI SB 229

Feathering Valve/Linkage Insp. FAA, U.S AD 2006-15-07 JCAB AD TCD-4379-96 LFV LVD2689

20-feb-96 30-jul-96

MITSUBISHI SB 230

Mod.of Bearing Box Ldg. Gear Act. LVD 2819

JCAB AD TCD-4684-97 LFV LVD2819 05-mar-97 09-mar-98

MITSUBISHI SB 231

B Inst.of Trim-In-Motion Alert System FAA, U.S AD 2000-09-15 Rev 1 FINNISH AD M 2460/97 UPPHÄVD FINNISH AD M 2786/00 JCAB AD TCD-4625A-2001 LFV

LVD3122 MAI SB 093/22-009 NYGE

TDM01-45

11-dec-02 B 03-mar-03 SL 079 allready performed.

MITSUBISHI SB 232

A De-Ice System Modification LVD 2800, TCD-4626-97

FAA, U.S AD 2000-09-15 Rev 1 FINNISH AD M 2786/00 JCAB AD TCD-4626-97 LFV

LVD2800 MAI SB 096/30-004

06-jun-02 A 06-jun-02 N/C due to previuosly complied with SB 232 rev 0.

MITSUBISHI SB

233

B Insp.of Engine Torque Indication

System. TCD-4889-98, LFV 2924


2608/98 JCAB AD TCD-4889-2-2007 JCAB

AD TCD-4889-98 LFV LVD2924

08-mar-07 B 18-apr-07 Checked, previously carried out

MITSUBISHI SB

234

Fl.Check of the Flight Idle Fuel Flow

Se TCD-4890-98, LVD 2925


4890-98 LFV LVD2925

07-Oct-

1998

16-nov-10

MITSUBISHI SB

235


train

JCAB AD TCD-4838-98 LFV LVD2897 04-aug-98 24-mar-09 N/A by model

MITSUBISHI SB

236

Inspection of Tip Tank Brackets JCAB AD TCD-5747-2001 LFV LVD3166 28-aug-01 04-Oct-

2001

MITSUBISHI SB

237

Inspection of Flap Drive Train JCAB AD TCD-5864-2001 LFV LVD3212 13-dec-01 17-jan-02

MITSUBISHI SB 238

Main Landing Gear Door Safety Pin 05-dec-02 09-jan-03 Perf. at each 600 h. insp.


2012-12-06


71(195)

MITSUBISHI SB

239

Pneumatic Line Insp. and

Modification

JCAB AD TCD-6127-2003 LFV LVD3322 26-dec-02 04-nov-03

MITSUBISHI SB

240

Inst.of Trottle Quadrant Placard 26-feb-03 20-Oct-

2003

MITSUBISHI SB

241

A Inspection of Wing Attachment

Hardware


7030-2006

21-nov-06 A 17-jan-07 c/o in conjunction with wingstudie

MITSUBISHI SL 060

System 17-feb-89 28-jun-91

MITSUBISHI SL

078

Automatic Autopilot Disconnect

System

28-jan-02 16-nov-10

MITSUBISHI SL

079

Diode inst.in Flap Position

Ind.Curcuit

28-jan-02 04-Oct-

2001

MITSUBISHI SL

080

Hartzell Propeller Mounting Bolt

Insp.

HARTZELL SB 61-256 05-apr-02 26-aug-02 Compliance in according to HC-SB-61-256.

MITSUBISHI SL

084

Pneumatic De-Ice Monitoring

System

14-jun-04 16-nov-10

MITSUBISHI SL

085

Hartzell prop. mount. bolt insp. HARTZELL SB 61-279 ALERT Rev 4 17-May-

2005

14-sep-05 Propellerbolts previously checked u/a

MITSUBISHI SN

053

B Rudder Torque Tube AD 86-20-01,

SB 020/34-005

05-nov-86 B 17-jan-88

MITSUBISHI SN

117

D Icing Awareness Training Video FAA, U.S AD 2003-22-07 Rev 1 JCAB AD

TCD-4753-98 LFV LVD2922

14-jun-04 D 17-May-

2004

MITSUBISHI SN

146

Water Ingress into Vertical Stabilizer 19-dec-03 12-mar-04

MITSUBISHI SN

148

Reminders for safe operation 18-nov-05 22-mar-06 Genomförs enl. AMP MU-2 & DHB

MITSUBISHI SN

156A


MITSUBISHI SN

157


Potential


MITSUBISHI SN

161

Repl Air Filter for Vacuum System MITSUBISHI STCSA01913SE 09-dec-09 11-mar-10 Ref STC SA01913SE

MITSUBISHI SN

164

IR Part 2, one time inspection of

mechanical stop bearing.

04-Oct-

2012

MITSUBISHI SR 053A

Modifiering av pitotrör FAA, U.S AD 86-20-01 JCAB AD TCD-2450A-87 LFV LVD2015 Rev B MAI SR

020/34-005 MITSUBISHI SB 223

23-Oct-1984

06-mar-86

MITSUBISHI SR

064

Pitot & Static System MITSUBISHI SB 223 30-apr-85 27-feb-00


2012-12-06


72(195)

MITSUBISHI SR

065

Warning Horn 20-jan-86 18-jan-88

MITSUBISHI SR

067

Emergency Exit Placard 17-sep-85 18-jan-88

MITSUBISHI SR

072

Air Filter Replacement for Vacuum

Syst.

25-apr-00 09-dec-05

MITSUBISHI SR 075

Inst. tip tank placard 29-Oct-2004

01-jun-05

MITSUBISHI STC

SA01913SE

Inst of a Vacuum System Air Filter MITSUBISHI SN 161 10-dec-09 11-mar-10 See MU-2B AMP Chpt 3 100h/1y inspection

NARCO, Narco

NARCO SB ELT10-

16

ELT ASSY 18-apr-88 28-jun-91 N/A

NYGE, Saab Aerotech Aircraft Services

NYGE TDM 01-45 Installation of Trim-In-Motion Alert

Syst. and Automatic A/P Disconnect syst.

JCAB AD TCD-4625A-2001 LFV LVD3122


07-May-

2001

04-Oct-

2001

NYGE TDM 02-10 Installation of TPE331-6-252M Engines

25-mar-02 04-Oct-2001

NYGE TDM 02-24 Installation Moving MAP 10-Oct-2002

28-Oct-2002

NYGE TDM 02-32 Installation EMI film 10-dec-02 10-jan-04

NYGE TDM 02-33 Viktminskning MU-2B 24-dec-02 01-mar-04

NYGE TDM 03-08 8 GNS430/530 & MODE S GTX330 install.

04-mar-03 8 31-Oct-2008

NYGE TDM 03-11 C Astor 2 MU-2B 19-mar-03 C 06-Oct-2003

Original compliance was as per TDM rev A.The A/C installation is IAW rev C as not affected by rev B

and C.F01322, F01347, F01349

NYGE TDM 03-15 A U95 with General Control System 24-apr-03 A 25-feb-08

NYGE TDM 03-28 F Nav Demo Pod 19-dec-03 F 27-nov-09 Original compliance by Rev D. Not affected by rev

F.

NYGE TDM 05-16 Viktor Counter Weight Pod 18-nov-05 18-nov-05

NYGE TDM 06-28 A Removable FR-31 29-jun-07 A 01-Oct-


2012-12-06


73(195)

2007

NYGE TDM 06-41 A Darts (to carry on MU-2B-20/26) 20-nov-06 A 07-feb-08

NYGE TDM 06-42 A Barlast DARTS MU-2B 04-dec-07 A 07-feb-08

NYGE TDM 07-30 A Install. of Emergency Axe 28-feb-08 A 28-feb-08

NYGE TDM 08-03 A Enhanced Surveillance MU-2B 28-feb-08 A 27-nov-09

NYGE TDM 08-28 B ELT 406 MU-2B 29-sep-08 B 31-Oct-

2008

Original compliance with TDM rev A. Rev B does

not affect previous complaiance.

NYGE TDM 09-22 A Electrical Wiring Feed Through 08-sep-09 A 27-nov-09

NYGE TDM 09-27 A GPS Splitter 12-Oct-

2009

A 27-nov-09

NYGE TDM 09-33 A MU-2B Loudspeaker in Cockpit 04-dec-09 A 04-May-

2010

C/W

NYGE TDM 10-25 A MU-2B Terminating Resistor 08-apr-10 A 19-May-2010

C/W

NYGE TDM 10-46 A MU-2 Alternate lap top computers A 10-Jun-2011

NYGE TDM 11-35 A Terminating resistor A 27-Jan-2012

NYGE TDM 12-21 A Avinstallation IK 14-Aug-2012

NYGE TDM 12-40 A MU-2B Relocation of MIC/Phone Jacks

04-Oct-2012

NYGE TDM 95-04 4 Vingstudie 20-sep-98 4 18-mar-03

NYGE TDM 97-03 Astor MU-2 25-feb-97 04-mar-98

NYGE TDM 98-08 Torrluft ASTOR 27-May-

1998

17-aug-98

NYGE TDM 99-03 Install. Auto Ignition 03-mar-99 19-mar-99

NYGE TVO 1/09 Inspektion av Stringers & struktur

vinge

25-feb-09 04-mar-09 Inspected with remarks

NYGE TVO 1/93 Low Volt Warning Light (BCL) 22-jan-93 31-mar-93

NYGE TVO 1/96 Slitage Flap Guide Rail 12-apr-96 09-Oct-

1998

NYGE TVO 1/97 3 De-Icertank MU-2B,

korrosionskontroll

12-feb-97 13-feb-97


2012-12-06


74(195)

NYGE TVO 2/00 Märkning av infästning domkraft

Mu2

01-dec-00 15-nov-00

NYGE TVO 2/07 A Prevent FR31 radio to xmit when

RM2 off

06-feb-07 A 28-feb-07

NYGE TVO 2/91 A/C Elecrical System 10-jan-91 07-aug-91

NYGE TVO 3/06 Inspect lower rudder hinge bracket 07-dec-06 16-nov-10

NYGE TVO 3/96 3 Wing Spar Flange Inspection. 24-feb-05 3 27-nov-09

NYGE TVO 4/11 A Static Inverter controll 15-Dec-2011

NYGE TVO 4/86 2 Wing Pod Inspection 06-apr-92 2 16-nov-10

NYGE TVO 4/91 Special Inspection (next E6.) 19-feb-91 07-aug-91

NYGE TVO 4/92 Engine Install. Kontr. rörledningar 29-apr-92 12-jun-92

NYGE TVO 4/94 3 Fwd. Wing Tiptank Attachment 28-sep-94 3 07-apr-10

NYGE TVO 4/96 Kontroll av Lagerhus i

noshjulsstyrning.

25-Oct-

1996

11-May-

1997

Utförd tidigare (ref.Ove N lista)

NYGE TVO 6/88 Allm. instruktion för metallpropeller 13-jun-88 07-apr-10

NYGE TVO 6/92 Elevator Trim Cable, check 07-Oct-

1992

12-nov-92

NYGE TVO 7/93 Starter Drive Splines 01-nov-93 18-jan-96

NYGE TVO 8/04 Kontr. av Spant vid bakre

feninfästning

08-dec-04 07-apr-10

NYGE TVO 8/92 Wheel Parts 27-Oct-

1992

31-mar-93

NYGE TVO 9/88 Emergency Extension System 08-aug-88 25-Oct-

1988


2012-12-06


75(195)

2.3 GFE Aircraft Mitsubishi MU-2 SE-GHB


Number:


total Hours:

Total

Landing

Cycles:

Date

Reference:

MU-2B-20 287 SE-GHB 11585 6415 2012-11-23


Serial

Number:

Total Hours

Since New:

Total

Cycles

Since New:

Hours remaining to

Overhau/HSI/GBI:

Left Engine P20019 11797 11513 1916/197/116

Right Engine P20146 9513 13195 3142/1346/1342


Left Propeller HC-B3TN-5C BVA 6205 2013-09-14














Airspeed Indicator LH / RH Aerosonic 065A-986402-003 /

20040-161







2012-12-06


76(195)

Attitude Gyro & Flight Director Ind.

LH

Century 52C77











GPS MAP


Laser Prism


Wing Pylon


EW system



Pylon


U95 Sorc Pod mounted system RH Wing Pylon




Chaff Dispenser


Pylon


TAPS


System:






Bus

Triax Cable x 1


115/200VAC 400 Hz 3-

AWG 12 x 4

twisted


2012-12-06


77(195)

Phase 3 x 10 A AWG 16 x 2


A

DC Power 28 VDC 200

A

AWG 2 x 2




2012-12-06


78(195)


rd 2012.


Aircraft SE-GHB

Vingstudie MU-2 AMP 2012-02-23 11477 12500

100 Hour Inspection AMP 2012-03-01 11477 11577,4 2013-03-01


600 Hour Inspection AMP 2011-03-08 11412 12012 2014-04-17


1200 Hour Inspection AMP 2007-07-31 11047 12247,5









Engine Gearbox Inspection AMP 11702 116,95

Engine S/N P-20146





Propeller R/H O/H AMP 2008-03-27 14144 2013-03-26


2012-12-06


79(195)

2.3.9 Implemented Changes Status dateNovember 23

rd 2012.

SB/AD etc

Reference

Rev Subject Document reference Eff. date Rev Complianc

e

Stat

us

Remarks


Systems Inc.

CENTURY SB CSB-2005-01

Check for frayed Bridle Cable 21-feb-05 31-mar-10

EASA, European Aviation

Safety Agency

EASA AD 2006-0265

Incorrect transponder altitude 30-aug-06 14-jan-10

EASA AD 2009-0251-E

Portable Fire Extinguishers-Ident/Repl 25-nov-09 07-May-2010


EASA AD 2009-

0262

Halon 1211 Fire Extinguishers Id/Repl EASA AD 2009-0278 FFE ASB26-115 Rev C 15-dec-09 07-May-

2010


EASA AD 2009-

0278

Halon 1211 Fire Extinguishers Id/Repl EASA AD 2009-0262 22-dec-09 07-May-

2010


EASA AD 2010-

0003

R1 Mode S Transponder -

Check/Modification


EASA AD 2012-

0037


FIRE EXTINGUISHER

06-Sep-

2012

EASA SIB 2008-

58R1


SSB0845 Rev IR




FAA, U.S AD 2000-02-25

AFM De-icing 25-jan-00 26-apr-00 N/A Due to paragraph b.

FAA, U.S AD 2000-

09-15 FAA, U.S AD

1 Flight in Icing Condition AFM De-icing FINNISH AD M 2435/97 FINNISH AD M

2786/00 MAI SB 086/74-002 Rev A MAI SB

07-jul-00 02-apr-02 N/A Due to paragraph b.


2012-12-06


80(195)

2000-02-25 093/22-009 MAI SB 096/30-004

MITSUBISHI SB 226 Rev E MITSUBISHI SB 231 Rev B MITSUBISHI SB 232 Rev A

FAA, U.S AD 2003-22-07


16-apr-04 17-May-2004


FAA, U.S AD 2005-14-12

Prop. mounting bolt insp. HARTZELL SB 61-279 ALERT Rev 4 29-jul-05 14-sep-05

FAA, U.S AD 2005-18-20


12-Oct-2005


FAA, U.S AD 2006-13-15


11-aug-06 17-nov-03 c/o in conjunction with vingstudie

FAA, U.S AD 2006-15-07

Safety evaluation (feathering linkage) MAI SB 090/76-003 MITSUBISHI SB 229 24-aug-06 24-aug-06 se Mitsubishi SB 229

FAA, U.S AD 2006-17-01



FAA, U.S AD 2006-17-05

Adjust flight idle fuel flow setting MITSUBISHI SB 234 22-sep-06 27-sep-10

FAA, U.S AD 2007-

17-09


trim


FAA, U.S AD 71-

14-01

Fuel Tank Fungus Coating Peeling 01-May-

1972

01-jan-96 N/A by s/n

FAA, U.S AD 74-

11-01

Windshield Outer Panes COP

2011/09/1 19:37:04

LFV LVA829 Rev A MITSUBISHI SB 163 Rev

B

30-jan-78 16-May-

1974

FAA, U.S AD 75-

16-13



05-aug-75 25-mar-77 Revision C PCW by Swedair.

FAA, U.S AD 75-

16-20

Propeller Pitch Control Lever JCAB AD TCD-1188-75 LFV LVA1012


12-aug-75 20-May-

1975

FAA, U.S AD 78-03-05


180 Rev A

23-feb-78 25-nov-75

FAA, U.S AD 81-

06-01

1 Engine Aft Nacelles 01-apr-81 1 25-May-

1997

Previously complied with

FAA, U.S AD 81-

25-04


003A, SB 043/71-005


FAA, U.S AD 82-

08-02

Electrical Wiring Inspection 15-apr-82 09-feb-82

FAA, U.S AD 83-

08-01

2 To preclude prop. attach bolt failures FINNISH AD M 1168/83 Rev 1 FINNISH AD


28-apr-82 2 20-May-

2005

Ref. MU2B MM chap 13.4 when using bolts P/N

B-3339 only


2012-12-06


81(195)

FAA US AD 83-09-

02

Strobe light assembles 16-Mar-12

FAA, U.S AD 84-

12-04


047/30-001, SB 196A


196 Rev A

28-jun-84 16-feb-84

FAA, U.S AD 84-

25-02

Elevator TrimTab Bracket Insp/Repl.

SB 031/27-005 R1, SB 176E

MAI SB 031/27-005 Rev 1 MITSUBISHI SB

176 Rev E

18-dec-84 23-apr-85

FAA, U.S AD 86-15-03

NLG Strut Assembley LFV LVA1546 MITSUBISHI SB 181 PART 2 Rev B


FAA, U.S AD 86-

20-01


SB 020/34-005, SB 053A

LFV LVD2015 Rev B MAI SR 020/34-005

MITSUBISHI SR 053A

06-Oct-

1986

30-aug-00

FAA, U.S AD 86-

26-02


iceing SB 74-0003, SR 040/74-001

GARRETT SB 74-0003 Rev 6 31-dec-87 09-mar-09 see applicable engine for c/o

FAA, U.S AD 87-

04-03


Insp SB 051/27-007, SB 198

MAI SB 051/27-007 MITSUBISHI SB 198 07-mar-87 29-jul-85

FAA, U.S AD 87-

12-02

Generator Shield Jumper Wires MITSUBISHI SB 201 Rev A 03-jul-87 23-apr-90

FAA, U.S AD 88-

13-01

Bendix Autopilot Disengagement SB

066/22-006

LFV LVD2190 MAI SB 066/22-006 Rev A

MITSUBISHI SB 206

11-jul-98 22-dec-89 N/A N/A due to Autopilot model

FAA, U.S AD 88-

21-01

1 To minimize confusion in

autopilot/manua SB 066/22-006


FAA, U.S AD 88-

23-01


067/27-008, SB 189B

LFV LVD2202 MAI SB 067/27-008 Rev A 04-dec-88 18-May-

1995

FAA, U.S AD 93-

07-11


010


FAA, U.S AD 94-

04-16

Elevator trim tab mod. LFV LVD2537 MITSUBISHI SB 216 11-apr-94 12-Oct-

1993

FAA, U.S AD 94-

11-04


016/61-001


FAA, U.S AD 96-

25-02


4552-96 LFV LVD2749

27-dec-96 12-nov-97

FAA, U.S AD 97-

04-13


1997

N/A N/A due to s/n.

FAA, U.S AD 97-

20-14 CNL


1997

02-dec-98

FAA, U.S AD 97-25-02

To prevent loss of airplane ctrl/overspe


FAA, U.S AD 98-20-39

Forward fitting bolt of wingtip tank SB MU-2 225, 089/57-002A


19-Oct-1998

07-Oct-1997


2012-12-06


82(195)

FAIRCHILD,

Fairchild Aircraft

FAIRCHILD SB 29-

005

2 In Service Hydraulic Leaks FAA, U.S AD 85-04-01 Rev 1 19-Jul-1985 02-jan-00 23-apr-85


Aviation Adm.

FINNISH AD M

2461/97

Avisningens "vervakningsanl,ggning JCAB AD TCD-4626-97 01-aug-97 11-mar-10

FINNISH AD M

2609/98


097/73-001, TCD-4890-98

JCAB AD TCD-4890-98, MAI SB 097/73-

001

12-nov-99 27-sep-10

GARMIN, Garmin

GARMIN SSB

0844

IR Software Version 5.04 EASA SIB2008-58R1 14-nov-08 A 20-May-

2010

GARMIN SSB

0845

IR Software Version 6.04 EASA SIB2008-58R1 14-nov-08 0 20-May-

2010

GARRETT,

AlliedSignal

Aerospace

GARRETT SB 74-0003

6 Replace Ignition Unit AD 74-0003 FAA, U.S AD 86-26-02 25-mar-94 09-mar-09 see applicable engine for c/o

HARTZELL,

Hartzell Propeller

Inc.

HARTZELL SB 61-

256

Propeller mounting bolt inspection MITSUBISHI SL 053/72-003, MITSUBISHI

SL 080

08-feb-02 02-Oct-

2002


4 Prop. mounting bolt insp. FAA, U.S AD 2005-14-12 04-Oct-2005

14-nov-05 Propellerbolts previously checked u/a

HARTZELL SB A61-313

3 Counterweight Slug Bolt Inspection EASA SIB2008-88 , FAA, U.S AD 2009-10-14

15-jul-09 3 20-sep-10 N/A by SSB 0844

HARTZELL SI 140A 9 Installation of Mounting Bolt FAA, U.S AD 83-08-01 Rev 2, LFV LVA1424 Rev A



2012-12-06


83(195)


Bureau

JCAB AD TCD-

0518-68

Rivet holes elevator hinge fitting 06-Feb-

1968


JCAB AD TCD-

0642-70

AFM revision regarding fuel spec. LFV LVA439 MITSUBISHI SB 112 Rev C 07-feb-70 30-jun-89

JCAB AD TCD-0643-70

Adjustment of fuelquantitygauge LFV LVA438 MITSUBISHI SB 114 07-feb-70 15-jul-04 N/A by s/n

JCAB AD TCD-

0652-70


JCAB AD TCD-

0653-70

Engine Nacelle Tail Area-Modification

of


JCAB AD TCD-

0660-70

Replacement of bearing in

nosegearstrut

LFV LVA457 MITSUBISHI SB 123 01-May-

1970


JCAB AD TCD-

0730-1-72


B


JCAB AD TCD-

0730-2-86


JCAB AD TCD-

0859-72

Mod. of electrical system LFV LVA645 MITSUBISHI SB 156 04-sep-72 10-sep-72 N/A N/A due to s/n.

JCAB AD TCD-

0866-72


1972


JCAB AD TCD-

0947A-74


A

12-nov-74 16-May-

1974

N/A N/A due to s/n.

JCAB AD TCD-

0948A-1-78


JCAB AD TCD-

0948A-74

Inspektion av frontrutor LFV LVA829 Rev A MITSUBISHI SB 163 Rev

B

07-Oct-

1974

16-May-

1974

JCAB AD TCD-

1001A-76

Insp./repl. of elevator trim tab rod LFV LVA886 Rev A MITSUBISHI SB 176 Rev

E

06-Oct-

1976

23-apr-85

JCAB AD TCD-

1001B-2-84

Replacement of Elevator Trim Tab

Bracket


MITSUBISHI SB 176 Rev E

12-dec-84 23-apr-85

JCAB AD TCD-

1094A-76

Insp. of wingflap controlsystem FAA, U.S AD 75-16-13 LFV LVA1011 Rev A

MITSUBISHI SB 167 Rev D

06-sep-76 25-mar-77 Revision C PCW by Swedair.

JCAB AD TCD-1188-75


06-May-1975

20-May-1975

JCAB AD TCD-1202-75

Engine Cowling Latches FAA, U.S AD 78-03-05 LFV LVA1014 Rev A MITSUBISHI SB 171 Rev B MITSUBISHI SB

180 Rev A



2012-12-06


84(195)

JCAB AD TCD-

1209-75

Insp/mod of NLG shimmydamper

locking

LFV LVA1013 MITSUBISHI SB 169 Rev B 16-jun-75 16-jun-75

JCAB AD TCD-

1235-75


emerg.cables

LFV LVA1083 MITSUBISHI SB 170 Rev A 19-sep-75 30-jun-89 N/A N/A due to model.

JCAB AD TCD-

1272-75


Mech.-I&M




JCAB AD TCD-

1328-76

Fire hazard in rear baggage

compartment


JCAB AD TCD-

1353-76


Repl.


JCAB AD TCD-

1370-76

Inspect strobelight conduit in Tiptank LFV LVA1196 18-Oct-

1976

22-dec-89 Part.1

JCAB AD TCD-

1379-1-80


heatdamage


Rev B

06-feb-02 25-May-

1977


JCAB AD TCD-

1520A-77


JCAB AD TCD-

1768-1-85

Fatigue failure of the NLG strut assy. LFV LVA1546 MITSUBISHI SB 181 PART 2

Rev B

12-jul-85 15-jul-04 PCW Found SB 181 part 2 PCW.

JCAB AD TCD-

1817-79

Modification of bagagecompartment LFV LVA1583 MITSUBISHI SB 182 05-feb-02 11-feb-80 N/A N/A due to s/n.

JCAB AD TCD-

2048-81


circuit


1981

N/A N/A due to s/n.

JCAB AD TCD-

2070-81

Inspect NLG downlock mechanism LFV LVA1753 MITSUBISHI SB 188 05-feb-02 02-sep-81

JCAB AD TCD-

2113-82


harness

LFV LVA1788 MITSUBISHI SB 191 06-feb-02 09-feb-82

JCAB AD TCD-

2252-2-88


TCD-2252-1-87

01-feb-89 24-mar-09 PCW

JCAB AD TCD-

2252-83

Flapcontrolsystem torquetubes LFV LVA1873 MITSUBISHI SB 189 Rev C 04-feb-83 18-May-

1995

JCAB AD TCD-

2263-83





JCAB AD TCD-2342-84


LFV LVA1942 MITSUBISHI SB 196 Rev A 06-feb-02 16-feb-84




2012-12-06


85(195)

JCAB AD TCD-

2451-1-87


1987


JCAB AD TCD-

2451-85



LFV LVD2037 MITSUBISHI SB 198 30-sep-85 29-jul-85

JCAB AD TCD-

2545-1-88

Generator System LFV LVD2191 MITSUBISHI SB 201 Rev A 01-jul-88 23-apr-90



01-feb-97 22-nov-01

JCAB AD TCD-

3378-90


leadingedge

LFV LVD2338 MITSUBISHI SB 211 28-mar-91 14-jul-04 N/A N/A by s7n.

JCAB AD TCD-

3393A-96



25-May-

1996

31-May-

2010

JCAB AD TCD-

3464-91

Unintentional engagement of A/P...... 17-jun-91 24-mar-09 N/A by model

JCAB AD TCD-

3740A-98


MSB 216, 228 LVD 2898


LVD2898 MITSUBISHI SB 216 MITSUBISHI

SB 228

17-aug-98 25-mar-99

JCAB AD TCD-3901-93


10-sep-93 01-mar-94



28-nov-94 08-mar-95

JCAB AD TCD-3942-94


JCAB AD TCD-

4310-96


MITSUBISHI SB 225

01-apr-96 07-Oct-

1997

JCAB AD TCD-

4379-96


MITSUBISHI SB 229

01-apr-96 30-jul-96

JCAB AD TCD-

4552-96


JCAB AD TCD-

4625-97


093/22-009

14-jul-97 02-apr-02

JCAB AD TCD-

4625A-2001

Mod of trim system/AFM revision LFV LVD3122 MITSUBISHI SB 231 Rev B 16-mar-01 02-apr-02 PCW Ref AMOC LFV Appr M15/01, TDM 01-45

JCAB AD TCD-

4626-97



01-May-

1997

14-jul-04 PCW

JCAB AD TCD-

4684-97


MITSUBISHI SB 230

01-jun-97 25-mar-99

JCAB AD TCD-

4753-98


2922,FAA AD 97-20-14, MHI SN 117A





2012-12-06


86(195)

JCAB AD TCD-

4753A-2004

Icing-related incidents VIDEO FAA, U.S AD 2003-22-07 Rev 1 24-feb-04 17-May-

2004


JCAB AD TCD-

4838-98


train


MITSUBISHI SB 235


JCAB AD TCD-

4889-2-2007

Inappropriate calib. of eng. trq-meter MITSUBISHI SB 233 Rev B 21-jun-07 11-sep-07 Previously carried out, ref. SB 233A.

JCAB AD TCD-4889-98

Insp. of Engine Torque Indication System LFV 2924, MU SB 233

FINNISH AD M 2608/98 LFV LVD2924 MITSUBISHI SB 233 Rev B

05-nov-98 14-jul-04 PCW

JCAB AD TCD-

4890-98


SB 234


MITSUBISHI SB 234

04-nov-98 27-sep-10

JCAB AD TCD-

5030-99


1999


JCAB AD TCD-

5432-2000


JCAB AD TCD-

5547-2001


JCAB AD TCD-

5747-2001

Inspection of Tip Tank Brackets LFV LVD3166 MITSUBISHI SB 236 12-sep-01 11-Oct-

2001

JCAB AD TCD-

5864-2001

Flap Drive Train Inspection LFV LVD3212 MITSUBISHI SB 237 27-dec-01 16-May-

2002

JCAB AD TCD-

6127-2003

Pneumatic Line insp. LFV LVD3322 MITSUBISHI SB 239 17-mar-03 14-nov-03

JCAB AD TCD-

7030-2006


Hardware


LFV,

Luftfartsverket



05-feb-02 A 25-mar-77 Revision C PCW by Swedair.

LFV LVA 1012 Kontroll av propellerreglagets

montering



05-feb-02 20-May-

1975

LFV LVA 1013 Kontr. och mod. av låsning på nosställ JCAB AD TCD-1209-75 MITSUBISHI SB 169

Rev B

05-feb-02 16-jun-75


låsanordning



05-feb-02 A 25-nov-75

LFV LVA 1083 Insp. & utbyte av lina för nödöppning JCAB AD TCD-1235-75 MITSUBISHI SB 170 Rev A

05-feb-02 30-jun-89 N/A N/A due to s/n.


2012-12-06


87(195)


bak.motorpl.


177 Rev B

06-feb-02 A 25-May-

1977



trimrod




06-feb-02 15-mar-84



n"dstr"mskret


Rev B


LFV LVA 1753 Kontroll av låsmekanism i nosställ JCAB AD TCD-2070-81 MITSUBISHI SB 188 05-feb-02 02-sep-81


motor COP 2011/09/1 19:37:04

JCAB AD TCD-2113-82 MITSUBISHI SB 191 06-feb-02 09-feb-82


Rev C

06-feb-02 18-May-

1995

LFV LVA 1942 Momentdragning/låsn.av koppl.i

varmlufts


Rev A

06-feb-02 16-feb-84



bränslespec.


Rev C

05-feb-02 30-jun-89


LFV LVA 457 Utbyte av lager i nosst,llets st"td,mp. JCAB AD TCD-0660-70 MITSUBISHI SB 123 05-feb-02 26-mar-09 N/A by s/n


LFV LVA 645 Modifiering av el-system JCAB AD TCD-0859-72 MITSUBISHI SB 156 05-feb-02 08-dec-09 N/A by A/C serial number


LFV LVA 828 A Kontr. & mod. av klaffdrivning JCAB AD TCD-0947A-74 MITSUBISHI SB

162 Rev A

05-feb-02 A 16-May-

1974

N/A N/A due to s/n.

LFV LVA 829 A Inspektion av frontrutor FAA, U.S AD 74-11-01 FAA, U.S AD 75-03-


163 Rev B

05-feb-02 A 26-mar-09

LFV LVA 886 A Kontroll/byte av höjdtrimroderarmar JCAB AD TCD-1001A-76 05-feb-02 A 23-apr-85


höjdtrimroder


LFV LVD 1971 Elevator Trim Tab MU2 SB 176E JCAB AD TCD-1001B-2-84 MITSUBISHI SB

176 Rev E

18-jan-85 23-apr-85


2012-12-06


88(195)

LFV LVD 2015 B Pitot Tube Wiring MAI SR 020/34-005

Rev A, MHI SR 53


2450A-87

24-May-

1985

B 20-May-

1986

LFV LVD 2037 Flap Flexible Shaft MU2 SB 198 JCAB AD TCD-2451-85 MITSUBISHI SB 198 30-sep-85 29-jul-85

LFV LVD 2069 Altimeter 25-mar-86 22-dec-89 N/A N/A by p/n & s/n


26-jan-87 15-jan-88

LFV LVD 2190 Autopilot Switch MU2 SB 066/22-006

och SB 206

FAA, U.S AD 88-13-01 MAI SB 066/22-006

Rev A MITSUBISHI SB 206

19-aug-88 22-dec-89 N/A Bendix A/P ej installerad

LFV LVD 2191 Generator System MU2 SB 201A JCAB AD TCD-2545-1-88 MITSUBISHI SB

201 Rev A

19-aug-88 28-sep-89



08-dec-88 18-May-

1995

LFV LVD 2206 Modifiering av Autopilot FAA, U.S AD 88-21-01 Rev 1 08-Dec-1988 12-feb-02

LFV LVD 2338 Kont./Mod.av sidorodrets trimroderframka Mitsubishi MHI SB

211



212A


212 Rev A

29-May-

1996

1 31-May-

2010


CHPT 9

23-May-

1991



216


216

03-dec-92 12-Oct-

1993

LFV LVD 2477 Electric Trim System AD930711, MU

SB 079/27-0-010


LFV LVD 2512 TIP TANK INST. (NXT 100H) JCAB AD TCD-3901-93 MITSUBISHI SB 221 02-dec-93 01-mar-94


216

FAA, U.S AD 94-04-16 MITSUBISHI SB 216 07-apr-94 12-Oct-1993

LFV LVD 2538 Byte Låspinne i landställets nödutf. SB

219


Rev A

07-apr-94 08-mar-95


LFV LVD 2592 Insp/Repl. of Lock-pin in L/G gearbox

TCD-3942-1-94, MSB 219A


219 Rev A

09-feb-95 08-mar-95

LFV LVD 2688 Kontr/byte av infästn.bult för tiptank

MU-2 SB 225



09-May-

1996

07-Oct-

1997


2012-12-06


89(195)


MU-2 SB 229


1996

30-jul-96




261 Rev 1

27-sep-96 16-May-

2002

Prop. BU10873 utbytt samt mod. till BUA


4552-96


96

21-jan-97 12-feb-02

LFV LVD 2761 Installation av autoignition system TCD-2679A-97

JCAB AD TCD-2679A-97 MITSUBISHI SB 226 Rev E

14-feb-97 26-mar-99

LFV LVD 2769 Demont.av backventil i

bränslesystemets MU-2 SB 130A

FAA, U.S AD 97-04-13 MITSUBISHI SB 130

Rev A

18-mar-97 05-May-

1997

N/A N/A due to s/n.

LFV LVD 2800 Mod. av De-ice Monitoring System

Mitsubishi SB 232, TCD-4626-97


Rev A

28-aug-97 27-May-

1998

LFV LVD 2819 Mod.av lagerboxar för

landställssystem Mitsubishi SB 230

JCAB AD TCD-4684-97 MITSUBISHI SB 230 18-nov-97 22-jan-98


nödutgång

23-mar-98 21-jan-11

LFV LVD 2897 Kontroll av landst,llets drivsystem

TCD-4838-98, SB 235


LFV LVD 2898 Mod. av autopilotens höjdtrimsystem

TCD-3740A-98, SB 216, 228



27-aug-98 12-mar-99

LFV LVD 2922 Änd.av Flyghandbok-Extra krav på

typutbi TCD-4753-98, MHI SN 117A

JCAB AD TCD-4753-98 MITSUBISHI SN 117

Rev D


LFV LVD 2924 Kontr/Just av motorernas Torque

indikeri MHI SB 233, TCD-4889-98


Rev B

01-dec-98 27-sep-99 SB 233A C/Out.

LFV LVD 2925 Kontr/just av mot bränsleflöde Flight

Id MHI SB 234

JCAB AD TCD-4890-98 MITSUBISHI SB 234 01-dec-98 27-sep-10

LFV LVD 2988 Sprickkontroll av kroppsspant JCAB AD TCD-5030-99 MITSUBISHI SB 209

Rev B



LFV LVD 3122 Modifiering av autopilotsystemet JCAB AD TCD-4625A-2001 MAI SB 093/22-

009 MITSUBISHI SB 231 Rev B NYGE TDM01-45

02-apr-01 02-apr-02 Ref AMOC LFV Appr M15/01, TDM 01-45


LFV LVD 3166 Sprickkontroll av infästning till ving-spetstank


20-sep-01 11-Oct-2001

LFV LVD 3212 Kontroll av vridaxel till vingklaff. JCAB AD TCD-5864-2001 MAI SB 099/27-012 MITSUBISHI SB 237

09-jan-02 16-May-2002

LFV LVD 3322 Kontroll av tryckluftsledningar JCAB AD TCD-6127-2003 MITSUBISHI SB 21-mar-03 14-nov-03


2012-12-06


90(195)

239


Internation

MAI SB 047/30-001



19-jul-84 A 16-feb-84

MAI SB 051/27-

007

Add.Seal and Flap Flexible Shaft

Torque AD 87-04-03, SB 198

FAA, U.S AD 87-04-03 01-feb-85 29-jul-85

MAI SB 067/27-

008

A Insp/Repl. of Flap Control System

Torque AD 88-23-01, SB 189B

FAA, U.S AD 88-23-01 LFV LVD2202 29-mar-95 A 18-May-

1995

MAI SB 069/24-

006

Split Radio Bus Inspection and

Rework

MAI SB 066/22-006 Rev A 17-nov-88 22-dec-89 N/A N/A due to Aircraft s/n

MAI SB 089/57-

002

A Insp/Repl. of Bolts for Wing Tip Tank FAA, U.S AD 98-20-39 05-nov-96 A 07-Oct-

1997

N/A N/A due to s/n.

MAI SN 110/00-

017A


MAI SN 111/77-

004


Potential


MAI SR 020/34-005

Anti Ice Capability AD 86-20-01, SR 053A

FAA, U.S AD 86-20-01 LFV LVD2015 Rev B MITSUBISHI SR 053A

06-Oct-1986

30-aug-00 N/A N/A due to s/n.


MITSUBISHI MSR

066 B

**RECOVERED RECORD** B 15-jan-88

MITSUBISHI SB

066

Bendix M4D 18-dec-87 28-sep-89

MITSUBISHI SB

076/22-008

M-4() Autop.Engage Switch Guard Install. 11-apr-91 12-apr-95 N/A

MITSUBISHI SB

112


1971

C 30-jun-89

MITSUBISHI SB 114

Fuel Quantity Indicator Readjustmnet JCAB AD TCD-0643-70 LFV LVA438 01-jan-70 15-jul-04 N/A N/A by s/n.

MITSUBISHI SB 119

The Bolt and Bolt Hole Diam. of Nose L.G JCAB AD TCD-0652-70 LFV LVA456 10-mar-70 26-mar-09 N/A by model

MITSUBISHI SB 123

Bearing,Oleo Strut,Nose L.G. -Repl. of JCAB AD TCD-0660-70 LFV LVA457 01-apr-70 26-mar-09 N/A by s/n

MITSUBISHI SB Scissors Switch,Nose L.G. -Install. of 31-aug-70 30-jun-89 N/A


2012-12-06


91(195)

124

MITSUBISHI SB

128


MITSUBISHI SB

143

B Top Coating, Wing Integral Main F.T.-SIo JCAB AD TCD-0730-1-72 JCAB AD TCD-

0730-2-86


MITSUBISHI SB

162

A Flex. Shafts, Flap Control Sys.-Insp. of

(AD750201)

JCAB AD TCD-0947A-74 LFV LVA828 Rev A 03-Oct-

1974

A 16-May-

1974

N/A

MITSUBISHI SB

163

B Insp. of Outer Pane, Front Winds. & Inst FAA, U.S AD 74-11-01 JCAB AD TCD-

0948A-1-78 JCAB AD TCD-0948A-74 LFV LVA829 Rev A

16-nov-78 16-May-

1974

MITSUBISHI SB 165

A Lubr. Interval,Wheel Bearing,Main & Nose

24-jul-80 29-jul-74 N/A

MITSUBISHI SB

166

Wing Flap 24-jul-80 08-jan-75

MITSUBISHI SB

167

D

Flap M.Jack Screw-Insp. of and/or Main

G


1094A-76 LFV LVA1011 Rev A

24-jul-80 D 25-mar-77 Revision C PCW by Swedair.

MITSUBISHI SB

168

A Propeller Pitch Control Lever-Insp. of

(AD761620)


75 LFV LVA1012

24-jul-80 A 20-May-

1975

MITSUBISHI SB

169

B Shimmy Damper-Insp. and Modification

of


MITSUBISHI SB

170

A MLG Forward Door Em.Op. Cable-Insp. &

Re (AD762204)

JCAB AD TCD-1235-75 LFV LVA1083 24-mar-77 A 30-jun-89 N/A N/A due to s/n

MITSUBISHI SB 171



17-nov-77 B 25-nov-78

MITSUBISHI SB 173

A Drag Strut, Main L.G.-Modification of JCAB AD TCD-1284-1-76 24-jul-80 05-mar-76


C Tip Tank Conduit Tube-Insp.of,and Rew.of (AD830902)

FINNISH AD M 1177/83 JCAB AD TCD-1370A-81 LFV LVA1196

02-Oct-1981

C 18-jun-10

MITSUBISHI SB 175

Barrel Nut, Inner/Outer Wing Conn.-Repl.

JCAB AD TCD-1353-76 26-jun-76 01-sep-09 N/A by s/n

MITSUBISHI SB 176

E Elevator Trim Tab Bracket-Repl. of LVD1971, AD 84-25-02, SB 031/27-005R1

FAA, U.S AD 84-25-02 FINNISH AD M 1080/82 JCAB AD TCD-1001A-76 JCAB AD

TCD-1001B-2-84 LFV LVD1971

26-sep-84 E 23-apr-85

MITSUBISHI SB

177

B Mod. of Engine Nacelle Tail Area

(AD810601)


A

11-sep-80 B 25-May-

1977


MITSUBISHI SB 179

Rodd Assem., Engine Nacelle Upper D.-R&M

27-May-1977

22-dec-89

MITSUBISHI SB 180

A Link, Engine Nacelle Upper D.-Repl. of (AD780305)

FAA, U.S AD 78-03-05 JCAB AD TCD-1202-75 JCAB AD TCD-1520A-77 LFV LVA1014

17-nov-77 A 09-May-1978


2012-12-06


92(195)

Rev A

MITSUBISHI SB

181 PART 2

B Insp. and Repl. of Nose L.G. Strut Assem

(AD801812)


1-85 LFV LVA1546

08-apr-85 B 15-mar-84

MITSUBISHI SB

182

Add. of Ceiling Cover, Rear Bagg. Comp. JCAB AD TCD-1817-79 LFV LVA1583 16-nov-79 16-nov-79 N/A N/A due to s/n.

MITSUBISHI SB

184

Turnbuckle, Control Cables -Repl. of 04-apr-80 15-dec-89

MITSUBISHI SB

188

Down Lock Mech., Nose L.G.-Insp. of JCAB AD TCD-2070-81 LFV LVA1753 13-jul-81 02-sep-81

MITSUBISHI SB

189

C Flap Control Torque Tube AD 88-23-01,

SB 067/27-008


2252-1-87 JCAB AD TCD-2252-83 LFV LVA1873 LFV LVD2202

28-jun-94 C 18-May-

1995

MITSUBISHI SB

190

A Trav. Nut Repl. of L.G. Mech. Stop Assem 28-jun-94 17-jan-84

MITSUBISHI SB

191

Engine El. Wire-Insp. and Replacement

of (AD820802)

JCAB AD TCD-2113-82 LFV LVA1788 21-dec-81 09-feb-82

MITSUBISHI SB

193

B Landing Gear Warning Horn Syst.Modif. 15-jun-94 B 04-dec-00 Rev A är utförd.

MITSUBISHI SB

194

Master Cauting Light Visibility-Impr. of 23-aug-82 30-May-

1983

MITSUBISHI SB

196

A Ret. of coupling nut on the bleed air tu

AD 84-12-04, SB 047/30-001



12-apr-84 A 16-feb-84

MITSUBISHI SB

198

Add. Seal & Torque Insp. of Flap Flex.Sh

LVD2037, AD 87-04-03, SB 051/27-007


85 LFV LVD2037

13-feb-85 29-jul-85

MITSUBISHI SB

199

A Engine Lubricating Tubing Insp. & Protec 24-jun-94 A 06-nov-09 PCW

MITSUBISHI SB

200

B Insp of Nose Ldg Gear Drag Strut Link 24-jun-94 A 17-feb-88

MITSUBISHI SB

201

A Generator Circuit Wires Insp. and Mod. FAA, U.S AD 87-12-02 JCAB AD TCD-2545-

1-88 LFV LVD2191

02-mar-88 A 23-apr-90

MITSUBISHI SB

204

Speed Placard Change 03-mar-87 23-apr-90

MITSUBISHI SB

206

Bendix Autop.Disengagement Method

Stand.


1-97 LFV LVD2190

13-Oct-

1987


MITSUBISHI SB 207

Rudder T.T. & Elevator T.T. Insp. & Rep. 20-May-1988

14-jan-10

MITSUBISHI SB 209



2012-12-06


93(195)

MITSUBISHI SB

210


MITSUBISHI SB

211

Rudder Trim Tab Modification (LVD

2338)

JCAB AD TCD-3378-90 LFV LVD2338 20-nov-90 14-jul-04 N/A N/A by s/n.

MITSUBISHI SB

212

A Insp of Anti-ice/Deice Systems (LVD

2347),

JCAB AD TCD-3393A-96 LFV LVD2347 Rev

1

25-apr-96 A 31-May-

2010

MITSUBISHI SB 214

Engine Control Rod Inspection 06-dec-91 08-apr-92

MITSUBISHI SB

215

Removel of Prop. Governor Speed Signal 23-Oct-

1991

17-feb-92 N/A N/A due to -1 engine

MITSUBISHI SB

216

Elevator Trim Tab Installation (LVD 2450 FAA, U.S AD 2007-17-09 FAA, U.S AD 94-

04-16 JCAB AD TCD-3740A-98 LFV

LVD2450 LFV LVD2537 LFV LVD2898

11-sep-92 12-Oct-

1993

MITSUBISHI SB

218

A Propeller Feathering Linkage Inspection 17-jan-94 A 01-mar-94

MITSUBISHI SB

219

A Emergency Gear Down G.box Lower Pin

Repl

JCAB AD TCD-3942-1-94 JCAB AD TCD-

3942-94 LFV LVD2538 LFV LVD2592

24-Oct-

1994

A 08-mar-95

MITSUBISHI SB 221

Tip Tank Conduit Tube Insp. and Rep. JCAB AD TCD-3901-93 LFV LVD2512 10-aug-93 01-mar-94

MITSUBISHI SB 222

Fuselage Waterproof Modification SR 019

28-jun-94 27-Oct-1998

MITSUBISHI SB 223

Pitot/Static System Improvement SR 064 MITSUBISHI SR 053A MITSUBISHI SR 064 28-jun-94 30-aug-00

MITSUBISHI SB

224

C Acrylic Windsheild/Window glass Insp.

UHB



30-apr-98 C 18-jun-10

MITSUBISHI SB

225

Forward fitting bult of wingtip tank LVD

2688


2351/96 JCAB AD TCD-4310-96 LFV

LVD2688

29-sep-95 07-Oct-

1997

MITSUBISHI SB 226


FAA, U.S AD 2000-09-15 Rev 1 FAA, U.S AD 86-26-02 FINNISH AD M 2435/97

FINNISH AD M 2786/00 JCAB AD TCD-2679A-97 LFV LVD2761 MAI SB 086/74-

002 Rev A

18-sep-01 E 22-nov-01 PCW no further action (rev.E) required due to s/n.

MITSUBISHI SB

227

Rudder Torque Tube Modification 20-dec-96 04-sep-97

MITSUBISHI SB 228


FAA, U.S AD 2007-17-09 FINNISH AD M 2581/98 JCAB AD TCD-3740A-98 LFV

LVD2898

13-jul-98 25-mar-99 Visuell kontroll utförd SB införd

MITSUBISHI SB

229

Feathering Valve/Linkage Insp. FAA, U.S AD 2006-15-07 JCAB AD TCD-

4379-96 LFV LVD2689

20-feb-96 17-apr-98


2012-12-06


94(195)

MITSUBISHI SB

230

Mod.of Bearing Box Ldg. Gear Act. LVD

2819

JCAB AD TCD-4684-97 LFV LVD2819 05-mar-97 22-jan-98

MITSUBISHI SB

231

B Inst.of Trim-In-Motion Alert System FAA, U.S AD 2000-09-15 Rev 1 FINNISH AD

M 2460/97 UPPHÄVD FINNISH AD M 2786/00 JCAB AD TCD-4625A-2001 LFV LVD3122 MAI SB 093/22-009 NYGE

TDM01-45

11-dec-02 B 03-mar-03 SL 079 performed earlier.

MITSUBISHI SB

232

A De-Ice System Modification LVD 2800,

TCD-4626-97

FAA, U.S AD 2000-09-15 Rev 1 FINNISH AD

M 2786/00 JCAB AD TCD-4626-97 LFV LVD2800 MAI SB 096/30-004


MITSUBISHI SB 233

B Insp.of Engine Torque Indication System. TCD-4889-98, LFV 2924

FAA, U.S AD 2006-17-01 FINNISH AD M 2608/98 JCAB AD TCD-4889-2-2007 JCAB AD TCD-4889-98 LFV LVD2924


MITSUBISHI SB 234

Fl.Check of the Flight Idle Fuel Flow Se TCD-4890-98, LVD 2925


07-Oct-1998

27-sep-10

MITSUBISHI SB 235

Inspection of landing gear power train JCAB AD TCD-4838-98 LFV LVD2897 04-aug-98 24-mar-09 N/A by model

MITSUBISHI SB 236

Inspection of Tip Tank Brackets JCAB AD TCD-5747-2001 LFV LVD3166 28-aug-01 11-Oct-2001

MITSUBISHI SB 237

Inspection of Flap Drive Train JCAB AD TCD-5864-2001 LFV LVD3212 13-dec-01 16-May-2002

MITSUBISHI SB 238


MITSUBISHI SB 239

Pneumatic Line Insp. and Modification JCAB AD TCD-6127-2003 LFV LVD3322 26-dec-02 14-nov-03

MITSUBISHI SB

240

Inst.of Trottle Quadrant Placard 26-feb-03 14-nov-03

MITSUBISHI SB

241


Hardware


7030-2006


MITSUBISHI SL

060

System 17-feb-89 07-jul-91

MITSUBISHI SL

078

Automatic Autopilot Disconnect System 28-jan-02 31-May-

2010

MITSUBISHI SL

079

Diode inst.in Flap Position Ind.Curcuit 28-jan-02 02-apr-02

MITSUBISHI SL 080

Hartzell Propeller Mounting Bolt Insp. HARTZELL SB 61-256 05-apr-02 02-Oct-2002

MITSUBISHI SL 084

Pneumatic De-Ice Monitoring System 14-jun-04 31-May-2010


2012-12-06


95(195)

MITSUBISHI SL

085


2005

14-sep-05

MITSUBISHI SN

053

B Rudder Torque Tube AD 86-20-01, SB

020/34-005

05-nov-86 B 22-dec-89

MITSUBISHI SN

117

D

Icing Awareness Training Video FAA, U.S AD 2003-22-07 Rev 1 JCAB AD

TCD-4753-98 LFV LVD2922

14-jun-04 D 17-May-

2004

MITSUBISHI SN 146

Water Ingress into Vertical Stabilizer 19-dec-03 06-mar-04

MITSUBISHI SN

148


MITSUBISHI SN

156A


MITSUBISHI SN

157

Torque Indicating System Shift Potential 20-nov-08 11-mar-09 SB 233 considered

MITSUBISHI SN

161

Repl Air Filter for Vacuum System MITSUBISHI STCSA01913SE 09-dec-09 11-mar-10

MITSUBISHI SR

053A

Modifiering av pitotrör FAA, U.S AD 86-20-01 JCAB AD TCD-

2450A-87 LFV LVD2015 Rev B MAI SR 020/34-005 MITSUBISHI SB 223

23-Oct-

1984

20-May-

1986

MITSUBISHI SR 064

Pitot & Static System MITSUBISHI SB 223 30-apr-85 30-aug-00

MITSUBISHI SR 065

Warning Horn 20-jan-86 22-dec-89

MITSUBISHI SR

067

Emergency Exit Placard 17-sep-85 03-feb-88

MITSUBISHI SR

072

Air Filter Replacement for Vacuum Syst. 25-apr-00 17-nov-03

MITSUBISHI SR

075

Inst. tip tank placard 29-Oct-

2004

24-feb-05

MITSUBISHI STC

SA01913SE


NARCO, Narco

NARCO SB ELT10-16


NYGE, Saab Aerotech

Aircraft Services


2012-12-06


96(195)

NYGE TDM 00-23 Wiring Left Wing ADRIAN 22-dec-00 22-dec-97

NYGE TDM 01-45 Installation of Trim-In-Motion Alert Syst.

and Automatic A/P Disconnect syst.



07-May-

2001

02-apr-02

NYGE TDM 02-10 Installation of TPE331-6-252M Engines 25-mar-02 16-May-

2002

NYGE TDM 02-24 Installation Moving MAP 10-Oct-

2002

30-Oct-

2002


NYGE TDM 02-33 Viktminskning MU-2B 24-dec-02 27-jan-04

NYGE TDM 03-08 8 GNS430/530 & MODE S GTX330 install. 04-mar-03 20-Oct-2008

NYGE TDM 03-11 C Astor 2 MU-2B 19-mar-03 C 05-nov-03 Original compliance was as per TDM rev A.The A/C installation is IAW rev C as not affected by rev B and C.F01323, F01346, F01348


NYGE TDM 03-28 F Nav Demo Pod 19-dec-03 F 10-jan-10 Original compliance by Rev D. Not affected by rev F.


NYGE TDM 06-28 A Removable FR-31 29-jun-07 A 15-jun-07




NYGE TDM 08-03 A Enhanced Surveillance MU-2B 28-feb-08 A 14-jan-10

NYGE TDM 08-28 B ELT 406 MU-2B 29-sep-08 B 20-Oct-2008

Original compliance with TDM rev A. Rev B does not affect previous complaiance.

NYGE TDM 09-23 A Electrical Wiring Feed Through 08-sep-09 A 10-jan-10

NYGE TDM 09-28 A GPS Splitter 12-Oct-2009

A 15-jan-10

NYGE TDM 10-25 A MU-2B Terminating Resistor 08-apr-10 A 18-May-2010

C/W

NYGE TDM 11-32 A MU-2B-20/26 Alteration oil hose A 18-May-12



2012-12-06


97(195)

NYGE TDM 12-21 A Avinstallation IK 26-Sep-

2012

NYGE TDM 12-28 A Alteration of rivet with bolt A 18-May-12

NYGE TDM 90-09 Rep. Sprickor undre vingpanel 23-aug-90 15-sep-90

NYGE TDM 95-04 4 Vingstudie 20-sep-98 4 17-nov-03

NYGE TDM 96-06 Rep. sprickor "hinge,front spar flange" 11-nov-96 14-nov-96


NYGE TDM 97-03 Astor MU-2 25-feb-97 01-sep-97


1998

17-jul-98

NYGE TDM 99-03 Install. Auto Ignition 03-mar-99 26-mar-99

NYGE TVO 1/09 Inspektion av Stringers & struktur vinge 25-feb-09 01-apr-09 Inspected with remarks

NYGE TVO 1/93 Low Volt Warning Light (BCL) 22-jan-93 24-jun-93

NYGE TVO 1/96 Slitage Flap Guide Rail 12-apr-96 26-nov-99

NYGE TVO 1/97 3 De-Icertank MU-2B, korrosionskontroll 12-feb-97 04-sep-97

NYGE TVO 2/00 Märkning av infästning domkraft Mu2 01-dec-00 08-May-2001

NYGE TVO 2/07 A Prevent FR31 radio to xmit when RM2 off

06-feb-07 A 28-feb-07

NYGE TVO 2/91 A/C Elecrical System 10-jan-91 10-jun-91

NYGE TVO 3/96 3 Wing Spar Flange Inspection. 24-feb-05 3 14-jan-10

NYGE TVO 4/11 A Static inverter control 15-Dec-11

NYGE TVO 4/86 2 Wing Pod Inspection 06-apr-92 2 31-May-

2010

NYGE TVO 4/91 Special Inspection (next E6.) 19-feb-91 10-jun-91

NYGE TVO 4/92 Engine Install. Kontr. rörledningar 29-apr-92 17-aug-92

NYGE TVO 4/94 3 Fwd. Wing Tiptank Attachment 28-sep-94 3 14-jan-10 L/H & R/H

NYGE TVO 4/96 Kontroll av Lagerhus i noshjulsstyrning. 25-Oct-1996

16-dec-96 Utförd tidigare (ref. Ove N.lista)

NYGE TVO 6/88 Allm. instruktion för metallpropeller 13-jun-88 27-sep-10


2012-12-06


98(195)


1992

02-feb-93

NYGE TVO 7/93 Starter Drive Splines 01-nov-93 31-aug-94

NYGE TVO 8/04 Kontr. av Spant vid bakre feninfästning 08-dec-04 14-jan-10

NYGE TVO 8/92 Wheel Parts 27-Oct-1992

08-mar-93

NYGE TVO 9/88 Emergency Extension System 08-aug-88 18-dec-89

PIPER, The New Piper

Aircraft Inc.

PIPER SB 700 A Nose Wheel Insp/Replacement FAA, U.S AD 97-07-03 12-Oct-

1981

05-May-

1997

N/A


2012-12-06


99(195)

2.4 GFE Aircraft Mitsubishi MU-2 SE-GHD


Number:


total Hours:

Total

Landing

Cycles:

Date

Reference:

MU-2B-20 293 SE-GHD 11316 6411 2012-11-23


Serial

Number:

Total Hours

Since New:

Total

Cycles

Since New:

Hours remaining to

Overhaul/HIS/GBl:

Left Engine P20038 9616 10264 4228/628/2428

Right Engine P20052 11551 11102 3444/1642/1644


Left Propeller HC-B3TN-5E BVA 6817 At overhaul 2012-11-23

Right Propeller HC-B3TN-5E BVA 7713 At overhaul 2012-11-23













Airspeed Indicator LH / RH Aerosonic 065A-986402-003 /

20040-161


Altimeter incl. encoder RH ARC 42540-3228





2012-12-06


100(195)


LH

Century 52C77











GPS MAP


Laser Prism

Wing Pylon


EW system

ADRIAN Pod mounted system RH Wing Pylon

Target Towing

MBV7S Inboard winch



System:


Adrian C & S General Signal Harness AWG22 shielded x 44


AC Power

115/200VAC 400 Hz 3-

Phase 3 x 10 A

AWG 16 x 4

twisted

AWG 16 x 2

AWG 20 x 2 Adrian C & S DC Power 28 VDC 200

A

AWG 2 x 2

Prepared installation Ethernet LAN Cable


2012-12-06


101(195)



2012-12-06


102(195)


rd 2012.


Aircraft SE-GHD

Vingstudie MU-2 AMP 2009-03-27 11158 12158,8















Engine S/N P-20052




Propeller L/H O/H (not installed) AMP

Propeller R/H O/H (not installed) AMP


2012-12-06


103(195)

2.4.9 Implemented Changes Status date November 23

rd 2012.

SB/AD etc

Reference


e

Stat

us

Remarks


Systems Inc.

CENTURY SB CSB-

2005-01

Check for frayed Bridle Cable 21-feb-05 20-aug-10


Safety Agency

EASA AD 2009-

0251-E

Portable Fire Extinguishers-Ident/Repl 25-nov-09 07-May-

2010


EASA AD 2009-

0262

Halon 1211 Fire Extinguishers Id/Repl EASA AD 2009-0278 FFE ASB26-115 Rev C 15-dec-09 07-May-

2010


EASA AD 2009-

0278

Halon 1211 Fire Extinguishers Id/Repl EASA AD 2009-0262 22-dec-09 07-May-

2010


EASA AD 2010-

0003


Check/Modification


EASA SIB 2008-58R1

Channel Spacing Switching GARMIN SSB0844 Rev IR GARMIN SSB0845 Rev IR




FAA, U.S AD 2000-02-25


FAA, U.S AD 2000-

09-15

1 Flight in Icing Condition FINNISH AD M 2435/97 FINNISH AD M

2786/00 MAI SB 086/74-002 Rev A MAI SB 093/22-009 MAI SB 096/30-004


07-jul-00 1 14-jun-02


2012-12-06


104(195)

FAA, U.S AD 2003-

17-04



01-Oct-

2003

20-aug-10

FAA, U.S AD 2003-22-07


16-apr-04 1 09-jun-04 Inserted in AFM Limitation Section

FAA, U.S AD 2005-14-12


FAA, U.S AD 2005-18-20


12-Oct-2005


FAA, U.S AD 2006-13-15


11-aug-06 19-jun-02 c/o in conjunction with vingstudie

FAA, U.S AD 2006-15-07


FAA, U.S AD 2006-17-01



FAA, U.S AD 2006-17-05

Adjust flight idle fuel flow setting MITSUBISHI SB 234 22-sep-06 13-sep-10

FAA, U.S AD 2007-

17-09


trim


FAA, U.S AD 71-14-

01

Fuel Tank Fungus Coating Peeling 01-May-1972 01-jan-96 N/A N/A by s/n

FAA, U.S AD 74-11-

01


B

30-jan-78 01-apr-76

FAA, U.S AD 75-16-

13



05-aug-75 06-May-

1977

Revision C PCW by Swedair.

FAA, U.S AD 75-16-

20



12-aug-75 24-feb-75

FAA, U.S AD 78-03-05


180 Rev A

23-feb-78 30-dec-77

FAA, U.S AD 81-06-

01

1 Engine Aft Nacelles 01-apr-81 1 06-May-

1997


FAA, U.S AD 81-25-

04


003A, SB 043/71-005


FAA, U.S AD 82-08-

02

Electrical Wiring Inspection 15-apr-82 15-feb-82

FAA, U.S AD 83-08-

01

2 To preclude prop. attach bolt failures FINNISH AD M 1168/83 Rev 1 FINNISH AD


28-apr-82 2 20-May-

2005

Ref. MU2B MM chap 13.4 when using bolts P/N B-

3339 only


2012-12-06


105(195)

FAA US AD 83-09-

02

Stobe light assemblies 16-Mar-12

FAA, U.S AD 84-12-

04


047/30-001, SB 196A


196 Rev A

28-jun-84 04-jun-84

FAA, U.S AD 84-25-

02


SB 031/27-005 R1, SB 176E


176 Rev E

18-dec-84 11-mar-86

FAA, U.S AD 86-15-03

NLG Strut Assembley LFV LVA1546 MITSUBISHI SB 181 PART 2 Rev B


FAA, U.S AD 86-20-

01


SB 020/34-005, SB 053A

LFV LVD2015 Rev B, MAI SR 020/34-005,

MITSUBISHI SR 053A

06-Oct-

1986

19-May-

2000

FAA, U.S AD 86-26-

02


iceing SB 74-0003, SR 040/74-001

GARRETT SB 74-0003 Rev 6 MAI SR

040/74-001 MITSUBISHI SB 226 Rev E

MITSUBISHI SR 066


FAA, U.S AD 87-04-

03


Insp SB 051/27-007, SB 198

MAI SB 051/27-007 MITSUBISHI SB 198 07-mar-87 08-jul-85

FAA, U.S AD 87-12-

02

Generator Shield Jumper Wires MITSUBISHI SB 201 Rev A 03-jul-87 04-May-

1990

FAA, U.S AD 88-13-01

Bendix Autopilot Disengagement SB 066/22-006


11-jul-98 06-feb-89 N/A N/A due to Autopilot model

FAA, U.S AD 88-21-01



FAA, U.S AD 88-23-01

To prevent flap control failure SB 067/27-008, SB 189B

LFV LVD2202 MAI SB 067/27-008 Rev A 04-dec-88 23-mar-95

FAA, U.S AD 93-07-

11


010


FAA, U.S AD 94-04-

16

Elevator trim tab mod. LFV LVD2537 MITSUBISHI SB 216 11-apr-94 11-mar-93

FAA, U.S AD 94-11-

04


016/61-001


FAA, U.S AD 96-25-

02


4552-96 LFV LVD2749

27-dec-96 01-jan-97

FAA, U.S AD 97-04-

13


1997

N/A N/A due to s/n.

FAA, U.S AD 97-20-

14 CNL


1997

02-dec-98

FAA, U.S AD 97-25-

02


ctrl/overspe


FAA, U.S AD 98-20-

39

Forward fitting bolt of wingtip tank SB

MU-2 225, 089/57-002A

LFV LVD2688, MITSUBISHI SB 225 19-Oct-

1998

28-jan-97


2012-12-06


106(195)


Aviation Adm.

FINNISH AD M

1177/83

Kontroll av rören till strobe-kablarna MITSUBISHI SB 174 PART 1 Rev C 07-jul-83 20-aug-10

FINNISH AD M

2609/98


097/73-001, TCD-4890-98

JCAB AD TCD-4890-98 MAI SB 097/73-001 12-nov-99 02-sep-10

FINNISH AD M

3076

Kontroll av vindrutor och fönster FAA, U.S AD 2003-17-04 MAI SB 087/56-

001 Rev B MITSUBISHI SB 224 Rev C

21-aug-03 20-aug-10

GARMIN, Garmin

GARMIN SSB 0844 IR Software Version 5.04 EASA SIB2008-58R1 14-nov-08 A 24-May-2010

GARMIN SSB 0845 IR Software Version 6.04 EASA SIB2008-58R 14-nov-08 0 24-May-

2010

GARRETT,

AlliedSignal

Aerospace

GARRETT SB 74-0003


HARTZELL, Hartzell

Propeller Inc.

HARTZELL SB 61-256

Propeller mounting bolt inspection MITSUBISHI SL 053/72-003, MITSUBISHI SL 080

08-feb-02 26-mar-02 R/H



04-Oct-2005

14-nov-05 Propellerbolts previously checked u/a

HARTZELL SB A61-313

3 Counterweight Slug Bolt Inspection EASA SIB2008-88 , MITSUBISHI SL 088 Rev A

15-jul-09 3 20-sep-10 N/A by SSB 0844




Bureau

JCAB AD TCD- Rivet holes elevator hinge fitting 06-feb-68 26-mar-09 N/A by s/n


2012-12-06


107(195)

0518-68

JCAB AD TCD-

0642-70

AFM revision regarding fuel spec. LFV LVA439 MITSUBISHI SB 112 Rev C 07-feb-70 11-mar-86

JCAB AD TCD-

0643-70

Adjustment of fuelquantitygauge LFV LVA438 MITSUBISHI SB 114 07-feb-70 15-jul-04 N/A N/A by s/n.

JCAB AD TCD-

0652-70


JCAB AD TCD-

0653-70


of


JCAB AD TCD-

0660-70


nosegearstrut


1970



Insp. and painting of maintanks LFV LVA543 Rev B MITSUBISHI SB 143 Rev B




JCAB AD TCD-0859-72


JCAB AD TCD-0866-72

NLG gearbox and structure LFV LVA664 MITSUBISHI SB 155 09-Oct-1972



Kontr. & mod. av klaffdrivning LFV LVA828 Rev A MITSUBISHI SB 162 Rev A

12-nov-74 24-Oct-1986

N/A N/A due to s/n.




Inspektion av frontrutor LFV LVA829 Rev A MITSUBISHI SB 163 Rev B

07-Oct-1974

01-apr-76



06-Oct-1976

11-mar-86




12-dec-84 11-mar-86

JCAB AD TCD-

1094A-76



06-sep-76 06-May-

1977


JCAB AD TCD-

1188-75

Insp. of propeller controllever inst. FAA, U.S AD 75-16-20 LFV LVA1012


06-May-

1975

24-feb-75

JCAB AD TCD-

1202-75

Engine Cowling Latches FAA, U.S AD 78-03-05 LFV LVA1014 Rev A

MITSUBISHI SB 171 Rev B MITSUBISHI SB 180 Rev A


JCAB AD TCD-1209-75




2012-12-06


108(195)

JCAB AD TCD-

1235-75


emerg.cables

LFV LVA1083 MITSUBISHI SB 170 Rev A 19-sep-75 19-feb-86 N/A N/A due to model.

JCAB AD TCD-

1272-75


Mech.-I&M


JCAB AD TCD-

1284-1-76


JCAB AD TCD-1328-76

Fire hazard in rear baggage compartment


JCAB AD TCD-

1353-76


Repl.


JCAB AD TCD-

1370-76


1976

28-aug-86 Part.1

JCAB AD TCD-

1370A-81

Inspect strobelight conduit in Tiptank

supersed TCD-1370-76

MITSUBISHI SB 174 PART 1 Rev C 05-nov-81 20-aug-10

JCAB AD TCD-

1379-1-80


heatdamage


Rev B

06-feb-02 06-May-

1977


JCAB AD TCD-

1520A-77


JCAB AD TCD-

1768-1-85


JCAB AD TCD-

1817-79

Modification of bagagecompartment LFV LVA1583 MITSUBISHI SB 182 05-feb-02 11-feb-80 N/A N/A due to s/n.

JCAB AD TCD-

2048-81


circuit


1985

N/A N/A due to model.

JCAB AD TCD-

2070-81

Inspect NLG downlock mechanism LFV LVA1753 MITSUBISHI SB 188 05-feb-02 24-nov-81

JCAB AD TCD-

2113-82


harness

LFV LVA1788 MITSUBISHI SB 191 06-feb-02 15-feb-82

JCAB AD TCD-

2252-2-88


TCD-2252-1-87

01-feb-89 24-mar-09 PCW

JCAB AD TCD-

2252-83

Flapcontrolsystem torquetubes LFV LVA1873 MITSUBISHI SB 189 Rev C 04-feb-83 23-mar-95

JCAB AD TCD-

2263-83





JCAB AD TCD-2342-84


LFV LVA1942 MITSUBISHI SB 196 Rev A 06-feb-02 04-jun-84




2012-12-06


109(195)

JCAB AD TCD-

2451-1-87


1987


JCAB AD TCD-

2451-85



LFV LVD2037 MITSUBISHI SB 198 30-sep-85 08-jul-85

JCAB AD TCD-

2545-1-88

Generator System LFV LVD2191 MITSUBISHI SB 201 Rev A 01-jul-88 06-feb-89



01-feb-97 22-nov-01

JCAB AD TCD-

3378-90


leadingedge


JCAB AD TCD-

3393A-96



25-May-

1996

20-aug-10

JCAB AD TCD-

3464-91


JCAB AD TCD-

3740A-98


MSB 216, 228 LVD 2898


LVD2898 MITSUBISHI SB 216 MITSUBISHI

SB 228

17-aug-98 24-nov-98

JCAB AD TCD-3901-93


10-sep-93 13-jun-94



28-nov-94 23-mar-95

JCAB AD TCD-3942-94


JCAB AD TCD-

4310-96


MITSUBISHI SB 225

01-apr-96 28-jan-97

JCAB AD TCD-

4311-95



01-nov-95 20-aug-10

JCAB AD TCD-

4379-96


MITSUBISHI SB 229

01-apr-96 30-jul-96

JCAB AD TCD-

4552-96

Icing Limitation FAA, U.S AD 96-25-02 LFV LVD2749 27-dec-96 01-jan-97

JCAB AD TCD-

4625-97


093/22-009

14-jul-97 04-jun-02

JCAB AD TCD-

4625A-2001


NYGE TDM01-45

16-mar-01 14-jun-02 PCW Ref AMOC LFV Appr M15/01, TDM 01-45

JCAB AD TCD-

4626-97



01-May-

1997

14-jul-04

JCAB AD TCD-

4684-97


MITSUBISHI SB 230

01-jun-97 25-mar-99


2012-12-06


110(195)

JCAB AD TCD-

4753-98


2922,FAA AD 97-20-14, MHI SN 117A




JCAB AD TCD-

4753A-2004

Icing-related incidents VIDEO FAA, U.S AD 2003-22-07 Rev 1 24-feb-04 09-jun-04 Inserted in AFM Limitation Section

JCAB AD TCD-

4838-98


train


MITSUBISHI SB 235


JCAB AD TCD-4889-2-2007


JCAB AD TCD-

4889-98





05-nov-98 14-jul-04 PCW

JCAB AD TCD-

4890-98


SB 234


MITSUBISHI SB 234

04-nov-98 13-sep-10

JCAB AD TCD-

5030-99


1999


JCAB AD TCD-

5432-2000


JCAB AD TCD-

5547-2001


JCAB AD TCD-

5747-2001

Inspection of Tip Tank Brackets LFV LVD3166 MITSUBISHI SB 236 12-sep-01 27-sep-01

JCAB AD TCD-

5864-2001


JCAB AD TCD-

6127-2003

Pneumatic Line insp. LFV LVD3322 MITSUBISHI SB 239 17-mar-03 12-jun-03

JCAB AD TCD-

7030-2006


Hardware


LFV,

Luftfartsverket

LFV LVA 1011 A Kontroll av vingklaffarnas

manöversystem


1094A-76 MITSUBISHI SB 167 Rev D

05-feb-02 A 06-May-

1977


LFV LVA 1012 Kontroll av propellerreglagets

montering



05-feb-02 24-feb-75

LFV LVA 1013 Kontr. och mod. av låsning på nosställ JCAB AD TCD-1209-75 MITSUBISHI SB 169

Rev B

05-feb-02 25-jun-75


låsanordning



05-feb-02 A 30-dec-77


2012-12-06


111(195)

LFV LVA 1083 Insp. & utbyte av lina för nödöppning JCAB AD TCD-1235-75 MITSUBISHI SB 170

Rev A

05-feb-02 19-feb-86 N/A N/A due to s/n.

LFV LVA 1196 Isolering av strobe light från bränsle JCAB AD TCD-1370-76 MITSUBISHI SB 174

PART 1 Rev C

06-feb-02 20-aug-10


bak.motorpl.


177 Rev B

06-feb-02 A 06-May-

1977


LFV LVA 1238 Kontr. & byte av infästningsdet. trimrod




06-feb-02 29-nov-84


LFV LVA 1740 Kontr.av brandvarnings-och n"dstr"mskret



LFV LVA 1753 Kontroll av låsmekanism i nosställ JCAB AD TCD-2070-81 MITSUBISHI SB 188 05-feb-02 24-nov-81


motor

JCAB AD TCD-2113-82 MITSUBISHI SB 191 06-feb-02 15-feb-82


Rev C

06-feb-02 23-mar-95

LFV LVA 1942 Momentdragning/låsn.av koppl.i varmlufts


06-feb-02 04-jun-84

LFV LVA 438 Justering av bränslemängdsmätare JCAB AD TCD-0643-70 MITSUBISHI SB 114 05-feb-02 11-mar-86 N/A N/A by s/n


bränslespec.


Rev C

05-feb-02 11-mar-86







162 Rev A

05-feb-02 A 24-Oct-

1986

N/A N/A due to s/n.



163 Rev B

05-feb-02 A 01-apr-76

LFV LVA 886 A Kontroll/byte av höjdtrimroderarmar JCAB AD TCD-1001A-76 05-feb-02 A 11-mar-86


2012-12-06


112(195)


höjdtrimroder



176 Rev E

18-jan-85 29-mar-85


Rev A, MHI SR 53


2450A-87 MAI SR 020/34-005 MITSUBISHI SR 053A

24-May-

1985

B 06-nov-86

LFV LVD 2037 Flap Flexible Shaft MU2 SB 198 JCAB AD TCD-2451-85 MITSUBISHI SB 198 30-sep-85 08-jul-85

LFV LVD 2069 Altimeter 25-mar-86 23-May-1986

N/A N/A by p/n & s/n


26-jan-87 25-mar-87

LFV LVD 2190 Autopilot Switch MU2 SB 066/22-006

och SB 206

FAA, U.S AD 88-13-01 MAI SB 066/22-006

Rev A MITSUBISHI SB 206

19-aug-88 06-feb-89 N/A Bendix A/P ej installerad


201 Rev A

19-aug-88 06-feb-89



08-dec-88 23-mar-95

LFV LVD 2206 Modifiering av Autopilot FAA, U.S AD 88-21-01 Rev 1 08-dec-88 12-feb-02


211


LFV LVD 2347 1 Control Deice-system Mitsubishi SB 212A

JCAB AD TCD-3393A-96 MITSUBISHI SB 212 Rev A

29-May-1996

1 20-aug-10

LFV LVD 2352 Shoulder Harness Inst. FAA AC 43-13 CHPT 9

23-May-1991

04-nov-91 checked OK.

LFV LVD 2450 Elevator Trim Tab Installation MU SB 216

JCAB AD TCD-3740A-98 MITSUBISHI SB 216

03-dec-92 11-mar-93

LFV LVD 2477 Electric Trim System AD930711, MU SB 079/27-0-010


LFV LVD 2512 TIP TANK INST. (NXT 100H) JCAB AD TCD-3901-93 MITSUBISHI SB 221 02-dec-93 13-jun-94

LFV LVD 2537 Reducering av Höjdrodrets

trimområde. FAA AD 94-04-16, SB

216

FAA, U.S AD 94-04-16 MITSUBISHI SB 216 07-apr-94 11-mar-93


219


Rev A

07-apr-94 23-mar-95


2012-12-06


113(195)



TCD-3942-1-94, MSB 219A


219 Rev A

09-feb-95 23-mar-95

LFV LVD 2678 Kontr. av vindrutor och fönster MHI

SB 224 Rev A



12-mar-96 20-aug-10

LFV LVD 2688 Kontr/byte av infästn.bult för tiptank

MU-2 SB 225



09-May-

1996

28-jan-97


MU-2 SB 229


1996

30-jul-96




261 Rev 1

27-sep-96 04-Oct-

1999

Prop. utbytt mot BVA

LFV LVD 2749 Revision av flyghandbok AFM TCD-4552-96

FAA, U.S AD 96-25-02 JCAB AD TCD-4552-96

21-jan-97 12-feb-02

LFV LVD 2761 Installation av autoignition system TCD-2679A-97

JCAB AD TCD-2679A-97 MITSUBISHI SB 226 Rev E

14-feb-97 29-sep-99



18-mar-97 05-May-1997

N/A N/A due to s/n.



28-aug-97 10-jun-98


JCAB AD TCD-4684-97 MITSUBISHI SB 230 18-nov-97 23-jun-98


23-mar-98 17-dec-09





27-aug-98 24-nov-98







Rev B

01-dec-98 12-apr-99

LFV LVD 2925 Kontr/just av mot bränsleflöde Flight

Id MHI SB 234

JCAB AD TCD-4890-98 MITSUBISHI SB 234 01-dec-98 02-sep-10


Rev B




009 MITSUBISHI SB 231 Rev B NYGE

02-apr-01 14-jun-02 Ref AMOC LFV Appr M15/01, TDM 01-45


2012-12-06


114(195)

TDM01-45




20-sep-01 27-sep-01


09-jan-02 16-jan-02

LFV LVD 3322 Kontroll av tryckluftsledningar JCAB AD TCD-6127-2003 MITSUBISHI SB

239

21-mar-03 12-jun-03


International

MAI SB 047/30-001



19-jul-84 A 04-jun-84

MAI SB 051/27-

007


Torque AD 87-04-03, SB 198

FAA, U.S AD 87-04-03 01-feb-85 08-jul-85

MAI SB 067/27-

008



FAA, U.S AD 88-23-01 LFV LVD2202 29-mar-95 A 23-mar-95

MAI SB 069/24-

006

Split Radio Bus Inspection and

Rework

MAI SB 066/22-006 Rev A 17-nov-88 06-feb-89 N/A N/A due to Aircraft s/n

MAI SB 086/74-

002

A Auto-Ignition System Installation FAA, U.S AD 2000-09-15 Rev 1 FINNISH AD

M 2435/97 MITSUBISHI SB 226 Rev E

05-Oct-

2000


MAI SB 089/57-

002

A Insp/Repl. of Bolts for Wing Tip Tank FAA, U.S AD 98-20-39 05-nov-96 A 28-jan-97 N/A N/A due to s/n.

MAI SN 110/00-017A


MAI SN 111/77-004

Torque Indicating System Shift Potential


MAI SR 020/34-005



06-Oct-1986

19-May-2000

N/A N/A due to s/n.

MITSUBISHI,

Mitsubishi Heavy

Industries Ltd

MITSUBISHI MSB

24-004

**RECOVERED RECORD** 19-feb-86 N/A

MITSUBISHI MSR

020

**RECOVERED RECORD** 06-nov-86


2012-12-06


115(195)

MITSUBISHI MSR

066

B **RECOVERED RECORD** 25-mar-87 B

MITSUBISHI SB 066 Bendix M4D 18-dec-87 06-feb-89 N/A

MITSUBISHI SB

076/22-008


Install.

11-apr-91 12-apr-95 N/A

MITSUBISHI SB 112 C Anti-Ice Additive in Fuel -Usage of JCAB AD TCD-0642-70 LFV LVA439 09-Oct-

1971

C 11-mar-86

MITSUBISHI SB 114 Fuel Quantity Indicator Readjustmnet JCAB AD TCD-0643-70 LFV LVA438 01-jan-70 15-jul-04 N/A N/A by s/n.

MITSUBISHI SB 119 The Bolt and Bolt Hole Diam. of Nose

L.G


MITSUBISHI SB 123 Bearing,Oleo Strut,Nose L.G. -Repl. of JCAB AD TCD-0660-70 LFV LVA457 01-apr-70 26-mar-09 N/A by s/n

MITSUBISHI SB 124 Scissors Switch,Nose L.G. -Install. of 31-aug-70 19-feb-86 N/A

MITSUBISHI SB 128 B Tip Tank Air Pressure Modification 28-jun-94 B 05-nov-09 N/A by model & s/n

MITSUBISHI SB 143 B Top Coating, Wing Integral Main F.T.-SIo

JCAB AD TCD-0730-1-72 JCAB AD TCD-0730-2-86


MITSUBISHI SB 152 Air Conditioning System-Improvement of

08-nov-71 13-jun-03 N/A N/A by s/n

MITSUBISHI SB 162 A Flex. Shafts, Flap Control Sys.-Insp. of (AD750201)


A 24-Oct-1986

N/A

MITSUBISHI SB 163 B Insp. of Outer Pane, Front Winds. & Inst

FAA, U.S AD 74-11-01 JCAB AD TCD-0948A-1-78 JCAB AD TCD-0948A-74 LFV LVA829 Rev A

16-nov-78 01-apr-76

MITSUBISHI SB 165 A Lubr. Interval,Wheel Bearing,Main & Nose

24-jul-80 19-feb-86 N/A

MITSUBISHI SB 166 Wing Flap 24-jul-80 11-mar-86 N/A

MITSUBISHI SB 167 D Flap M.Jack Screw-Insp. of and/or Main G


24-jul-80 D 06-May-1977


MITSUBISHI SB 168 A Propeller Pitch Control Lever-Insp. of (AD761620)

FAA, U.S AD 75-16-20 JCAB AD TCD-1188-75 LFV LVA1012

24-jul-80 A 24-feb-75

MITSUBISHI SB 169 B Shimmy Damper-Insp. and Modification of


MITSUBISHI SB 170 A MLG Forward Door Em.Op. Cable-Insp. & Re (AD762204)

JCAB AD TCD-1235-75 LFV LVA1083 24-mar-77 A 19-feb-86 N/A N/A due to s/n

MITSUBISHI SB 171 B Latches,Eng. Nacelle Upper D.-Insp.& Mod (AD780305)


17-nov-77 B 30-dec-78

MITSUBISHI SB 173 A Drag Strut, Main L.G.-Modification of JCAB AD TCD-1284-1-76 24-jul-80 01-apr-76


2012-12-06


116(195)

MITSUBISHI SB 174

PART 1


Rew.of (AD830902)


1370A-81 LFV LVA1196

02-Oct-

1981

C 20-aug-10

MITSUBISHI SB 175 Barrel Nut, Inner/Outer Wing Conn.-

Repl.

JCAB AD TCD-1353-76 26-jun-76 01-sep-09 N/A by s/n

MITSUBISHI SB 176 E Elevator Trim Tab Bracket-Repl. of

LVD1971, AD 84-25-02, SB 031/27-005R1


1080/82 JCAB AD TCD-1001A-76 JCAB AD TCD-1001B-2-84 LFV LVD1971

26-sep-84 E 11-mar-86

MITSUBISHI SB 177 B Mod. of Engine Nacelle Tail Area

(AD810601)


A

11-sep-80 B 06-May-

1977


MITSUBISHI SB 179 Rodd Assem., Engine Nacelle Upper

D.-R&M

27-May-

1977

10-mar-88

MITSUBISHI SB 180 A Link, Engine Nacelle Upper D.-Repl. of

(AD780305)



17-nov-77 A 30-dec-77




08-apr-85 B 29-nov-84

MITSUBISHI SB 182 Add. of Ceiling Cover, Rear Bagg. Comp.


MITSUBISHI SB 184 Turnbuckle, Control Cables -Repl. of 04-apr-80 19-feb-86 N/A

MITSUBISHI SB 188 Down Lock Mech., Nose L.G.-Insp. of JCAB AD TCD-2070-81 LFV LVA1753 13-jul-81 24-nov-81

MITSUBISHI SB 189 C Flap Control Torque Tube AD 88-23-01, SB 067/27-008

FINNISH AD M 2722/00 JCAB AD TCD-2252-1-87 JCAB AD TCD-2252-83 LFV

LVA1873 LFV LVD2202

28-jun-94 C 23-mar-95

MITSUBISHI SB 190 A Trav. Nut Repl. of L.G. Mech. Stop Assem

28-jun-94 23-jul-82

MITSUBISHI SB 191 Engine El. Wire-Insp. and Replacement of (AD820802)

JCAB AD TCD-2113-82 LFV LVA1788 21-dec-81 15-feb-82

MITSUBISHI SB 193 B Landing Gear Warning Horn Syst.Modif.


MITSUBISHI SB 194 Master Cauting Light Visibility-Impr. of

23-aug-82 14-feb-83

MITSUBISHI SB 196 A Ret. of coupling nut on the bleed air tu AD 84-12-04, SB 047/30-001

FAA, U.S AD 84-12-04 JCAB AD TCD-2342-1-84 JCAB AD TCD-2342-84 LFV LVA1942

MAI SB 047/30-001 Rev A

12-apr-84 A 04-jun-84

MITSUBISHI SB 198 Add. Seal & Torque Insp. of Flap

Flex.Sh LVD2037, AD 87-04-03, SB

051/27-007


85 LFV LVD2037

13-feb-85 08-jul-85

MITSUBISHI SB 199 A Engine Lubricating Tubing Insp. &

Protec



2012-12-06


117(195)

MITSUBISHI SB 200 B Insp of Nose Ldg Gear Drag Strut Link 24-jun-94 A 09-aug-88

MITSUBISHI SB 201 A Generator Circuit Wires Insp. and

Mod.


1-88 LFV LVD2191

02-mar-88 A 04-May-

1990

MITSUBISHI SB 204 Speed Placard Change 03-mar-87 13-jun-88

MITSUBISHI SB 206 Bendix Autop.Disengagement Method Stand.

FAA, U.S AD 88-13-01 JCAB AD TCD-2856-1-97 LFV LVD2190

13-Oct-1987


MITSUBISHI SB 207 Rudder T.T. & Elevator T.T. Insp. &

Rep.

20-May-

1988

17-dec-09

MITSUBISHI SB 209 B Fuselage inspection JCAB AD TCD-5030-99 LFV LVD2988 19-apr-99 B 24-mar-09 N/A by model

MITSUBISHI SB 210 A Engine Ignition Unit Replacement 12-nov-96 06-mar-98

MITSUBISHI SB 211 Rudder Trim Tab Modification (LVD

2338)


MITSUBISHI SB 212 A Insp of Anti-ice/Deice Systems (LVD

2347),

JCAB AD TCD-3393A-96 LFV LVD2347 Rev

1

25-apr-96 A 20-aug-10

MITSUBISHI SB 214 Engine Control Rod Inspection 06-dec-91 11-mar-93

MITSUBISHI SB 215 Removel of Prop. Governor Speed Signal

23-Oct-1991

30-jan-92 N/A N/A due to -1 engine

MITSUBISHI SB 216 Elevator Trim Tab Installation (LVD 2450

FAA, U.S AD 2007-17-09 FAA, U.S AD 94-04-16 JCAB AD TCD-3740A-98 LFV LVD2450

11-sep-92 11-mar-93

MITSUBISHI SB 218 A Propeller Feathering Linkage Inspection

17-jan-94 A 18-feb-94

MITSUBISHI SB 219 A Emergency Gear Down G.box Lower Pin Repl


24-Oct-1994

A 23-mar-95

MITSUBISHI SB 221 Tip Tank Conduit Tube Insp. and Rep. JCAB AD TCD-3901-93 LFV LVD2512 10-aug-93 13-jun-94

MITSUBISHI SB 222 Fuselage Waterproof Modification SR 019

28-jun-94 30-sep-98

MITSUBISHI SB 223 Pitot/Static System Improvement SR 064

MITSUBISHI SR 053A MITSUBISHI SR 064 28-jun-94 19-May-2000

MITSUBISHI SB 224 C Acrylic Windsheild/Window glass Insp. UHB

FAA, U.S AD 2003-17-04 FINNISH AD M 3076 JCAB AD TCD-4311-95 LFV LVD2678

30-apr-98 C 20-aug-10

MITSUBISHI SB 225 Forward fitting bult of wingtip tank LVD 2688

FAA, U.S AD 98-20-39 FINNISH AD M 2351/96 JCAB AD TCD-4310-96 LFV

LVD2688

29-sep-95 28-jan-97

MITSUBISHI SB 226 E Auto-Ignition System Installation LVD 2761 (2113), AD TCD-2679A-97




2012-12-06


118(195)



MITSUBISHI SB 227 Rudder Torque Tube Modification 20-dec-96 23-jun-98

MITSUBISHI SB 228 Elevator Trim Indicator Modification LFV 2898


LVD2898

13-jul-98 24-nov-98

MITSUBISHI SB 229 Feathering Valve/Linkage Insp. FAA, U.S AD 2006-15-07 JCAB AD TCD-4379-96 LFV LVD2689

20-feb-96 23-jun-98

MITSUBISHI SB 230 Mod.of Bearing Box Ldg. Gear Act. LVD 2819

JCAB AD TCD-4684-97 LFV LVD2819 05-mar-97 23-jun-98

MITSUBISHI SB 231 B Inst.of Trim-In-Motion Alert System FAA, U.S AD 2000-09-15 Rev 1 FINNISH AD M 2460/97 UPPHÄVD FINNISH AD M

2786/00 JCAB AD TCD-4625A-2001 LFV LVD3122 MAI SB 093/22-009 NYGE TDM01-45


MITSUBISHI SB 232 A De-Ice System Modification LVD 2800, TCD-4626-97

FAA, U.S AD 2000-09-15 Rev 1 FINNISH AD M 2786/00 JCAB AD TCD-4626-97 LFV

LVD2800 MAI SB 096/30-004


MITSUBISHI SB 233 B Insp.of Engine Torque Indication



2608/98 JCAB AD TCD-4889-2-2007 JCAB AD TCD-4889-98 LFV LVD2924


MITSUBISHI SB 234 Fl.Check of the Flight Idle Fuel Flow

Se TCD-4890-98, LVD 2925


4890-98

07-Oct-

1998

02-sep-10

MITSUBISHI SB 235 Inspection of landing gear power

train


MITSUBISHI SB 236 Inspection of Tip Tank Brackets JCAB AD TCD-5747-2001 LFV LVD3166 28-aug-01 27-sep-01

MITSUBISHI SB 237 Inspection of Flap Drive Train JCAB AD TCD-5864-2001 LFV LVD3212 13-dec-01 16-jan-02

MITSUBISHI SB 238 Main Landing Gear Door Safety Pin 05-dec-02 09-jan-03 Perf. at each 600 h. insp.

MITSUBISHI SB 239 Pneumatic Line Insp. and Modification

JCAB AD TCD-6127-2003 LFV LVD3322 26-dec-02 12-jun-03

MITSUBISHI SB 240 Inst.of Trottle Quadrant Placard 26-feb-03 12-jun-03

MITSUBISHI SB 241 A Inspection of Wing Attachment

Hardware


7030-2006


MITSUBISHI SL 060 System 17-feb-89 04-nov-91

MITSUBISHI SL 078 Automatic Autopilot Disconnect 28-jan-02 20-aug-10


2012-12-06


119(195)

System

MITSUBISHI SL 079 Diode inst.in Flap Position Ind.Curcuit 28-jan-02 14-jun-02

MITSUBISHI SL 080 Hartzell Propeller Mounting Bolt Insp. HARTZELL SB 61-256 05-apr-02 26-aug-02 Compliance in according to HC-SB-61-256.

MITSUBISHI SL 084 Pneumatic De-Ice Monitoring System 14-jun-04 20-aug-10

MITSUBISHI SL 085 Hartzell prop. mount. bolt insp. HARTZELL SB 61-279 ALERT Rev 4 17-May-2005

14-sep-05

MITSUBISHI SN 053

B Rudder Torque Tube AD 86-20-01, SB 020/34-005

05-nov-86 B 12-jun-87

MITSUBISHI SN 117

D Icing Awareness Training Video FAA, U.S AD 2003-22-07 Rev 1 JCAB AD TCD-4753-98

14-jun-04 D 09-jun-04

MITSUBISHI SN

146

Water Ingress into Vertical Stabilizer 19-dec-03 09-jun-04

MITSUBISHI SN

148


MITSUBISHI SN

156A


MITSUBISHI SN

157


Potential


MITSUBISHI SN

161


MITSUBISHI SR

053A



23-Oct-

1984

14-nov-86

MITSUBISHI SR 064 Pitot & Static System MITSUBISHI SB 223 30-apr-85 19-May-2000

MITSUBISHI SR 065 Warning Horn 20-jan-86 13-jun-88

MITSUBISHI SR 067 Emergency Exit Placard 17-sep-85 15-jan-86

MITSUBISHI SR 072 Air Filter Replacement for Vacuum Syst.

25-apr-00 29-jan-01

MITSUBISHI SR 075 Inst. tip tank placard 29-Oct-2004

02-May-2005

MITSUBISHI STC SA01913SE


NARCO, Narco


2012-12-06


120(195)

NARCO SB ELT10-

16

ELT ASSY 18-apr-88 04-nov-91 N/A ELT ASSY

NYGE, Saab Aerotech

Aircraft Services

NYGE TDM 01-45 Installation of Trim-In-Motion Alert

Syst. and Automatic A/P Disconnect syst.



07-May-

2001

14-jun-02

NYGE TDM 02-10 Installation of TPE331-6-252M Engines

25-mar-02 13-jun-03


18-dec-02



04-mar-03 21-Oct-2008

NYGE TDM 03-12 Installation Ugglan 25-mar-03 07-apr-03


NYGE TDM 03-28 F Nav Demo Pod 19-dec-03 F 31-aug-09 Original compliance by Rev D. Not affected by rev F.


NYGE TDM 05-35 A Installation FR-31 11-May-2006

A 12-May-2006

Approved i.a.w. DOA 21j.108.05-35

NYGE TDM 06-28 A Removable FR-31 29-jun-07 A 18-sep-07




NYGE TDM 08-03 A Enhanced Surveillance MU-2B 28-feb-08 A 17-dec-09



NYGE TDM 09-24 A Electrical Wiring Feed Through 08-sep-09 A 31-aug-09

NYGE TDM 09-31 A GPS Splitter 12-nov-09 A 10-dec-09

NYGE TDM 10-02 A Target surveillance camera 03-jun-10 A 01-Oct-2010


2012-12-06


121(195)

NYGE TDM 10-03 A Pressure Bulkhead Feed Through 04-May-

2010

A 01-Oct-

2010

NYGE TDM 10-25 A MU-2B Terminating Resistor 08-apr-10 A 25-May-

2010

NYGE TDM 11-35 A Terminating resistor A 21-Feb-12

NYGE TDM 12-21 A Avinstallation IK A 4-Jun-12


NYGE TDM 96-06 Rep. sprickor "hinge,front spar flange"

11-nov-96 14-nov-96

NYGE TDM 99-03 Install. Auto Ignition 03-mar-99 29-sep-99

NYGE TVO 1/09 Inspektion av Stringers & struktur

vinge

25-feb-09 08-apr-09 Inspected with remarks

NYGE TVO 1/93 Low Volt Warning Light (BCL) 22-jan-93 03-mar-93

NYGE TVO 1/96 Slitage Flap Guide Rail 12-apr-96 20-jun-02

NYGE TVO 1/97 3 De-Icertank MU-2B, korrosionskontroll

12-feb-97 24-jun-98

NYGE TVO 2/00 Märkning av infästning domkraft Mu2 01-dec-00 01-feb-01


06-feb-07 A 02-mar-07

NYGE TVO 2/91 A/C Elecrical System 10-jan-91 24-jun-92

NYGE TVO 3/06 Inspect lower rudder hinge bracket 07-dec-06 20-aug-10

NYGE TVO 3/96 3 Wing Spar Flange Inspection. 24-feb-05 3 17-dec-09

NYGE TVO 4/86 2 Wing Pod Inspection 06-apr-92 2 20-aug-10

NYGE TVO 4/91 Special Inspection (next E6.) 19-feb-91 24-jun-92

NYGE TVO 4/92 Engine Install. Kontr. rörledningar 29-apr-92 24-jun-92

NYGE TVO 4/94 3 Fwd. Wing Tiptank Attachment 28-sep-94 3 20-aug-10

NYGE TVO 4/96 Kontroll av Lagerhus i

noshjulsstyrning.

25-Oct-

1996

01-jul-97 Utförd tidigare (ref. Ove N lista)

NYGE TVO 6/88 Allm. instruktion för metallpropeller 13-jun-88 17-dec-09


1992

27-Oct-

1992


2012-12-06


122(195)

NYGE TVO 7/93 Starter Drive Splines 01-nov-93 09-aug-94


feninfästning

08-dec-04 17-dec-09


1992

11-mar-93

NYGE TVO 9/88 Emergency Extension System 08-aug-88 06-feb-89


2012-12-06


123(195)

2.5 GFE Aircraft Mitsubishi MU-2 SE-GHF


Number:


total Hours:

Total

Landing

Cycles:

Date

Reference:

MU-2B-20 299 SE-GHF 12688 6751 2012-11-23


Serial

Number:

Total

Hours

Since New:

Total

Cycles

Since New:

Hours remaining to

overhaul/HIS/GBI:

Left Engine P20388 7806 6761 3101/1288/1301

Right

Engine

P27037 14603 16508 1233/352/2152













XPDR 1 / 2 Garmin GTX 330 *) Mode S EHS




0186

Altimeter LH United Instr. Inc. 5934 PAM-3





2012-12-06


124(195)



LH

Century 52C77






RMI/ADF adapter Bendix/King KDA-692






GPS MAP


Laser Prism


Wing Pylon


EW system



Pylon


U95 Sorc Pod mounted system RH Wing Pylon U95 Sorc




Chaff Dispenser


Pylon


System:






Bus

MIL-STD-1553B Data

Bus

Triax Cable x 1


115/200VAC 400 Hz 3-

AWG 12 x 4

twisted


2012-12-06


125(195)

Phase 3 x 10 A AWG 16 x 2


A

DC Power 28 VDC 200

A

AWG 2 x 2

Adrian C & S Coax Cable 1 x 50 Ω Coax Cable 1 x 50 Ω Prepared installation Coax Cable 1 x 75 Ω Prepared installation Ethernet LAN Cable



2012-12-06


126(195)


rd 2012.


Aircraft SE-GHF






1200 Hour Inspection AMP 11700 12900






Engine S/N P-20388

Remaining


Engine Hot Section Inspection AMP 13977 1288,8


Engine S/N P-27037




Propeller L/H O/H AMP 2008-01-08 15177 2013-01-06



2012-12-06


127(195)


rd 2012.

SB/AD etc

Reference


SB/AD etc

Reference


e

Stat

us

Remarks


Systems Inc.

CENTURY SB CSB-

2005-01

Check for frayed Bridle Cable 21-feb-05 15-sep-10


Safety Agency

EASA AD 2006-0265 Incorrect transponder altitude 30-aug-06 09-dec-10

EASA AD 2009-

0251-E

Portable Fire Extinguishers-

Ident/Repl

25-nov-09 07-May-

2010


EASA AD 2009-0262 Halon 1211 Fire Extinguishers

Id/Repl

EASA AD 2009-0278 FFE ASB26-115 Rev C 15-dec-09 07-May-

2010


EASA AD 2009-0278 Halon 1211 Fire Extinguishers

Id/Repl

EASA AD 2009-0262 22-dec-09 07-May-

2010


EASA AD 2010-0003 R1 Mode S Transponder -

Check/Modification


EASA AD 2012-0037 Kidde Graviner hand operated fire

extinguisher

25-Jun-12

EASA SIB 2008-

58R1


SSB0845 Rev IR




2012-12-06


128(195)


FAA, U.S AD 2000-

02-25


FAA, U.S AD 2000-

09-15




07-jul-00 1 23-nov-01

FAA, U.S AD 2003-

17-04



01-Oct-

2003

09-sep-10

FAA, U.S AD 2003-22-07

1 Forecast Icing Conditions FINNISH AD T5007/03 JCAB AD TCD-4753A-2004 MAI SN 071/00-006 Rev D


16-apr-04 17-May-2004

inserted in AFM

FAA, U.S AD 2005-14-12

Prop. mounting bolt insp. HARTZELL SB 61-279 ALERT Rev 4 29-jul-05 17-sep-08 L/H side

FAA, U.S AD 2005-18-20


12-Oct-2005


FAA, U.S AD 2006-13-15


11-aug-06 26-apr-04 c/o in conjunction with vingstudie

FAA, U.S AD 2006-15-07

Safety evaluation (feathering linkage)

MAI SB 090/76-003 MITSUBISHI SB 229 24-aug-06 24-aug-06 se Mitsubishi SB 229

FAA, U.S AD 2006-17-01

Detect & correct torque transducers

MAI SB 095/77-002 MITSUBISHI SB 233 Rev B


FAA, U.S AD 2006-17-05

Adjust flight idle fuel flow setting MITSUBISHI SB 234 22-sep-06 13-Oct-2010

FAA, U.S AD 2007-17-09

Reduce max deflect elev nose-down trim


FAA, U.S AD 71-14-01

Fuel Tank Fungus Coating Peeling 01-May-1972

01-jan-96 N/A N/A by s/n

FAA, U.S AD 74-11-

01


B

30-jan-78 01-dec-10 PCW See JCAB AD TCD-0948A-1-78

FAA, U.S AD 75-16-

13



05-aug-75 03-May-

1977


FAA, U.S AD 75-16-

20



12-aug-75 25-apr-75

FAA, U.S AD 78-03-

05

Cowling Latches JCAB AD TCD-1202-75 LFV LVA1014 Rev A


23-feb-78 11-aug-75


2012-12-06


129(195)

FAA, U.S AD 81-06-

01

1 Engine Aft Nacelles 01-apr-81 1 23-jun-97 Previously complied with

FAA, U.S AD 81-25-

04

1 Engine's Electrical wiring SB

036/71-003A, SB 043/71-005


FAA, U.S AD 82-08-

02

Electrical Wiring Inspection 15-apr-82 25-mar-82

FAA, U.S AD 83-08-01

2 To preclude prop. attach bolt failures

FINNISH AD M 1168/83 Rev 1 FINNISH AD T5114/05 HARTZELL SI 140A Rev 9

28-apr-82 2 20-May-2005

Ref. MU2B MM chap 13.4 when using bolts P/N B-3339 only

FAA US AD 83-09-

02

Strobe light assemblies 16-Mar-12

FAA, U.S AD 84-12-

04

Torque of Air Tube Coupling Nuts

SB 047/30-001, SB 196A


196 Rev A

28-jun-84 19-jun-84

FAA, U.S AD 84-25-

02

Elevator TrimTab Bracket

Insp/Repl. SB 031/27-005 R1, SB

176E


176 Rev E

18-dec-84 19-mar-86

FAA, U.S AD 86-15-

03


Rev B


FAA, U.S AD 86-20-01

To assure anti-ice capability of pitot SB 020/34-005, SB 053A

LFV LVD2015 Rev B, MAI SR 020/34-005 , MITSUBISHI SR 053A

06-Oct-1986

17-May-2004

FAA, U.S AD 86-26-02

To prevent engine flameout in an iceing SB 74-0003, SR 040/74-001

GARRETT SB 74-0003 Rev 6 MAI SR 040/74-001 MITSUBISHI SB 226 Rev E

MITSUBISHI SR 066


FAA, U.S AD 87-04-

03


Insp SB 051/27-007, SB 198

MAI SB 051/27-007 MITSUBISHI SB 198 07-mar-87 27-jan-83

FAA, U.S AD 87-12-

02

Generator Shield Jumper Wires MITSUBISHI SB 201 Rev A 03-jul-87 02-Oct-

1990

FAA, U.S AD 88-13-

01


066/22-006


MITSUBISHI SB 206

11-jul-98 01-sep-89 N/A N/A due to Autopilot model

FAA, U.S AD 88-21-01



FAA, U.S AD 88-23-01

To prevent flap control failure SB 067/27-008, SB 189B


FAA, U.S AD 93-07-11

ELECTRIC TRIM SYSTEM SB 079/27-010


FAA, U.S AD 94-04-16

Elevator trim tab mod. LFV LVD2537 MITSUBISHI SB 216 11-apr-94 26-May-1993

FAA, U.S AD 94-11-04

Change of Flight Idle Blade Angel SB 016/61-001


FAA, U.S AD 96-25-

02


4552-96 LFV LVD2749

27-dec-96 19-feb-02


2012-12-06


130(195)

FAA, U.S AD 97-04-

13


1997

N/A N/A due to s/n.

FAA, U.S AD 97-20-

14 CNL


1997

02-dec-98

FAA, U.S AD 97-25-

02


ctrl/overspe


FAA, U.S AD 98-20-39

Forward fitting bolt of wingtip tank SB MU-2 225, 089/57-002A

LFV LVD2688 , MITSUBISHI SB 225 19-Oct-1998

30-jan-97

FINNISH, Finnish

Civil Aviation Adm.

FINNISH AD M 1177/83

Kontroll av rören till strobe-kablarna

MITSUBISHI SB 174 PART 1 Rev C 07-jul-83 09-sep-10


Justering av br,nslefl"de MHI SB 097/73-001, TCD-4890-98

JCAB AD TCD-4890-98 MAI SB 097/73-001 12-nov-99 13-Oct-2010

FINNISH AD M 3076 Kontroll av vindrutor och fönster FAA, U.S AD 2003-17-04 MAI SB 087/56-001 Rev B MITSUBISHI SB 224 Rev C

21-aug-03 09-sep-10

GARMIN, Garmin

GARMIN SSB 0844 IR Software Version 5.04 EASA SIB2008-58R1 14-nov-08 A 20-May-

2010

GARMIN SSB 0845 IR Software Version 6.04 EASA SIB2008-58R 14-nov-08 0 20-May-

2010

GARRETT,

AlliedSignal

Aerospace

GARRETT SB 74-

0003


HARTZELL, Hartzell

Propeller Inc.

HARTZELL SB 61-256


08-feb-02 19-mar-02 L/H & R/H side

HARTZELL SB 61-

279 ALERT

4 Prop. mounting bolt insp. FAA, U.S AD 2005-14-12 , MITSUBISHI SL

085

04-Oct-

2005

17-sep-08 L/H side


2012-12-06


131(195)

HARTZELL SI 140A 9 Installation of Mounting Bolt FAA, U.S AD 83-08-01 Rev 2 , LFV LVA1424

Rev A


JCAB, Japan Civil

Aviation Bureau

JCAB AD TCD-0518-

68

Rivet holes elevator hinge fitting 06-feb-68 26-mar-09 N/A by s/n

JCAB AD TCD-0642-

70

AFM revision regarding fuel spec. LFV LVA439 MITSUBISHI SB 112 Rev C 07-feb-70 17-apr-86

JCAB AD TCD-0643-

70


JCAB AD TCD-0652-70


JCAB AD TCD-0653-70

Engine Nacelle Tail Area-Modification of


JCAB AD TCD-0660-70





Insp. and painting of maintanks LFV LVA543 Rev B MITSUBISHI SB 143 Rev B




JCAB AD TCD-0859-72


JCAB AD TCD-0866-72




Kontr. & mod. av klaffdrivning LFV LVA828 Rev A MITSUBISHI SB 162 Rev A

12-nov-74 21-aug-86 N/A N/A due to s/n.



JCAB AD TCD-

0948A-74


B

07-Oct-

1974

15-mar-86

JCAB AD TCD-

1001A-76

Insp./repl. of elevator trim tab rod LFV LVA886 Rev A MITSUBISHI SB 176 Rev

E

06-Oct-

1976

19-mar-86

JCAB AD TCD-

1001B-2-84


Bracket



12-dec-84 19-mar-86

JCAB AD TCD-

1094A-76



06-sep-76 03-May-

1977


JCAB AD TCD-1188-

75



06-May-

1975

25-apr-75


2012-12-06


132(195)

JCAB AD TCD-1202-

75

Engine Cowling Latches FAA, U.S AD 78-03-05 LFV LVA1014 Rev A



JCAB AD TCD-1209-75



JCAB AD TCD-1235-75

Insp./repl. of MLG fwd door emerg.cables

LFV LVA1083 MITSUBISHI SB 170 Rev A 19-sep-75 17-apr-86 N/A N/A due to model.

JCAB AD TCD-1272-

75


Mech.-I&M


JCAB AD TCD-1284-

1-76

Prevent failure of MLG. dragstrut MITSUBISHI SB 173 Rev A 31-mar-76 01-sep-09 PCW Ref. SB 173

JCAB AD TCD-1328-

76


compartment


JCAB AD TCD-1353-

76

Barrel Nut, Inner/Outer Wing

Conn.-Repl.

MITSUBISHI SB 175 16-aug-76 01-sep-09 N/A by p/n

JCAB AD TCD-1370-

76


Tiptank

LFV LVA1196 18-Oct-

1976

21-aug-86 Part.1


Inspect strobelight conduit in Tiptank supersed TCD-1370-76

MITSUBISHI SB 174 PART 1 Rev C 05-nov-81 09-sep-10


Insp. rear eng. cowling reg. heatdamage

LFV LVA1197 Rev A MITSUBISHI SB 177 Rev B

06-feb-02 23-jun-77 Previously complied with



JCAB AD TCD-1768-

1-85

Fatigue failure of the NLG strut

assy.

LFV LVA1546 MITSUBISHI SB 181 PART 12-jul-85 15-jul-04 PCW Found SB 181 part 2 PCW.

JCAB AD TCD-1817-

79

Modification of

bagagecompartment

LFV LVA1583 MITSUBISHI SB 182 05-feb-02 11-feb-80 N/A N/A due to s/n.

JCAB AD TCD-2048-

81


circuit


1981

N/A N/A due to model.

JCAB AD TCD-2070-

81

Inspect NLG downlock mechanism LFV LVA1753 MITSUBISHI SB 188 05-feb-02 25-mar-82

JCAB AD TCD-2113-

82


harness

LFV LVA1788 MITSUBISHI SB 191 06-feb-02 25-mar-82 Checked N/A due to color (brown) of cables i.a.w.

SB 191

JCAB AD TCD-2252-

2-88


TCD-2252-1-87

01-feb-89 24-mar-09 PCW

JCAB AD TCD-2252-

83


JCAB AD TCD-2263-

83



2012-12-06


133(195)

JCAB AD TCD-2342-

1-84

Engine inlet anti-ice tubing.

Torq./lock


JCAB AD TCD-2342-

84

Engine inlet anti-ice tubing.

Torq./lock


JCAB AD TCD-

2450A-87



Add. seal/Tq. insp of flap flex. shaft 01-May-1987


JCAB AD TCD-2451-

85



LFV LVD2037 MITSUBISHI SB 198 30-sep-85 27-jan-83

JCAB AD TCD-2545-

1-88

Generator System LFV LVD2191 MITSUBISHI SB 201 Rev A 01-jul-88 02-Oct-

1986

JCAB AD TCD-

2679A-97

Auto-ignition System FINNISH AD M 2435/97 LFV LVD2761


01-feb-97 22-nov-01

JCAB AD TCD-3378-

90


leadingedge


JCAB AD TCD-

3393A-96



25-May-

1996

15-sep-10

JCAB AD TCD-3464-

91

Unintentional engagement of

A/P......


JCAB AD TCD-

3740A-98


MSB 216, 228 LVD 2898



17-aug-98 08-dec-98

JCAB AD TCD-3901-

93

Tiptank inst FINNISH AD M 2110/93 LFV LVD2512

MITSUBISHI SB 221

10-sep-93 15-mar-94

JCAB AD TCD-3942-

1-94

Inspection of landing gear lower pin FINNISH AD M 2238/95 LFV LVD2592


28-nov-94 03-mar-95

JCAB AD TCD-3942-

94


JCAB AD TCD-4310-

96


MITSUBISHI SB 225

01-apr-96 30-jan-97

JCAB AD TCD-4311-

95



01-nov-95 09-sep-10

JCAB AD TCD-4379-

96


MITSUBISHI SB 229

01-apr-96 30-jul-96

JCAB AD TCD-4552-

96


JCAB AD TCD-4625-

97


093/22-009

14-jul-97 23-nov-01


2012-12-06


134(195)

JCAB AD TCD-

4625A-2001


NYGE TDM01-45

16-mar-01 13-mar-09 PCW Ref AMOC LFV Appr M15/01, TDM 01-45

JCAB AD TCD-4626-

97



01-May-

1997

14-jul-04 PCW

JCAB AD TCD-4684-

97


MITSUBISHI SB 230

01-jun-97 25-mar-99

JCAB AD TCD-4753-98

Ändring av flyghandbok LVD 2922,FAA AD 97-20-14, MHI SN

117A

FINNISH AD M 2518/98 LFV LVD2922 MITSUBISHI SN 117 Rev D


JCAB AD TCD-

4753A-2004

Icing-related incidents VIDEO FAA, U.S AD 2003-22-07 Rev 1 24-feb-04 17-May-

2004

inserted in AFM

JCAB AD TCD-4838-

98


train


MITSUBISHI SB 235


JCAB AD TCD-4889-

2-2007

Inappropriate calib. of eng. trq-

meter

MITSUBISHI SB 233 Rev B 21-jun-07 11-sep-07 Previously carried out, ref. SB 233A.

JCAB AD TCD-4889-

98





05-nov-98 14-jul-04 PCW

JCAB AD TCD-4890-98

Check of flight idle FF LVD 2925, MU SB 234

FINNISH AD M 2609/98 LFV LVD2925 MITSUBISHI SB 234

04-nov-98 13-Oct-2010

JCAB AD TCD-5030-99

Inspect the fuselage frame LFV LVD2988 MITSUBISHI SB 209 Rev B 17-May-1999




JCAB AD TCD-5547-

2001


JCAB AD TCD-5747-

2001

Inspection of Tip Tank Brackets LFV LVD3166 MITSUBISHI SB 236 12-sep-01 08-Oct-

2001

JCAB AD TCD-5864-

2001


JCAB AD TCD-6127-

2003

Pneumatic Line insp. LFV LVD3322 MITSUBISHI SB 239 17-mar-03 09-Oct-

2003

JCAB AD TCD-7030-

2006


Hardware


LFV, Luftfartsverket



05-feb-02 A 03-May-1977


LFV LVA 1012 Kontroll av propellerreglagets FAA, U.S AD 75-16-20 JCAB AD TCD-1188- 05-feb-02 25-apr-75


2012-12-06


135(195)

montering 75 MITSUBISHI SB 168 Rev A

LFV LVA 1013 Kontr. och mod. av låsning på

nosställ


Rev B

05-feb-02 11-jun-75


låsanordning



05-feb-02 A 11-aug-75

LFV LVA 1083 Insp. & utbyte av lina för nödöppning


05-feb-02 17-apr-86 N/A N/A due to s/n.

LFV LVA 1196 Isolering av strobe light från bränsle

JCAB AD TCD-1370-76 MITSUBISHI SB 174 PART 1 Rev C

06-feb-02 09-sep-10

LFV LVA 1197 A Förhindr. av värmeskador på bak.motorpl.

JCAB AD TCD-1379-1-80 MITSUBISHI SB 177 Rev B

06-feb-02 A 23-jun-77 Previously complied with


trimrod




06-feb-02 24-aug-84





LFV LVA 1753 Kontroll av låsmekanism i nosställ JCAB AD TCD-2070-81 MITSUBISHI SB 188 05-feb-02 25-mar-82

LFV LVA 1788 Kontroll/Utbyte av elledningar på motor

JCAB AD TCD-2113-82 MITSUBISHI SB 191 06-feb-02 25-mar-82 Checked N/A due to color (brown) of cables i.a.w. SB 191

LFV LVA 1873 Insp./utbyte av infäst.till torsionsrör

JCAB AD TCD-2252-83 MITSUBISHI SB 189 Rev C

06-feb-02 03-mar-95


varmlufts


Rev A

06-feb-02 19-jun-84



bränslespec.


Rev C

05-feb-02 17-apr-86


LFV LVA 457 Utbyte av lager i nosst,llets st"td,mp.

JCAB AD TCD-0660-70 MITSUBISHI SB 123 05-feb-02 26-mar-09 N/A by s/n





2012-12-06


136(195)


162 Rev A

05-feb-02 A 21-aug-86 N/A N/A due to s/n.


06 JCAB AD TCD-0948A-74 MITSUBISHI SB 163 Rev B

05-feb-02 A 26-mar-09

LFV LVA 886 A Kontroll/byte av höjdtrimroderarmar

JCAB AD TCD-1001A-76 05-feb-02 A 19-mar-86


höjdtrimroder



176 Rev E

18-jan-85 19-mar-86

LFV LVD 2015 B Pitot Tube Wiring MAI SR 020/34-

005 Rev A, MHI SR 53



24-May-

1985

B 06-Oct-

1986

LFV LVD 2037 Flap Flexible Shaft MU2 SB 198 JCAB AD TCD-2451-85 MITSUBISHI SB 198 30-sep-85 03-jun-85

LFV LVD 2069 Altimeter 25-mar-86 07-jul-86 N/A N/A by p/n & s/n


26-jan-87 12-jun-87



19-aug-88 01-sep-89 N/A Bendix A/P ej installerad


19-aug-88 01-sep-89

LFV LVD 2202 Kontr. av koppl. för tors.rör till klaff FAA, U.S AD 88-23-01 JCAB AD TCD-2252-1-87 MAI SB 067/27-008 Rev A MITSUBISHI SB 189 Rev C

08-dec-88 03-mar-95

LFV LVD 2206 Modifiering av Autopilot FAA, U.S AD 88-21-01 Rev 1 08-Dec-1988

12-feb-02


211



212A


212 Rev A

29-May-

1996

1 15-sep-10

LFV LVD 2352 Shoulder Harness Inst. FAA AC 43-

13 CHPT 9

23-May-

1991

16-Oct-

1991

checked OK.

LFV LVD 2450 Elevator Trim Tab Installation MU

SB 216


216

03-dec-92 26-May-

1993




2012-12-06


137(195)

LFV LVD 2512 TIP TANK INST. (NXT 100H) JCAB AD TCD-3901-93 MITSUBISHI SB 221 02-dec-93 15-mar-94

LFV LVD 2537 Reducering av Höjdrodrets

trimområde. FAA AD 94-04-16, SB 216

FAA, U.S AD 94-04-16 MITSUBISHI SB 216 07-apr-94 26-May-

1993

LFV LVD 2538 Byte Låspinne i landställets nödutf. SB 219


07-apr-94 03-mar-95

LFV LVD 2551 Adj.of Ground Idle FAA AD 94-11-04

FAA, U.S AD 94-11-04 22-jun-94 27-mar-09 N/A by s/n



09-feb-95 03-mar-95

LFV LVD 2678 Kontr. av vindrutor och fönster MHI SB 224 Rev A

FAA, U.S AD 2003-17-04 JCAB AD TCD-4311-95 MITSUBISHI SB 224 Rev C

12-mar-96 09-sep-10

LFV LVD 2688 Kontr/byte av infästn.bult för

tiptank MU-2 SB 225



09-May-

1996

26-jun-00 L/H-side


MU-2 SB 229


1996

30-jul-96




261 Rev 1

27-sep-96 16-nov-98 Prop. utbytt mot BVA


4552-96


96

21-jan-97 19-feb-02


TCD-2679A-97


226 Rev E

14-feb-97 15-jun-99



18-mar-97 05-May-1997

N/A N/A due to s/n.



28-aug-97 10-jun-98


JCAB AD TCD-4684-97 MITSUBISHI SB 230 18-nov-97 21-apr-98


23-mar-98 02-feb-11



LFV LVD 2898 Mod. av autopilotens höjdtrimsystem TCD-3740A-98, SB

216, 228


27-aug-98 08-dec-98






01-dec-98 01-apr-99


2012-12-06


138(195)

LFV LVD 2925 Kontr/just av mot bränsleflöde

Flight Id MHI SB 234

JCAB AD TCD-4890-98 MITSUBISHI SB 234 01-dec-98 13-Oct-

2010


Rev B




009 MITSUBISHI SB 231 Rev B NYGE TDM01-45

02-apr-01 23-nov-01 Ref AMOC LFV Appr M15/01, TDM 01-45




20-sep-01 08-Oct-2001


09-jan-02 17-jan-02

LFV LVD 3322 Kontroll av tryckluftsledningar JCAB AD TCD-6127-2003 MITSUBISHI SB 239

21-mar-03 09-Oct-2003

MAI, Mitsubishi

Aircraft

International

MAI SB 047/30-001 A Torque of Bleed Air Tube Coupling

Nuts AD 84-12-04,SB 196A


Rev A

19-jul-84 A 19-jun-84

MAI SB 051/27-007 Add.Seal and Flap Flexible Shaft

Torque AD 87-04-03, SB 198

FAA, U.S AD 87-04-03 01-feb-85 27-jan-83

MAI SB 067/27-008 A Insp/Repl. of Flap Control System



MAI SB 069/24-006 Split Radio Bus Inspection and

Rework

MAI SB 066/22-006 Rev A 17-nov-88 01-sep-89 N/A N/A due to Aircraft s/n

MAI SB 086/74-002 A Auto-Ignition System Installation FAA, U.S AD 2000-09-15 Rev 1 FINNISH AD M 2435/97 MITSUBISHI SB 226 Rev E

05-Oct-2000


MAI SB 089/57-002 A Insp/Repl. of Bolts for Wing Tip Tank

FAA, U.S AD 98-20-39 05-nov-96 A 30-jan-97 N/A N/A due to s/n.

MAI SN 110/00-017A


MAI SN 111/77-004 Torque Indicating System Shift Potential


MAI SR 020/34-005 Anti Ice Capability AD 86-20-01, SR

053A

FAA, U.S AD 86-20-01 LFV LVD2015 Rev B

MITSUBISHI SR 053A

06-Oct-

1986

21-jan-00 N/A N/A due to s/n.


2012-12-06


139(195)


MITSUBISHI MSB 24-004

**RECOVERED RECORD** 27-jan-83 N/A

MITSUBISHI MSR 020

**RECOVERED RECORD** 12-jun-87

MITSUBISHI MSR

066

B **RECOVERED RECORD** 12-jun-87 B

MITSUBISHI SB 066 Bendix M4D 18-dec-87 18-May-

1988

N/A

MITSUBISHI SB

076/22-008


Install.

11-apr-91 12-apr-95 N/A

MITSUBISHI SB 112 C Anti-Ice Additive in Fuel -Usage of JCAB AD TCD-0642-70 LFV LVA439 09-Oct-

1971

C 17-apr-86

MITSUBISHI SB 114 Fuel Quantity Indicator

Readjustmnet

JCAB AD TCD-0643-70 LFV LVA438 01-jan-70 15-jul-04 N/A N/A by s/n.

MITSUBISHI SB 119 The Bolt and Bolt Hole Diam. of

Nose L.G


MITSUBISHI SB 123 Bearing,Oleo Strut,Nose L.G. -Repl. of

JCAB AD TCD-0660-70 LFV LVA457 01-apr-70 26-mar-09 N/A by s/n

MITSUBISHI SB 124 Scissors Switch,Nose L.G. -Install. of 31-aug-70 17-apr-86 N/A

MITSUBISHI SB 128 B Tip Tank Air Pressure Modification 28-jun-94 B 05-nov-09 N/A by model & s/n

MITSUBISHI SB 143 B Top Coating, Wing Integral Main

F.T.-SIo


0730-2-86


MITSUBISHI SB 162 A Flex. Shafts, Flap Control Sys.-Insp.

of (AD750201)

JCAB AD TCD-0947A-74 LFV LVA828 Rev A 03-Oct-

1974

A 21-aug-86 N/A

MITSUBISHI SB 163 B Insp. of Outer Pane, Front Winds. &

Inst


0948A-1-78 JCAB AD TCD-0948A-74 LFV

LVA829 Rev A

16-nov-78 15-mar-86

MITSUBISHI SB 165 A Lubr. Interval,Wheel Bearing,Main

& Nose

24-jul-80 17-jun-86 N/A

MITSUBISHI SB 166 Wing Flap 24-jul-80 10-mar-86

MITSUBISHI SB 167 D Flap M.Jack Screw-Insp. of and/or Main G


24-jul-80 D 03-May-1977


MITSUBISHI SB 168 A Propeller Pitch Control Lever-Insp.

of (AD761620)


75 LFV LVA1012

24-jul-80 A 25-apr-75


2012-12-06


140(195)

MITSUBISHI SB 169 B Shimmy Damper-Insp. and

Modification of


MITSUBISHI SB 170 A MLG Forward Door Em.Op. Cable-

Insp. & Re (AD762204)

JCAB AD TCD-1235-75 LFV LVA1083 24-mar-77 A 17-apr-86 N/A N/A due to s/n

MITSUBISHI SB 171 B Latches,Eng. Nacelle Upper D.-

Insp.& Mod (AD780305)


75 LFV LVA1014 Rev A

17-nov-77 B 11-aug-78

MITSUBISHI SB 173 A Drag Strut, Main L.G.-Modification of

JCAB AD TCD-1284-1-76 24-jul-80 11-aug-75

MITSUBISHI SB 174

PART 1


Rew.of (AD830902)


1370A-81 LFV LVA1196

02-Oct-

1981

C 09-sep-10

MITSUBISHI SB 175 Barrel Nut, Inner/Outer Wing

Conn.-Repl.

JCAB AD TCD-1353-76 26-jun-76 01-sep-09 N/A by p/n

MITSUBISHI SB 176 E Elevator Trim Tab Bracket-Repl. of

LVD1971, AD 84-25-02, SB 031/27-

005R1


1080/82 JCAB AD TCD-1001A-76 JCAB AD

TCD-1001B-2-84 LFV LVD1971

26-sep-84 E 19-mar-86

MITSUBISHI SB 177 B Mod. of Engine Nacelle Tail Area

(AD810601)


A

11-sep-80 B 23-jun-77 Previously complied with

MITSUBISHI SB 179 Rodd Assem., Engine Nacelle Upper D.-R&M

27-May-1977

04-feb-86

MITSUBISHI SB 180 A Link, Engine Nacelle Upper D.-Repl. of (AD780305)

FAA, U.S AD 78-03-05, JCAB AD TCD-1202-75 , LFV LVA1014 Rev A

17-nov-77 A 29-mar-78




08-apr-85 B 24-aug-84

MITSUBISHI SB 182 Add. of Ceiling Cover, Rear Bagg.

Comp.


MITSUBISHI SB 184 Turnbuckle, Control Cables -Repl. of 04-apr-80 25-mar-82

MITSUBISHI SB 188 Down Lock Mech., Nose L.G.-Insp. of

JCAB AD TCD-2070-81 LFV LVA1753 13-jul-81 25-mar-82

MITSUBISHI SB 189 C Flap Control Torque Tube AD 88-23-01, SB 067/27-008

FINNISH AD M 2722/00 JCAB AD TCD-2252-1-87 JCAB AD TCD-2252-83 LFV

LVA1873 LFV LVD2202

28-jun-94 C 03-mar-95

MITSUBISHI SB 190 A Trav. Nut Repl. of L.G. Mech. Stop

Assem

28-jun-94 25-mar-82

MITSUBISHI SB 191 Engine El. Wire-Insp. and

Replacement of (AD820802)

JCAB AD TCD-2113-82 LFV LVA1788 21-dec-81 25-mar-82

MITSUBISHI SB 193 B Landing Gear Warning Horn Syst.Modif.


MITSUBISHI SB 194 Master Cauting Light Visibility-Impr. of

23-aug-82 27-jan-83


2012-12-06


141(195)

MITSUBISHI SB 196 A Ret. of coupling nut on the bleed

air tu AD 84-12-04, SB 047/30-001



12-apr-84 A 19-jun-84

MITSUBISHI SB 198 Add. Seal & Torque Insp. of Flap Flex.Sh LVD2037, AD 87-04-03, SB 051/27-007


13-feb-85 27-jan-83

MITSUBISHI SB 199 A Engine Lubricating Tubing Insp. & Protec


MITSUBISHI SB 200 B Insp of Nose Ldg Gear Drag Strut Link

24-jun-94 A 02-aug-88

MITSUBISHI SB 201 A Generator Circuit Wires Insp. and Mod.


02-mar-88 A 02-Oct-1986

MITSUBISHI SB 204 Speed Placard Change 03-mar-87 18-May-1988

MITSUBISHI SB 206 Bendix Autop.Disengagement Method Stand.


13-Oct-1987


MITSUBISHI SB 207 Rudder T.T. & Elevator T.T. Insp. & Rep.

20-May-1988

28-aug-09

MITSUBISHI SB 209 B Fuselage inspection JCAB AD TCD-5030-99 LFV LVD2988 19-apr-99 B 24-mar-09 N/A by model

MITSUBISHI SB 210 A Engine Ignition Unit Replacement 12-nov-96 06-mar-98

MITSUBISHI SB 211 Rudder Trim Tab Modification (LVD 2338)


MITSUBISHI SB 212 A Insp of Anti-ice/Deice Systems (LVD 2347),


25-apr-96 A 15-sep-10

MITSUBISHI SB 214 Engine Control Rod Inspection 06-dec-91 13-mar-92

MITSUBISHI SB 215 Removel of Prop. Governor Speed

Signal

23-Oct-

1991

13-mar-92 N/A N/A due to -1 engine

MITSUBISHI SB 216 Elevator Trim Tab Installation (LVD 2450

FAA, U.S AD 2007-17-09 FAA, U.S AD 94-04-16 JCAB AD TCD-3740A-98 LFV


11-sep-92 26-May-1993

MITSUBISHI SB 218 A Propeller Feathering Linkage

Inspection

17-jan-94 A 15-mar-94

MITSUBISHI SB 219 A Emergency Gear Down G.box

Lower Pin Repl


3942-94 LFV LVD2538 LFV LVD2592

24-Oct-

1994

A 03-mar-95

MITSUBISHI SB 221 Tip Tank Conduit Tube Insp. and

Rep.

JCAB AD TCD-3901-93 LFV LVD2512 10-aug-93 15-mar-94

MITSUBISHI SB 222 Fuselage Waterproof Modification

SR 019

28-jun-94 08-dec-98


2012-12-06


142(195)

MITSUBISHI SB 223 Pitot/Static System Improvement

SR 064

MITSUBISHI SR 053A MITSUBISHI SR 064 28-jun-94 21-jan-00

MITSUBISHI SB 224 C Acrylic Windsheild/Window glass

Insp. UHB



30-apr-98 C 09-sep-10

MITSUBISHI SB 225 Forward fitting bult of wingtip tank

LVD 2688



29-sep-95 30-jan-97

MITSUBISHI SB 226 E Auto-Ignition System Installation

LVD 2761 (2113), AD TCD-2679A-97

FAA, U.S AD 2000-09-15 Rev 1 FAA, U.S

AD 86-26-02 FINNISH AD M 2435/97 FINNISH AD M 2786/00 JCAB AD TCD-



MITSUBISHI SB 227 Rudder Torque Tube Modification 20-dec-96 21-apr-98

MITSUBISHI SB 228 Elevator Trim Indicator Modification LFV 2898

FAA, U.S AD 2007-17-09 FINNISH AD M 2581/98 , LFV LVD2898

13-jul-98 08-dec-98

MITSUBISHI SB 229 Feathering Valve/Linkage Insp. FAA, U.S AD 2006-15-07 JCAB AD TCD-4379-96 LFV LVD2689

20-feb-96 30-jul-96

MITSUBISHI SB 230 Mod.of Bearing Box Ldg. Gear Act. LVD 2819

JCAB AD TCD-4684-97 LFV LVD2819 05-mar-97 21-apr-98

MITSUBISHI SB 231 B Inst.of Trim-In-Motion Alert System FAA, U.S AD 2000-09-15 Rev 1 FINNISH AD

M 2460/97 UPPHÄVD FINNISH AD M 2786/00 JCAB AD TCD-4625A-2001 LFV

LVD3122 MAI SB 093/22-009 NYGE

TDM01-45

11-dec-02 B 03-mar-03 SL079 performed earlier.

MITSUBISHI SB 232 A De-Ice System Modification LVD

2800, TCD-4626-97


M 2786/00 JCAB AD TCD-4626-97 LFV LVD2800 MAI SB 096/30-004


MITSUBISHI SB 233 B Insp.of Engine Torque Indication System. TCD-4889-98, LFV 2924

FAA, U.S AD 2006-17-01 FINNISH AD M 2608/98 JCAB AD TCD-4889-2-2007 JCAB

AD TCD-4889-98 LFV LVD2924


MITSUBISHI SB 234 Fl.Check of the Flight Idle Fuel Flow

Se TCD-4890-98, LVD 2925


4890-98 LFV LVD2925

07-Oct-

1998

13-Oct-

2010

MITSUBISHI SB 235 Inspection of landing gear power train


MITSUBISHI SB 236 Inspection of Tip Tank Brackets JCAB AD TCD-5747-2001 LFV LVD3166 28-aug-01 08-Oct-2001

MITSUBISHI SB 237 Inspection of Flap Drive Train JCAB AD TCD-5864-2001 LFV LVD3212 13-dec-01 17-jan-02

MITSUBISHI SB 238 Main Landing Gear Door Safety Pin 05-dec-02 09-jan-03 Perf. at each 600 h. insp.


2012-12-06


143(195)

MITSUBISHI SB 239 Pneumatic Line Insp. and

Modification

JCAB AD TCD-6127-2003 LFV LVD3322 26-dec-02 09-Oct-

2003

MITSUBISHI SB 240 Inst.of Trottle Quadrant Placard 26-feb-03 09-Oct-

2003

MITSUBISHI SB 241 A Inspection of Wing Attachment

Hardware


7030-2006


MITSUBISHI SL 060 System 17-feb-89 16-Oct-1991

MITSUBISHI SL 078 Automatic Autopilot Disconnect

System

28-jan-02 09-sep-10

MITSUBISHI SL 079 Diode inst.in Flap Position

Ind.Curcuit

28-jan-02 23-nov-01

MITSUBISHI SL 080 Hartzell Propeller Mounting Bolt

Insp.

HARTZELL SB 61-256 05-apr-02 26-aug-02 Compliance in according to HC-SB-61-256.

MITSUBISHI SL 084 Pneumatic De-Ice Monitoring

System

14-jun-04 09-sep-10

MITSUBISHI SL 085 Hartzell prop. mount. bolt insp. HARTZELL SB 61-279 ALERT Rev 4 17-May-

2005

17-sep-08 L/H side

MITSUBISHI SN 053 B Rudder Torque Tube AD 86-20-01,

SB 020/34-005

05-nov-86 B 30-jun-87

MITSUBISHI SN 117 D Icing Awareness Training Video FAA, U.S AD 2003-22-07 Rev 1 JCAB AD

TCD-4753-98 LFV LVD2922

14-jun-04 D 17-May-

2004

MITSUBISHI SN 146 Water Ingress into Vertical

Stabilizer

19-dec-03 26-apr-04

MITSUBISHI SN 148 Reminders for safe operation 18-nov-05 22-mar-06 Genomförs enl. AMP MU-2 & DHB

MITSUBISHI SN 156A


MITSUBISHI SN 157 Torque Indicating System Shift Potential


MITSUBISHI SN 161 Repl Air Filter for Vacuum System MITSUBISHI STCSA01913SE 09-dec-09 11-mar-10 Ref STC SA01913SE

MITSUBISHI SN 164 part 2

IR Part 2, one time inspection of mechanical stop bearing

25-Jun-12

MITSUBISHI SR 053A

Modifiering av pitotrör FAA, U.S AD 86-20-01 JCAB AD TCD-2450A-87 LFV LVD2015 Rev B MAI SR 020/34-005 MITSUBISHI SB 223

23-Oct-1984

06-Oct-1986

MITSUBISHI SR 064 Pitot & Static System MITSUBISHI SB 223 30-apr-85 21-jan-00

MITSUBISHI SR 065 Warning Horn 20-jan-86 06-May-1988


2012-12-06


144(195)

MITSUBISHI SR 067 Emergency Exit Placard 17-sep-85 15-apr-86

MITSUBISHI SR 072 Air Filter Replacement for Vacuum

Syst.

25-apr-00 29-apr-04

MITSUBISHI SR 075 Inst. tip tank placard 29-Oct-

2004

06-apr-05

MITSUBISHI STC

SA01913SE


NARCO, Narco

NARCO SB ELT10-16 ELT ASSY 18-apr-88 16-Oct-1991

N/A

NYGE, Saab Aerotech

Aircraft Services

NYGE TDM 00-20 Fågelkollisionskada 07-Dec-

2000

11-dec-00

NYGE TDM 00-23 Wiring Left Wing ADRIAN 22-dec-00 06-jul-00

NYGE TDM 01-45 Installation of Trim-In-Motion Alert Syst. and Automatic A/P Disconnect syst.

JCAB AD TCD-4625A-2001 LFV LVD3122 MITSUBISHI SB 231 Rev B

07-May-2001

23-nov-01

NYGE TDM 01-61 Installation Ceis ELT 10-dec-01 08-jan-02

NYGE TDM 02-10 Installation of TPE331-6-252M

Engines

25-mar-02 29-apr-04


31-Oct-2002


NYGE TDM 02-33 Viktminskning MU-2B 24-dec-02 09-aug-01

NYGE TDM 03-08 8 GNS430/530 & MODE S GTX330

install.

04-mar-03 31-Oct-

2008

NYGE TDM 03-11 C Astor 2 MU-2B 19-mar-03 C 04-mar-03 Original compliance was as per TDM rev A.The A/C

installation is IAW rev C as not affected by rev B and C.F01324, F01341, F01342


NYGE TDM 03-28 F Nav Demo Pod 19-dec-03 F 30-aug-05 Original compliance with previous revision not affected by rev F.F01211, M03323,R01395


2012-12-06


145(195)

NYGE TDM 05-03 Marcus "Installation" 16-feb-05 02-feb-06

NYGE TDM 05-04 ADL Installation 16-feb-05


NYGE TDM 06-28 A Removable FR-31 29-jun-07 A 29-nov-07




NYGE TDM 08-03 A Enhanced Surveillance MU-2B 28-feb-08 A 28-aug-09



NYGE TDM 09-29 A GPS Splitter 12-Oct-2009

A 10-feb-10

NYGE TDM 10-25 A MU-2B Terminating Resistor 08-apr-10 A 18-May-

2010

C/W

NYGE TDM 11-16 19" instrumentrack 04-Oct-

2012

NYGE TDM 11-35 A Terminating resistor 27-Jan-12

NYGE TDM 12-21 A Avinstallation IK 29-Jun-12

NYGE TDM 95-04 4 Vingstudie 20-sep-98 4 26-apr-04

NYGE TDM 97-03 Astor MU-2 25-feb-97 23-apr-97


1998

23-jul-98

NYGE TDM 99-03 Install. Auto Ignition 03-mar-99 15-jun-99

NYGE TVO 1/09 Inspektion av Stringers & struktur vinge

25-feb-09 08-apr-09 Inspected with remarks

NYGE TVO 1/93 Low Volt Warning Light (BCL) 22-jan-93 26-May-1993

NYGE TVO 1/96 Slitage Flap Guide Rail 12-apr-96 26-jun-00


korrosionskontroll

12-feb-97 14-May-

1997

NYGE TVO 2/00 Märkning av infästning domkraft Mu2

01-dec-00 04-apr-01


2012-12-06


146(195)

NYGE TVO 2/07 A Prevent FR31 radio to xmit when

RM2 off

06-feb-07 A 02-mar-07

NYGE TVO 2/91 A/C Elecrical System 10-jan-91 13-mar-92

NYGE TVO 3/06 Inspect lower rudder hinge bracket 07-dec-06 09-sep-10

NYGE TVO 3/96 3 Wing Spar Flange Inspection. 24-feb-05 3 28-aug-09

NYGE TVO 4/11 Static inverter controll A 15-Dec-11

NYGE TVO 4/86 2 Wing Pod Inspection 06-apr-92 2 09-sep-10

NYGE TVO 4/91 Special Inspection (next E6.) 19-feb-91 16-Oct-1991

NYGE TVO 4/92 Engine Install. Kontr. rörledningar 29-apr-92 14-Oct-1992

NYGE TVO 4/94 3 Fwd. Wing Tiptank Attachment 28-sep-94 3 09-sep-10 R/H

NYGE TVO 4/96 Kontroll av Lagerhus i noshjulsstyrning.

25-Oct-1996

20-mar-97

NYGE TVO 4/99 Kontroll av rullbälten 09-apr-99 15-apr-99

NYGE TVO 6/88 Allm. instruktion för

metallpropeller

13-jun-88 15-sep-08

NYGE TVO 6/92 Elevator Trim Cable, check 07-Oct-1992

20-nov-92

NYGE TVO 7/93 Starter Drive Splines 01-nov-93 15-mar-94


feninfästning

08-dec-04 09-sep-10


1992

02-apr-93

NYGE TVO 9/88 Emergency Extension System 08-aug-88 03-nov-88


2012-12-06


147(195)

2.6 GFE Aircraft Mitsubishi MU-2 SE-IOV


Number:


total Hours:

Total

Landing

Cycles:

Date

Reference:

MU-2B-26 337 SE-IOV 11473 4130 2012-11-23


Serial

Number:

Total Hours

Since New:

Total

Cycles

Since New:

Hours remaining

overhaul/HSI/GBI:

Left Engine P20067 11697 10203 1598/1428/3228

Right Engine P20376 10279 10813 2884/1161/1084


Left Propeller HC-B3TN-5E BUA 19597 2013-11-25



Autopilot & Flight Director Bendix M4D

COM/NAV/GPS 1 & 2 Garmin GNS 430


MKR Bendix/King KMR 675

DME Bendix/King KN 63

ADF Bendix/King KR 87

XPDR 1 Garmin GTX 330D

XPDR 2 Garmin GTX 330 *)




0186

Altimeter LH United Instr. Inc. 5934 PAM-3


Altitude Reporter Ameri-King AK-350

Altitude Alerter Century 1D960


Attitude Gyro & Flight Director Ind. Bendix GH-14


2012-12-06


148(195)

LH


Turn & Bank Ind. LH Bendix 4099-B

Horizontal Situation Indicator LH Bendix RD-44


RMI Indicator Collins 332C-10






VHF/UHF COM FR31

GPS MAP


Laser Prism


Wing Pylon


EW system


Pylon

U95 Sorc Pod mounted system RH Wing Pylon




Chaff Dispenser


Pylon

Target Towing

MBV7S Inboard winch



TAPS

Radar Calibration System

GPS Sphere


System:


Adrian C & S, U95 Sorc,

A100, DARTS and BOX 3 General Signal Harness AWG22 shielded x 44


U95-Sorc and A100 MIL-STD-1553B Data Triax Cable x 1


2012-12-06


149(195)

Bus U95 Sorc, A100 and DARTS AC Power

115/200VAC 400 Hz 3-

Phase 3 x 10 A

AWG 16 x 4

twisted

AWG 16 x 2


A

DC Power 28 VDC 200

A

AWG 2 x 2

Adrian C & S Coax Cable 1 x 50 Ω Coax Cable 1 x 50 Ω

U95 Sorc Ethernet LAN Cable



2012-12-06


150(195)


rd 2012.


Aircraft SE-IOV













Engine Assembly (Overhaul) AMP 13072 1598,7



Engine S/N P-20376







2012-12-06


151(195)


rd 2012.

SB/AD etc

Reference

Rev Subject Document reference Eff. date Rev Compliance Stat

us

Remarks


Safety Agency

EASA AD 2006-0265

Incorrect transponder altitude 30-aug-06 11-feb-10

EASA AD 2009-

0251-E

Portable Fire Extinguishers-Ident/Repl 25-nov-09 07-May-2010 N/A N/A by current P/N installed

EASA AD 2009-

0262

Halon 1211 Fire Extinguishers Id/Repl EASA AD 2009-0278 FFE ASB26-115 Rev C 15-dec-09 07-May-2010 N/A N/A by current P/N installed

EASA AD 2009-

0278

Halon 1211 Fire Extinguishers Id/Repl EASA AD 2009-0262 22-dec-09 07-May-2010 N/A N/A by current P/N installed

EASA AD 2010-

0003


Check/Modification


EASA AD 2012-

0037


FIRE EXTINGUISHER

06-Sep-12

EASA SIB 2008-58R1





FAA, U.S AD 2000-

02-25


FAA, U.S AD 2000-

09-15




07-jul-00 22-nov-01 Action not required due to s/n.

FAA, U.S AD 2003-17-04

Windshield check FINNISH AD M 3076 LFV LVD2678 MAI SB 087/56-001 Rev B MITSUBISHI SB 224 Rev C

01-Oct-2003

08-mar-11


2012-12-06


152(195)

FAA, U.S AD 2003-

22-07

1 Forecast Icing Conditions FINNISH AD T5007/03 JCAB AD TCD-

4753A-2004 MAI SN 071/00-006 Rev D MITSUBISHI SN 117 Rev D

16-apr-04 17-May-2004 inserted in AFM limitations

FAA, U.S AD 2005-14-12


FAA, U.S AD 2005-18-20


12-Oct-2005 N/A Due to boots p/n

FAA, U.S AD 2006-

13-15

Safety evaluation wing barrel nuts) MAI SB 103/57-004 Rev A MITSUBISHI SB

241 Rev A

11-aug-06 23-feb-04 c/o in conjunction with vingstudie

FAA, U.S AD 2006-

15-07


FAA, U.S AD 2006-

17-01

Detect & correct torque transducers MAI SB 095/77-002 MITSUBISHI SB 233

Rev B


FAA, U.S AD 2006-

17-05

Adjust flight idle fuel flow setting MITSUBISHI SB 234 22-sep-06 11-feb-10

FAA, U.S AD 2007-

17-09


trim


FAA, U.S AD 71-14-01



FAA, U.S AD 75-03-06

Cracks and Optical Distortion LFV LVA829 Rev A 13-nov-74 21-aug-85 N/A N/A due to s/n.

FAA, U.S AD 75-16-13

Main Wing Flap JCAB AD TCD-1094A-76 LFV LVA1011 Rev A MITSUBISHI SB 167 Rev D

05-aug-75 05-feb-02 N/A Ej tillämplig p.g.a. s/n.

FAA, U.S AD 75-

16-20



12-aug-75 21-aug-85

FAA, U.S AD 78-

03-05

Cowling Latches JCAB AD TCD-1202-75 LFV LVA1014 Rev A

MITSUBISHI SB 171 Rev B MITSUBISHI SB

180 Rev A

23-feb-78 21-aug-85

FAA, U.S AD 81-06-01

1 Engine Aft Nacelles 01-apr-81 1 27-jan-86 Previously complied with

FAA, U.S AD 82-08-02

Electrical Wiring Inspection 15-apr-82 27-aug-87

FAA, U.S AD 83-08-01

2 To preclude prop. attach bolt failures FINNISH AD M 1168/83 Rev 1 FINNISH AD T5114/05 HARTZELL SI 140A Rev 9

28-apr-82 2 20-May-2005 Ref. MU2B MM chap 13.4 when using bolts P/N B-3339 only

FAA, U.S AD 84-12-04

Torque of Air Tube Coupling Nuts SB 047/30-001, SB 196A

MAI SB 047/30-001 Rev A MITSUBISHI SB 196 Rev A

28-jun-84 27-jan-86

FAA, U.S AD 84-25-02

Elevator TrimTab Bracket Insp/Repl. SB 031/27-005 R1, SB 176E

MAI SB 031/27-005 Rev 1 MITSUBISHI SB 176 Rev E

18-dec-84 21-aug-85

FAA, U.S AD 86-

15-03


Rev B



2012-12-06


153(195)

FAA, U.S AD 86-

20-01


SB 020/34-005, SB 053A


MITSUBISHI SR 053A

06-Oct-

1986

27-mar-00

FAA, U.S AD 86-

26-02


iceing SB 74-0003, SR 040/74-001

GARRETT SB 74-0003 Rev 6 31-dec-87 09-mar-09 see applicable engine for c/o

FAA, U.S AD 87-

04-03


Insp SB 051/27-007, SB 198

MAI SB 051/27-007 MITSUBISHI SB 198 07-mar-87 27-aug-84

FAA, U.S AD 87-12-02

Generator Shield Jumper Wires MITSUBISHI SB 201 Rev A 03-jul-87 27-mar-09 N/A by s/n

FAA, U.S AD 88-

13-01


066/22-006


MITSUBISHI SB 206

11-jul-98 25-jul-89

FAA, U.S AD 88-

21-01




FAA, U.S AD 88-

23-01


067/27-008, SB 189B


FAA, U.S AD 93-

07-11


010


FAA, U.S AD 94-

04-16

Elevator trim tab mod. LFV LVD2537 MITSUBISHI SB 216 11-apr-94 07-May-1993

FAA, U.S AD 94-

11-04


016/61-001


FAA, U.S AD 96-

18-14

Inspection / Replacement of Prop

Hub. LVD 2732, Hx SB 136G

FINNISH AD M 2404/96 Rev 1 HARTZELL

SB 61-261 Rev 1 LFV LVD2732

16-Oct-

1996

01-sep-99 Prop utbytt mot S/N BVA-series

FAA, U.S AD 96-

25-02


4552-96 LFV LVD2749

27-dec-96 11-mar-02

FAA, U.S AD 97-

04-13

Vent Check Valve Assy LFV LVD2769 16-apr-97 05-May-1997 N/A N/A due to model.

FAA, U.S AD 97-

20-14 CNL


1997

02-dec-98

FAA, U.S AD 97-

25-02


ctrl/overspe


FAA, U.S AD 98-

20-39


MU-2 225, 089/57-002A

LFV LVD2688 , MITSUBISHI SB 225 19-Oct-

1998

04-dec-96


Aviation Adm

FINNISH AD M

3076

Kontroll av vindrutor och fönster FAA, U.S AD 2003-17-04 , MAI SB

087/56-001 Rev B , MITSUBISHI SB 224 Rev C

21-aug-03 08-mar-11


2012-12-06


154(195)

GARMIN, Garmin

GARMIN SB 0004 Incorp.of Main Software Version 2.16 01-May-2000

18-May-2000

GARMIN SSB 0844

IR Software Version 5.04 EASA SIB2008-58R1 14-nov-08 A 24-May-2010

GARRETT,

AlliedSignal

Aerospace

GARRETT SB 74-

0003

6 Replace Ignition Unit AD 74-0003 FAA, U.S AD 86-26-02 25-mar-94 09-mar-09 see applicable engine for c/o

HARTZELL,

Hartzell Propeller

Inc.

HARTZELL SB 61-

256

Propeller mounting bolt inspection MITSUBISHI SL 053/72-003, MITSUBISHI

SL 080

08-feb-02 24-apr-02 R/H side

HARTZELL SB 61-

279 ALERT

4 Prop. mounting bolt insp. FAA, U.S AD 2005-14-12 , MITSUBISHI SL

085

04-Oct-

2005

14-nov-05 propellerbolts previously checked u/a

HARTZELL SI 140A 9 Installation of Mounting Bolt FAA, U.S AD 83-08-01 Rev 2 , LFV

LVA1424 Rev A


JCAB, Japan Civil

Aviation Bureau

JCAB AD TCD-

0518-68


JCAB AD TCD-

0642-70

AFM revision regarding fuel spec. LFV LVA439 MITSUBISHI SB 112 Rev C 07-feb-70 21-aug-85 N/A by s/n

JCAB AD TCD-0643-70


JCAB AD TCD-0652-70


JCAB AD TCD-0653-70

Engine Nacelle Tail Area-Modification of 25-mar-70 26-mar-09 N/A by model

JCAB AD TCD-0660-70





2012-12-06


155(195)

JCAB AD TCD-

0730-1-72

Insp. and painting of maintanks LFV LVA543 Rev B MITSUBISHI SB 143

Rev B


JCAB AD TCD-

0730-2-86


JCAB AD TCD-

0859-72

Mod. of electrical system LFV LVA645 MITSUBISHI SB 156 04-sep-72 10-sep-72 N/A N/A due to model.

JCAB AD TCD-0866-72


31-dec-72 N/A N/A due to model.

JCAB AD TCD-

0947A-74

Kontr. & mod. av klaffdrivning LFV LVA828 Rev A MITSUBISHI SB 162

Rev A

12-nov-74 27-jan-86 N/A N/A due to s/n.

JCAB AD TCD-

0948A-1-78

Inspection of Windshields MITSUBISHI SB 163 Rev B 22-dec-78 26-mar-09 N/A by s/n

JCAB AD TCD-

0948A-74

Inspektion av frontrutor LFV LVA829 Rev A MITSUBISHI SB 163

Rev B

07-Oct-

1974

21-aug-85 N/A N/A due to s/n.

JCAB AD TCD-

1001A-76

Insp./repl. of elevator trim tab rod LFV LVA886 Rev A MITSUBISHI SB 176

Rev E

06-Oct-

1976

27-aug-84

JCAB AD TCD-

1001B-2-84


Bracket



12-dec-84 21-aug-85

JCAB AD TCD-

1094A-76

Insp. of wingflap controlsystem FAA, U.S AD 75-16-13 LFV LVA1011 Rev


06-sep-76 05-feb-02 N/A Ej tillämplig p.g.a. s/n.

JCAB AD TCD-

1188-75



06-May-

1975

21-aug-85

JCAB AD TCD-

1202-75

Engine Cowling Latches FAA, U.S AD 78-03-05 LFV LVA1014 Rev

A MITSUBISHI SB 171 Rev B MITSUBISHI

SB 180 Rev A


JCAB AD TCD-

1209-75


locking

LFV LVA1013 MITSUBISHI SB 169 Rev B 16-jun-75 27-jan-86

JCAB AD TCD-

1235-75


emerg.cables

LFV LVA1083 MITSUBISHI SB 170 Rev A 19-sep-75 21-aug-85 N/A N/A due to model.

JCAB AD TCD-

1272-75


Mech.-I&M


JCAB AD TCD-

1284-1-76

Prevent failure of MLG. dragstrut MITSUBISHI SB 173 Rev A 31-mar-76 09-nov-09 PCW Carried out ref SB 173, date 1985/08/21

JCAB AD TCD-

1328-76


compartment


JCAB AD TCD-

1353-76


Repl.

MITSUBISHI SB 175 16-aug-76 26-mar-09

JCAB AD TCD-

1370-76


1976

27-jan-86 N/A by s/n


2012-12-06


156(195)

JCAB AD TCD-

1370A-81



MITSUBISHI SB 174 PART 1 Rev C 05-nov-81 24-mar-09 N/A by s/n

JCAB AD TCD-

1379-1-80

Insp. rear eng. cowling reg. heatdamage LFV LVA1197 Rev A MITSUBISHI SB 177

Rev B

06-feb-02 27-jan-86

JCAB AD TCD-

1520A-77



Fatigue failure of the NLG strut assy. LFV LVA1546 MITSUBISHI SB 181 PART 2 Rev B

12-jul-85 15-jul-04 PCW Found SB 181 part 2 PCW.

JCAB AD TCD-

1817-79

Modification of bagagecompartment LFV LVA1583 MITSUBISHI SB 182 05-feb-02 27-May-1986 N/A N/A due to s/n.

JCAB AD TCD-

2048-81

Insp. firewarning & emerg.power circuit LFV LVA1740 MITSUBISHI SB 187 Rev B 05-feb-02 27-May-1981 N/A N/A due to s/n.

JCAB AD TCD-

2070-81

Inspect NLG downlock mechanism LFV LVA1753 MITSUBISHI SB 188 05-feb-02 27-aug-84

JCAB AD TCD-

2113-82

Insp./replace engine electrical harness LFV LVA1788 MITSUBISHI SB 191 06-feb-02 27-aug-84

JCAB AD TCD-

2252-2-88

Flap system torquetubes supersed TCD-

2252-1-87

01-feb-89 24-mar-09 PCW

JCAB AD TCD-

2252-83


JCAB AD TCD-

2263-83


JCAB AD TCD-

2342-1-84

Engine inlet anti-ice tubing. Torq./lock MITSUBISHI SB 196 Rev A 05-jun-84 10-mar-09 PCW

JCAB AD TCD-

2342-84

Engine inlet anti-ice tubing. Torq./lock LFV LVA1942 MITSUBISHI SB 196 Rev A 06-feb-02 27-jan-86

JCAB AD TCD-

2450A-87


JCAB AD TCD-

2451-1-87


1987


JCAB AD TCD-

2451-85



LFV LVD2037 MITSUBISHI SB 198 30-sep-85 27-aug-84

JCAB AD TCD-

2545-1-88

Generator System LFV LVD2191 MITSUBISHI SB 201 Rev A 01-jul-88 24-mar-09 N/A by s/n


Auto-ignition System FINNISH AD M 2435/97 LFV LVD2761 01-feb-97 22-nov-01


Bendix M4C Autopilot System MITSUBISHI SB 206 05-nov-97 06-nov-09 N/A Due to model

JCAB AD TCD-3378-90

Insp./mod. of rudder trimtab leadingedge



2012-12-06


157(195)

JCAB AD TCD-

3393A-96

Anti ice/De-ice system FINNISH AD M 2364/96 LFV LVD2347

Rev 1 MITSUBISHI SB 212 Rev A

25-May-

1996

11-feb-10

JCAB AD TCD-

3464-91


JCAB AD TCD-

3740A-98


MSB 216, 228 LVD 2898


LFV LVD2898 MITSUBISHI SB 216 MITSUBISHI SB 228

17-aug-98 09-nov-98

JCAB AD TCD-

3901-93

Tiptank inst FINNISH AD M 2110/93 LFV LVD2512

MITSUBISHI SB 221

10-sep-93 25-apr-94

JCAB AD TCD-

3942-1-94

Inspection of landing gear lower pin FINNISH AD M 2238/95 LFV LVD2592


28-nov-94 27-mar-95

JCAB AD TCD-

3942-94


JCAB AD TCD-

4310-96


MITSUBISHI SB 225

01-apr-96 04-dec-96

JCAB AD TCD-

4311-95



01-nov-95 08-mar-11

JCAB AD TCD-4379-96

Feathering Valve/Linkage insp. FINNISH AD M 2352/96 LFV LVD2689 MITSUBISHI SB 229

01-apr-96 30-jul-96

JCAB AD TCD-4552-96

Icing Limitation FAA, U.S AD 96-25-02 LFV LVD2749 27-dec-96 11-mar-02

JCAB AD TCD-4625-97

Mod.of Trimsystem/AFM Revision FINNISH AD M 2460/97 UPPHÄVD MAI SB 093/22-009

14-jul-97 15-May-2001

JCAB AD TCD-

4625A-2001


NYGE TDM01-45

16-mar-01 13-mar-09 PCW

JCAB AD TCD-

4626-97



01-May-

1997

14-jul-04 PCW

JCAB AD TCD-

4684-97


MITSUBISHI SB 230

01-jun-97 25-mar-99

JCAB AD TCD-

4753-98

Ändring av flyghandbok LVD 2922,FAA

AD 97-20-14, MHI SN 117A




JCAB AD TCD-

4753A-2004

Icing-related incidents VIDEO FAA, U.S AD 2003-22-07 Rev 1 24-feb-04 17-May-2004 inserted in AFM limitations

JCAB AD TCD-

4838-98

Inspection of landing gear power train FINNISH AD M 2574/98 LFV LVD2897

MITSUBISHI SB 235


JCAB AD TCD-

4889-2-2007


JCAB AD TCD-

4889-98





05-nov-98 14-jul-04 PCW


2012-12-06


158(195)

JCAB AD TCD-

4890-98

Check of flight idle FF LVD 2925, MU SB

234


MITSUBISHI SB 234

04-nov-98 11-feb-10

JCAB AD TCD-

5030-99


1999


JCAB AD TCD-

5432-2000




JCAB AD TCD-

5747-2001

Inspection of Tip Tank Brackets LFV LVD3166 MITSUBISHI SB 236 12-sep-01 18-Oct-2001

JCAB AD TCD-

5864-2001


JCAB AD TCD-

6127-2003

Pneumatic Line insp. LFV LVD3322 MITSUBISHI SB 239 17-mar-03 02-Oct-2003

JCAB AD TCD-

7030-2006


Hardware


LFV,

Luftfartsverket



05-feb-02 A 05-feb-02 N/A Ej tillämplig p.g.a. s/n.



05-feb-02 05-feb-02 N/A Ej tillämplig p.g.a. s/n.

LFV LVA 1013 Kontr. och mod. av låsning på nosställ JCAB AD TCD-1209-75 MITSUBISHI SB 169 Rev B

05-feb-02 27-jan-86

LFV LVA 1014 A Kontr. & byte av motorinkl. låsanordning

FAA, U.S AD 78-03-05 JCAB AD TCD-1202-75 MITSUBISHI SB 171 Rev B MITSUBISHI SB 180 Rev A

05-feb-02 A 21-aug-85


05-feb-02 21-aug-85 N/A N/A due to s/n

LFV LVA 1196 Isolering av strobe light från bränsle JCAB AD TCD-1370-76 MITSUBISHI SB 174 PART 1 Rev C

06-feb-02 06-feb-02 N/A by s/n

LFV LVA 1197 A Förhindr. av värmeskador på bak.motorpl.

JCAB AD TCD-1379-1-80 MITSUBISHI SB 177 Rev B

06-feb-02 A 27-jan-86

LFV LVA 1238 Kontr. & byte av infästningsdet. trimrod 06-feb-02 21-apr-09 N/A by s/n

LFV LVA 1546 Sprickundersökning av nosställ FAA, U.S AD 86-15-03 JCAB AD TCD-1768-1-85 MITSUBISHI SB 181 PART 2

Rev B

06-feb-02 27-May-1986


2012-12-06


159(195)

LFV LVA 1583 Modifiering av bagageutrymme JCAB AD TCD-1817-79 MITSUBISHI SB

182

05-feb-02 11-feb-80 N/A N/A due to s/n.


n"dstr"mskret


187 Rev B


LFV LVA 1753 Kontroll av låsmekanism i nosställ JCAB AD TCD-2070-81 MITSUBISHI SB

188

05-feb-02 27-aug-84



06-feb-02 27-aug-84

LFV LVA 1873 Insp./utbyte av infäst.till torsionsrör JCAB AD TCD-2252-83 MITSUBISHI SB

189 Rev C

06-feb-02 11-mar-96


varmlufts


196 Rev A

06-feb-02 27-jan-86

LFV LVA 438 Justering av bränslemängdsmätare JCAB AD TCD-0643-70 MITSUBISHI SB

114

05-feb-02 21-aug-85 N/A N/A by s/n

LFV LVA 439 Rev. av flyghandbok betr. bränslespec. JCAB AD TCD-0642-70 MITSUBISHI SB

112 Rev C

05-feb-02 21-aug-85 N/A by model

LFV LVA 456 Inspektion av bultar i nossst,ll JCAB AD TCD-0652-70 MITSUBISHI SB

119

05-feb-02 26-mar-09 N/A by model

LFV LVA 457 Utbyte av lager i nosst,llets st"td,mp. JCAB AD TCD-0660-70 MITSUBISHI SB

123

05-feb-02 26-mar-09 N/A by s/n


LFV LVA 645 Modifiering av el-system JCAB AD TCD-0859-72 MITSUBISHI SB 156

05-feb-02 08-dec-09 N/A by A/C serial number

LFV LVA 664 Nosställsväxellåda och struktur JCAB AD TCD-0866-72 05-feb-02 31-aug-09 N/A by s/n & model

LFV LVA 828 A Kontr. & mod. av klaffdrivning JCAB AD TCD-0947A-74 MITSUBISHI SB 162 Rev A

05-feb-02 A 27-jan-86 N/A N/A due to s/n.

LFV LVA 829 A Inspektion av frontrutor FAA, U.S AD 74-11-01 FAA, U.S AD 75-03-06 JCAB AD TCD-0948A-74


05-feb-02 A 21-aug-85 N/A N/A due to s/n.

LFV LVA 886 A Kontroll/byte av höjdtrimroderarmar JCAB AD TCD-1001A-76 05-feb-02 A 27-aug-84

LFV LVD 1238 Kontr./byte infästn.det. höjdtrimroder 15-apr-77 31-aug-09 N/A by s/n

LFV LVD 1971 Elevator Trim Tab MU2 SB 176E JCAB AD TCD-1001B-2-84 MITSUBISHI

SB 176 Rev E

18-jan-85 27-May-1986


Rev A, MHI SR 53



24-May-

1985

B 21-aug-85

LFV LVD 2037 Flap Flexible Shaft MU2 SB 198 JCAB AD TCD-2451-85 MITSUBISHI SB 30-sep-85 27-May-1986


2012-12-06


160(195)

198

LFV LVD 2069 Altimeter 25-mar-86 27-May-1986 N/A N/A by p/n & s/n


26-jan-87 19-feb-87



19-aug-88 25-jul-89


201 Rev A

19-aug-88 24-mar-09 N/A by s/n

LFV LVD 2202 Kontr. av koppl. för tors.rör till klaff FAA, U.S AD 88-23-01 JCAB AD TCD-

2252-1-87 MAI SB 067/27-008 Rev A MITSUBISHI SB 189 Rev C

08-dec-88 11-mar-96


12-feb-02

LFV LVD 2338 Kont./Mod.av sidorodrets trimroderframka Mitsubishi MHI SB 211



LFV LVD 2347 1 Control Deice-system Mitsubishi SB 212A

JCAB AD TCD-3393A-96 MITSUBISHI SB 212 Rev A

29-May-1996

1 11-feb-10

LFV LVD 2352 Shoulder Harness Inst. FAA AC 43-13 CHPT 9

23-May-1991



216


216

03-dec-92 07-May-1993

LFV LVD 2477 Electric Trim System AD930711, MU SB

079/27-0-010

FAA, U.S AD 93-07-11 MAI SB 079/27-

010

03-jun-93 27-mar-09 N/A by s/n

LFV LVD 2512 TIP TANK INST. (NXT 100H) JCAB AD TCD-3901-93 MITSUBISHI SB

221

02-dec-93 25-apr-94

LFV LVD 2537 Reducering av Höjdrodrets trimområde.

FAA AD 94-04-16, SB 216

FAA, U.S AD 94-04-16 MITSUBISHI SB

216

07-apr-94 07-May-1993


219


219 Rev A

07-apr-94 27-mar-95



TCD-3942-1-94, MSB 219A


219 Rev A

09-feb-95 27-mar-95

LFV LVD 2678 Kontr. av vindrutor och fönster MHI SB

224 Rev A



12-mar-96 08-mar-11

LFV LVD 2688 Kontr/byte av infästn.bult för tiptank MU-2 SB 225

FAA, U.S AD 98-20-39 JCAB AD TCD-4310-96 MITSUBISHI SB 225

09-May-1996

04-dec-96

LFV LVD 2689 Kontroll av linkage för prop.flöjning MU-2 SB 229


09-May-1996

30-jul-96


2012-12-06


161(195)

LFV LVD 2732 Inspection/ Replacement of Prop Hub.

FAA AD 96-18-14, Hz SB 136H


261 Rev 1

27-sep-96 01-sep-99 Prop. utbytt mot BVA


4552-96


4552-96

21-jan-97 11-mar-02

LFV LVD 2761 Installation av autoignition system TCD-

2679A-97


226 Rev E

14-feb-97 05-mar-99



18-mar-97 05-May-1997 N/A N/A due to s/n.




232 Rev A

28-aug-97 10-May-1998

LFV LVD 2819 Mod.av lagerboxar för landställssystem

Mitsubishi SB 230


230

18-nov-97 18-mar-98

LFV LVD 2897 Kontroll av landst,llets drivsystem TCD-

4838-98, SB 235


235


LFV LVD 2898 Mod. av autopilotens höjdtrimsystem

TCD-3740A-98, SB 216, 228



27-aug-98 09-nov-98

LFV LVD 2922 Änd.av Flyghandbok-Extra krav på

typutbi TCD-4753-98, MHI SN 117A

JCAB AD TCD-4753-98 MITSUBISHI SN

117 Rev D





233 Rev B

01-dec-98 03-jun-99

LFV LVD 2925 Kontr/just av mot bränsleflöde Flight Id

MHI SB 234


234

01-dec-98 20-apr-99

LFV LVD 2988 Sprickkontroll av kroppsspant JCAB AD TCD-5030-99 MITSUBISHI SB

209 Rev B



LFV LVD 3122 Modifiering av autopilotsystemet JCAB AD TCD-4625A-2001 MAI SB 093/22-009 MITSUBISHI SB 231 Rev B NYGE TDM01-45

02-apr-01 15-May-2001




20-sep-01 18-Oct-2001


09-jan-02 17-jan-02


21-mar-03 02-Oct-2003

MAI, Mitsubishi

Aircraft


2012-12-06


162(195)

International

MAI SB 047/30-

001

A Torque of Bleed Air Tube Coupling Nuts

AD 84-12-04,SB 196A

FAA, U.S AD 84-12-04 MITSUBISHI SB

196 Rev A

19-jul-84 A 27-jan-86

MAI SB 051/27-

007

Add.Seal and Flap Flexible Shaft Torque

AD 87-04-03, SB 198

FAA, U.S AD 87-04-03 01-feb-85 27-aug-84

MAI SB 066/22-

006

Bendix autopilot disengagement 21-Mar-12

MAI SB 067/27-

008




MAI SB 069/24-

006

Split Radio Bus Inspection and Rework MAI SB 066/22-006 Rev A 17-nov-88 25-jul-89 N/A N/A due to Aircraft s/n

MAI SB 086/74-002


05-Oct-2000


MAI SB 089/57-002

A Insp/Repl. of Bolts for Wing Tip Tank FAA, U.S AD 98-20-39 05-nov-96 A 04-dec-96 N/A N/A due to s/n.

MAI SN 110/00-017A


MAI SN 111/77-004


MAI SR 020/34-005



06-Oct-1986

27-mar-00 N/A N/A due to s/n.

MITSUBISHI,

Mitsubishi Heavy

Industries Ltd

MITSUBISHI MSB

24-002

A **RECOVERED RECORD** 27-aug-84 N/A

MITSUBISHI MSB

24-004

**RECOVERED RECORD** 17-Oct-

1984

N/A


**RECOVERED RECORD** 27-aug-84 N/A







MITSUBISHI MSB **RECOVERED RECORD** 27-aug-84 N/A


2012-12-06


163(195)

27-007

MITSUBISHI MSB

30-001


MITSUBISHI MSB

32-001


MITSUBISHI MSB

32-004


MITSUBISHI MSB

32-006


MITSUBISHI MSB

32-010

**RECOVERED RECORD** 07-jul-86 N/A










B **RECOVERED RECORD** 27-aug-84 N/A



MITSUBISHI MSR 066

B **RECOVERED RECORD** 19-feb-87

MITSUBISHI SB 066

Bendix M4D 18-dec-87 25-jul-89

MITSUBISHI SB 076/22-008

M-4() Autop.Engage Switch Guard Install.

11-apr-91 07-dec-94

MITSUBISHI SB

112


1971

C 21-aug-85

MITSUBISHI SB

114


MITSUBISHI SB

119

The Bolt and Bolt Hole Diam. of Nose

L.G


MITSUBISHI SB

123

Bearing,Oleo Strut,Nose L.G. -Repl. of JCAB AD TCD-0660-70 LFV LVA457 01-apr-70 26-mar-09 N/A by s/n

MITSUBISHI SB

124

Scissors Switch,Nose L.G. -Install. of 31-aug-70 21-aug-85 N/A


2012-12-06


164(195)

MITSUBISHI SB

128


MITSUBISHI SB

143

B Top Coating, Wing Integral Main F.T.-

SIo


0730-2-86


MITSUBISHI SB

162

A Flex. Shafts, Flap Control Sys.-Insp. of

(AD750201)

JCAB AD TCD-0947A-74 LFV LVA828 Rev

A

03-Oct-

1974

A 27-jan-86 N/A due to S/N

MITSUBISHI SB 163

B Insp. of Outer Pane, Front Winds. & Inst FAA, U.S AD 74-11-01 JCAB AD TCD-0948A-1-78 JCAB AD TCD-0948A-74 LFV

LVA829 Rev A

16-nov-78 21-aug-85 N/A

MITSUBISHI SB

165

A Lubr. Interval,Wheel Bearing,Main &

Nose

24-jul-80 21-aug-85 N/A

MITSUBISHI SB

167

D Flap M.Jack Screw-Insp. of and/or Main

G



24-jul-80 D 05-feb-02 N/A Ej tillämplig p.g.a. s/n.

MITSUBISHI SB

168


(AD761620)


1188-75 LFV LVA1012

24-jul-80 A 21-aug-85

MITSUBISHI SB

169

B Shimmy Damper-Insp. and Modification

of


MITSUBISHI SB 170


JCAB AD TCD-1235-75 LFV LVA1083 24-mar-77 A 21-aug-85 N/A N/A due to s/n

MITSUBISHI SB 171



17-nov-77 B 21-aug-85

MITSUBISHI SB 173

A Drag Strut, Main L.G.-Modification of JCAB AD TCD-1284-1-76 24-jul-80 21-aug-85

MITSUBISHI SB

174 PART 1


Rew.of (AD830902)


1370A-81 LFV LVA1196

02-Oct-

1981

C 27-jan-86 N/A by s/n

MITSUBISHI SB

174 PART 2

C Tip Tank Conduit Tube Rework 02-Oct-

1981

C 27-jan-86 N/A N/A by A/C S/N

MITSUBISHI SB

175


Repl.

JCAB AD TCD-1353-76 26-jun-76 21-aug-85

MITSUBISHI SB

176

E Elevator Trim Tab Bracket-Repl. of

LVD1971, AD 84-25-02, SB 031/27-005R1



26-sep-84 E 21-aug-85

MITSUBISHI SB 177

B Mod. of Engine Nacelle Tail Area (AD810601)

JCAB AD TCD-1379-1-80 LFV LVA1197 Rev A

11-sep-80 B 27-jan-86

MITSUBISHI SB 179


27-May-1977

21-aug-85

MITSUBISHI SB 180

A Link, Engine Nacelle Upper D.-Repl. of (AD780305)

FAA, U.S AD 78-03-05 JCAB AD TCD-1202-75 JCAB AD TCD-1520A-77 LFV

LVA1014 Rev A

17-nov-77 A 21-aug-85


2012-12-06


165(195)

MITSUBISHI SB

181 PART 2

B Insp. and Repl. of Nose L.G. Strut Assem

(AD801812)


1768-1-85 LFV LVA1546

08-apr-85 B 27-May-1986

MITSUBISHI SB

182

Add. of Ceiling Cover, Rear Bagg. Comp. JCAB AD TCD-1817-79 LFV LVA1583 16-nov-79 27-May-1986 N/A N/A due to s/n.

MITSUBISHI SB

184

Turnbuckle, Control Cables -Repl. of 04-apr-80 21-aug-85

MITSUBISHI SB 188

Down Lock Mech., Nose L.G.-Insp. of JCAB AD TCD-2070-81 LFV LVA1753 13-jul-81 27-aug-84

MITSUBISHI SB

189

C Flap Control Torque Tube AD 88-23-01,

SB 067/27-008


2252-1-87 JCAB AD TCD-2252-83 LFV

LVA1873 LFV LVD2202

28-jun-94 C 11-mar-96

MITSUBISHI SB

191

Engine El. Wire-Insp. and Replacement

of (AD820802)

JCAB AD TCD-2113-82 LFV LVA1788 21-dec-81 27-aug-84

MITSUBISHI SB

193

B Landing Gear Warning Horn Syst.Modif. 15-jun-94 B 04-dec-00 Rev A är utförd.

MITSUBISHI SB

194

Master Cauting Light Visibility-Impr. of 23-aug-82 27-aug-84

MITSUBISHI SB 196

A Ret. of coupling nut on the bleed air tu AD 84-12-04, SB 047/30-001

FAA, U.S AD 84-12-04 JCAB AD TCD-2342-1-84 JCAB AD TCD-2342-84 LFV

LVA1942 MAI SB 047/30-001 Rev A

12-apr-84 A 27-jan-86

MITSUBISHI SB

198

Add. Seal & Torque Insp. of Flap Flex.Sh

LVD2037, AD 87-04-03, SB 051/27-007


2451-85 LFV LVD2037

13-feb-85 27-aug-84

MITSUBISHI SB

199


Protec


MITSUBISHI SB

200

B Insp of Nose Ldg Gear Drag Strut Link 24-jun-94 A 07-Oct-1988

MITSUBISHI SB

201

A Generator Circuit Wires Insp. and Mod. FAA, U.S AD 87-12-02 JCAB AD TCD-

2545-1-88 LFV LVD2191

02-mar-88 A 24-mar-09 N/A by s/n

MITSUBISHI SB 204

Speed Placard Change 03-mar-87 02-May-1988

MITSUBISHI SB 206

Bendix Autop.Disengagement Method Stand.


13-Oct-1987

06-nov-09 N/A Due to model

MITSUBISHI SB 207

Rudder T.T. & Elevator T.T. Insp. & Rep. 20-May-1988

11-feb-10

MITSUBISHI SB 209


MITSUBISHI SB 210


MITSUBISHI SB

211

Rudder Trim Tab Modification (LVD

2338)



2012-12-06


166(195)

MITSUBISHI SB

212

A Insp of Anti-ice/Deice Systems (LVD

2347),


Rev 1

25-apr-96 A 26-May-2010

MITSUBISHI SB

214

Engine Control Rod Inspection 06-dec-91 01-sep-92

MITSUBISHI SB

215

Removel of Prop. Governor Speed

Signal

23-Oct-

1991

28-feb-92

MITSUBISHI SB 216

Elevator Trim Tab Installation (LVD 2450

FAA, U.S AD 2007-17-09 FAA, U.S AD 94-04-16 JCAB AD TCD-3740A-98 LFV


11-sep-92 07-May-1993

MITSUBISHI SB

218

A Propeller Feathering Linkage Inspection 17-jan-94 A 25-apr-94

MITSUBISHI SB

219

A Emergency Gear Down G.box Lower Pin

Repl


3942-94 LFV LVD2538 LFV LVD2592

24-Oct-

1994

A 27-mar-95

MITSUBISHI SB

221

Tip Tank Conduit Tube Insp. and Rep. JCAB AD TCD-3901-93 LFV LVD2512 10-aug-93 25-apr-94

MITSUBISHI SB

223

Pitot/Static System Improvement SR

064

MITSUBISHI SR 053A MITSUBISHI SR 064 28-jun-94 27-mar-00

MITSUBISHI SB 224

C Acrylic Windsheild/Window glass Insp. FAA U.S AD 2003-17-04, FINNISH AD M 3076, JCAB AD TCD-4311-95, LFV

LVD2678

30-apr-98 C 08-mar-11

MITSUBISHI SB

225

Forward fitting bult of wingtip tank LVD

2688



29-sep-95 04-dec-96

MITSUBISHI SB 226


FAA, U.S AD 2000-09-15 Rev 1 FAA, U.S AD 86-26-02 FINNISH AD M 2435/97 FINNISH AD M 2786/00 JCAB AD TCD-



MITSUBISHI SB 227

Rudder Torque Tube Modification 20-dec-96 10-apr-97

MITSUBISHI SB 228


FAA, U.S AD 2007-17-09 FINNISH AD M 2581/98 JCAB AD TCD-3740A-98 LFV LVD2898

13-jul-98 09-nov-98

MITSUBISHI SB 229

Feathering Valve/Linkage Insp. FAA, U.S AD 2006-15-07 JCAB AD TCD-4379-96 LFV LVD2689

20-feb-96 30-jul-96

MITSUBISHI SB 230

Mod.of Bearing Box Ldg. Gear Act. LVD 2819

JCAB AD TCD-4684-97 LFV LVD2819 05-mar-97 18-mar-98

MITSUBISHI SB 231

B Inst.of Trim-In-Motion Alert System FAA, U.S AD 2000-09-15 Rev 1 FINNISH AD M 2460/97 UPPHÄVD FINNISH AD M

2786/00 JCAB AD TCD-4625A-2001 LFV



2012-12-06


167(195)

LVD3122

MITSUBISHI SB

232

A De-Ice System Modification LVD 2800,

TCD-4626-97

FAA, U.S AD 2000-09-15 Rev 1 FINNISH

AD M 2786/00 JCAB AD TCD-4626-97 LFV LVD2800 MAI SB 096/30-004

06-jun-02 A 06-jun-02 N/C due to previuosly complied with SB 232 rev

0.

MITSUBISHI SB 233

B Insp.of Engine Torque Indication System. TCD-4889-98, LFV 2924

FAA, U.S AD 2006-17-01 FINNISH AD M 2608/98 JCAB AD TCD-4889-2-2007

JCAB AD TCD-4889-98 LFV LVD2924


MITSUBISHI SB 234



07-Oct-1998

11-feb-10

MITSUBISHI SB 235

Inspection of landing gear power train JCAB AD TCD-4838-98 LFV LVD2897 04-aug-98 24-mar-09 N/A by model

MITSUBISHI SB 236

Inspection of Tip Tank Brackets JCAB AD TCD-5747-2001 LFV LVD3166 28-aug-01 18-Oct-2001

MITSUBISHI SB 237

Inspection of Flap Drive Train JCAB AD TCD-5864-2001 LFV LVD3212 13-dec-01 17-jan-02

MITSUBISHI SB 238


MITSUBISHI SB 239

Pneumatic Line Insp. and Modification JCAB AD TCD-6127-2003 LFV LVD3322 26-dec-02 02-Oct-2003

MITSUBISHI SB 240

Inst.of Trottle Quadrant Placard 26-feb-03 02-Oct-2003

MITSUBISHI SB 241

A Inspection of Wing Attachment Hardware



MITSUBISHI SL

060

System 17-feb-89 20-aug-91

MITSUBISHI SL

078

Automatic Autopilot Disconnect System 28-jan-02 26-May-2010

MITSUBISHI SL

079

Diode inst.in Flap Position Ind.Curcuit 28-jan-02 15-May-2001 Carried out by Mitsubishi (manufacturing-

made)

MITSUBISHI SL

080

Hartzell Propeller Mounting Bolt Insp. HARTZELL SB 61-256 05-apr-02 26-aug-02 Compliance in according to HC-SB-61-256.

MITSUBISHI SL

084

Pneumatic De-Ice Monitoring System 14-jun-04 26-May-2010

MITSUBISHI SL

085


2005

20-sep-05

MITSUBISHI SN 053


05-nov-86 B 22-dec-87

MITSUBISHI SN 117

D Icing Awareness Training Video FAA, U.S AD 2003-22-07 Rev 1 JCAB AD TCD-4753-98 LFV LVD2922

14-jun-04 D 17-May-2004


2012-12-06


168(195)

MITSUBISHI SN

146

Water Ingress into Vertical Stabilizer 19-dec-03 24-feb-04

MITSUBISHI SN

148


MITSUBISHI SN

156A


MITSUBISHI SN 157


MITSUBISHI SN

161


MITSUBISHI SR

053A


2450A-87 LFV LVD2015 Rev B MAI SR

020/34-005 MITSUBISHI SB 223

23-Oct-

1984

08-May-1998

MITSUBISHI SR

064

Pitot & Static System MITSUBISHI SB 223 30-apr-85 27-mar-00

MITSUBISHI SR

065

Warning Horn 20-jan-86 22-dec-87

MITSUBISHI SR 067

Emergency Exit Placard 17-sep-85 27-May-1986

MITSUBISHI SR 072

Air Filter Replacement for Vacuum Syst. 25-apr-00 24-feb-04

MITSUBISHI SR 075

Inst. tip tank placard 29-Oct-2004

04-apr-05

MITSUBISHI STC

SA01913SE


NARCO, Narco

NARCO SB ELT10-

16


NYGE, Saab Aerotech Aircraft

Services

NYGE TDM 00-09 Operatörsplats MU-2 11-apr-00 12-jan-00

NYGE TDM 00-23 Wiring Left Wing ADRIAN 22-dec-00 08-Oct-1999

NYGE TDM 02-24 Installation Moving MAP 10-Oct-

2002

29-Oct-2002


2012-12-06


169(195)


NYGE TDM 03-08 8 GNS430/530 & MODE S

GTX330 install.

04-mar-03 20-Oct-2008


NYGE TDM 06-41 A Darts (to carry on MU-2B-20/26)

20-nov-06 A 07-feb-08


NYGE TDM 07-30 A Install. of Emergency Axe 28-feb-08 A 07-mar-08

NYGE TDM 08-03 A Enhanced Surveillance MU-2B 28-feb-08 A 07-sep-09

NYGE TDM 08-28 B ELT 406 MU-2B 29-sep-08 B 20-Oct-2008 Original compliance with TDM rev A. Rev B does not affect previous complaiance.

NYGE TDM 09-02 C U-95 SORC Lite MU-2B 15-dec-09 C 29-apr-10 Original compliance I.A.W rev is not affected by rev C.

NYGE TDM 09-07 A GPS Splitter 18-May-2009

A 10-jun-09

NYGE TDM 10-02 A Target surveillance camera 03-jun-10 A 01-Oct-2010

NYGE TDM 10-03 A Pressure Bulkhead Feed Through

04-May-2010

A 04-Oct-2010

NYGE TDM 10-25 A MU-2B Terminating Resistor 08-apr-10 A 18-May-2010 C/W


NYGE TDM 12-21 A Avinstallation IK 14-Aug-12



NYGE TDM 99-09 Installation BRNAV MU-2 01-nov-99 30-Oct-1999

NYGE TVO 1/09 Inspektion av Stringers &

struktur vinge

25-feb-09 02-mar-09 Inspected u/a

NYGE TVO 1/93 Low Volt Warning Light (BCL) 22-jan-93 07-May-1993

NYGE TVO 1/96 Slitage Flap Guide Rail 12-apr-96 20-apr-99


korrosionskontroll

12-feb-97 11-feb-97

NYGE TVO 2/00 Märkning av infästning domkraft Mu2

01-dec-00 29-jan-01


2012-12-06


170(195)

NYGE TVO 2/07 A Prevent FR31 radio to xmit

when RM2 off

06-feb-07 A 27-feb-07

NYGE TVO 2/10 1 Visual inspection of center

wing

19-apr-10 08-mar-11

NYGE TVO 2/91 A/C Elecrical System 10-jan-91 26-apr-91

NYGE TVO 3/06 Inspect lower rudder hinge

bracket

07-dec-06 08-mar-11

NYGE TVO 3/96 3 Wing Spar Flange Inspection. 24-feb-05 3 11-feb-10

NYGE TVO 4/11 A Static inverter controll A 15-Dec-11

NYGE TVO 4/91 Special Inspection (next E6.) 19-feb-91 07-dec-91

NYGE TVO 4/92 Engine Install. Kontr.

rörledningar

29-apr-92 19-May-1992

NYGE TVO 4/94 3 Fwd. Wing Tiptank Attachment 28-sep-94 11-feb-10


25-Oct-1996

26-aug-97 Utförd tidigare (ref. Ove N lista)

NYGE TVO 6/88 Allm. instruktion för metallpropeller

13-jun-88 08-mar-11


19-Oct-1992

NYGE TVO 7/05 RMI-nål park. ej / ILS frekvens är vald

11-nov-05 25-nov-05 Carried out i.a.w. drawing NA-MF-199-008 & NA-MF-199-009

NYGE TVO 7/93 Starter Drive Splines 01-nov-93 07-dec-94


07-May-1993


2012-12-06


171(195)

2.7 GFE Aircraft Mitsubishi MU-2 SE-IUA


Number:


total Hours:

Total

Landing

Cycles:

Date

Reference:

MU-2B-26 345 SE-IUA 10619 4226 2012-11-23


Serial

Number:

Total Hours

Since New:

Total

Cycles

Since New:

Hours remaining

overhaul/HSI/GBI:

Left Engine P20461 10937 9971 2876/667/2467

Right Engine P20502 7706 8168 439/835/2317





Autopilot & Flight Director Bendix M4D

COM/NAV/GPS 1 & 2 Garmin GNS 430


MKR Bendix/King KMR 675

DME Bendix/King KN 63

ADF Bendix/King KR 87

XPDR 1 Garmin GTX 330D

XPDR 2 Garmin GTX 330 *)




0161

Altimeter LH Aerosonic 101735-01555


Altitude Reporter Ameri-King AK-350

Altitude Alerter Century 1D960


Attitude Gyro & Flight Director Ind. Bendix GH-14


2012-12-06


172(195)

LH


Turn & Bank Ind. LH Bendix 4099-B

Horizontal Situation Indicator LH Bendix RD-44


RMI Indicator Collins 332C-10






VHF/UHF COM FR31

GPS MAP


Laser Prism


Wing Pylon


EW system


Pylon




Chaff Dispenser


Pylon

Target Towing

MBV7S Inboard winch



TAPS

Radar Calibration System

GPS Sphere


System:


Adrian C & S, A100, DARTS

and BOX 3 General Signal Harness AWG22 shielded x 44


A100 MIL-STD-1553B Data

Bus

Triax Cable x 1


2012-12-06


173(195)

A100 and DARTS AC Power

115/200VAC 400 Hz 3-

Phase 3 x 10 A

AWG 16 x 4

twisted

AWG 16 x 2


A

DC Power 28 VDC 200

A

AWG 2 x 2




2012-12-06


174(195)


rd 2012.

Description Maint. RefC/Out date C/Out Hrs Due Hrs Due date

Aircraft SE-IUA

Vingstudie MU-2 AMP 10000 11000








1 Year Inspection AMP 2012-04-23 10577





Engine Hot Section Inspection AMP 11286,3 667

Engine Gearbox Inspection AMP 13086,3 2467

Engine S/N P-20502


Engine Hot Section Inspection AMP 11455 835,7




Unclassified Date FMV Document ID Subject type

2012-12-06 ange ange


ange 175(195)


rd 2012.

SB/AD etc

Reference


e

Statu

s

Remarks

SB/AD etc

Reference

Rev Subject Document reference Eff. date Rev Compliance Stat

us

Remarks


Safety Agency

EASA AD 2006-0265

Incorrect transponder altitude 30-aug-06

14-mar-09

EASA AD 2009-0251-E

Portable Fire Extinguishers-Ident/Repl 25-nov-09

07-May-2010 N/A N/A by current P/N installed

EASA AD 2009-0262

Halon 1211 Fire Extinguishers Id/Repl EASA AD 2009-0278 FFE ASB26-115 Rev C 15-dec-09


EASA AD 2009-0278

Halon 1211 Fire Extinguishers Id/Repl EASA AD 2009-0262 22-dec-09


EASA AD 2010-0003



EASA AD 2012-0037

Kidde Gravinier hand operated fire extinguisher

4-May-12

EASA SIB 2008-58R1


17-dec-08

21-sep-10 N/A by SSB 0844 incorporated


FAA, U.S, Federal

Aviation

Administration

FAA, U.S AD 2000-

02-25


FAA, U.S AD 2000-09-15

1 Flight in Icing Condition FINNISH AD M 2435/97 FINNISH AD M 2786/00 MAI SB 086/74-002 Rev A MAI SB

07-jul-00 1 22-nov-01 Action not required due to s/n.

Öppen/Unclassified Datum Diarienummer Ärendetyp


Dokumentnummer Sida

ange 176(195)

093/22-009 MAI SB 096/30-004 MITSUBISHI SB 226 Rev E MITSUBISHI SB 231 Rev B MITSUBISHI SB 232 Rev A

FAA, U.S AD 2003-17-04

Windshield check FINNISH AD M 3076 LFV LVD2678 MAI SB 087/56-001 Rev B MITSUBISHI SB 224 Rev

C

01-Oct-2003

07-Oct-2010

FAA, U.S AD 2005-

14-12


FAA, U.S AD 2005-

18-20

Prop de-icer "FASTprop" 14-Oct-

2005

12-Oct-2005 N/A Due to boots p/n

FAA, U.S AD 2006-

13-15

Safety evaluation wing barrel nuts) MAI SB 103/57-004 Rev A MITSUBISHI SB

241 Rev A

11-aug-

06

11-nov-02 c/o in conjunction with vingstudie

FAA, U.S AD 2006-15-07

Safety evaluation (feathering linkage) MAI SB 090/76-003 MITSUBISHI SB 229 24-aug-06

24-aug-06 se Mitsubishi SB 229

FAA, U.S AD 2006-17-01


22-sep-06

21-sep-06 PCW see MSB 233A

FAA, U.S AD 2006-17-05

Adjust flight idle fuel flow setting MITSUBISHI SB 234 22-sep-06

11-Oct-2010

FAA, U.S AD 2007-17-09

Reduce max deflect elev nose-down trim

MITSUBISHI SB 216 MITSUBISHI SB 228 25-sep-07

11-sep-07 Previously carried out i.a.w. mentioned SB's.

FAA, U.S AD 71-14-01



FAA, U.S AD 75-03-06

Cracks and Optical Distortion LFV LVA829 Rev A 13-nov-74

15-jul-86 N/A N/A due to s/n.

FAA, U.S AD 75-16-13

Main Wing Flap JCAB AD TCD-1094A-76 05-aug-75

05-feb-02 N/A Ej tillämplig p.g.a. s/n.

FAA, U.S AD 75-16-20

Propeller Pitch Control Lever JCAB AD TCD-1188-75 LFV LVA1012 MITSUBISHI SB 168 Rev A

12-aug-75

10-nov-82

FAA, U.S AD 78-03-05

Cowling Latches JCAB AD TCD-1202-75 LFV LVA1014 Rev A MITSUBISHI SB 171 Rev B MITSUBISHI SB 180 Rev A

23-feb-78 10-apr-87

FAA, U.S AD 81-06-01

1 Engine Aft Nacelles 01-apr-81

1 08-jun-87 Previously complied with

FAA, U.S AD 81-25-04

1 Engine's Electrical wiring SB 036/71-003A, SB 043/71-005

21-jan-82 1 27-mar-09 N/A by model

FAA, U.S AD 82-08-02

Electrical Wiring Inspection 15-apr-82

02-aug-82

FAA, U.S AD 83-08-01

2 To preclude prop. attach bolt failures FINNISH AD M 1168/83 Rev 1 FINNISH AD T5114/05 HARTZELL SI 140A Rev 9

28-apr-82

2 20-May-2005 Ref. MU2B MM chap 13.4 when using bolts P/N B-3339 only



Dokumentnummer Sida

ange 177(195)

FAA, U.S AD 83-09-02

Strobe Light Assemblies 17-May-1983


FAA, U.S AD 84-12-

04


047/30-001, SB 196A


196 Rev A

28-jun-84 16-jun-87

FAA, U.S AD 84-25-

02


SB 031/27-005 R1, SB 176E


176 Rev E

18-dec-

84

16-jun-86

FAA, U.S AD 86-15-

03


Rev B

13-aug-

86

15-jul-04 Found SB 181 part 2 PCW.

FAA, U.S AD 86-20-

01


SB 020/34-005, SB 053A


MITSUBISHI SR 053A

06-Oct-

1986

15-feb-00

FAA, U.S AD 86-26-

02


iceing SB 74-0003, SR 040/74-001

GARRETT SB 74-0003 Rev , MITSUBISHI SB

226 Rev E

31-dec-

87

09-mar-09 see applicable engine for c/o

FAA, U.S AD 87-04-

03


Insp SB 051/27-007, SB 198

MAI SB 051/27-007 MITSUBISHI SB 198 07-mar-

87

16-May-1986

FAA, U.S AD 87-12-

02

Generator Shield Jumper Wires MITSUBISHI SB 201 Rev A 03-jul-87 27-mar-09 N/A by s/n

FAA, U.S AD 88-13-

01


066/22-006


MITSUBISHI SB 206

11-jul-98 03-mar-88

FAA, U.S AD 88-21-

01



LFV LVD2206 MAI SB 066/22-006 Rev A 28-jan-89 1 25-jan-12

FAA, U.S AD 88-23-

01


067/27-008, SB 189B

LFV LVD2202 MAI SB 067/27-008 Rev A 04-dec-

88

14-sep-95

FAA, U.S AD 93-07-11

ELECTRIC TRIM SYSTEM SB 079/27-010


FAA, U.S AD 94-04-16

Elevator trim tab mod. LFV LVD2537 MITSUBISHI SB 216 11-apr-94

08-apr-93

FAA, U.S AD 94-11-04

Change of Flight Idle Blade Angel SB 016/61-001


FAA, U.S AD 96-25-02

Cap. of the icing protection system FINNISH AD M 2423/97 JCAB AD TCD-4552-96 LFV LVD2749

27-dec-96

12-nov-97

FAA, U.S AD 97-04-13

Vent Check Valve Assy LFV LVD2769 16-apr-97

05-May-1997 N/A N/A due to model.

FAA, U.S AD 97-20-14 CNL

Icing related incidents/accidents 17-Oct-1997

02-dec-98

FAA, U.S AD 97-25-

02


ctrl/overspe


FAA, U.S AD 98-20-

39


MU-2 225, 089/57-002A

LFV LVD2688 MAI SB 089/57-002 Rev A ,

MITSUBISHI SB 225

19-Oct-

1998

24-Oct-1996



Dokumentnummer Sida

ange 178(195)

FINNISH, Finnish

Civil Aviation

Adm.


Justering av br,nslefl"de MHI SB 097/73-001, TCD-4890-98

JCAB AD TCD-4890-98 , MAI SB 097/73-001

12-nov-99

11-Oct-2010

FINNISH AD M 3076

Kontroll av vindrutor och fönster FAA, U.S AD 2003-17-04 , MAI SB 087/56-001 Rev B , MITSUBISHI SB 224 Rev C

21-aug-03

07-Oct-2010

GARMIN, Garmin

GARMIN SB 0004 Incorp.of Main Software Version 2.16 01-May-

2000

18-May-2000

GARMIN SSB 0844 IR Software Version 5.04 EASA SIB2008-58R1 14-nov-

08

A 19-May-2010

GARRETT,

AlliedSignal

Aerospace

GARRETT SB 74-

0003

6 Replace Ignition Unit AD 74-0003 FAA, U.S AD 86-26-02 25-mar-

94

09-mar-09 see applicable engine for c/o

HARTZELL,

Hartzell Propeller

Inc.

HARTZELL SB 61-256


08-feb-02 13-maj-02 L/H side



04-Oct-2005

14-nov-05 propellerbolts previously checked u/a


30-mar-05

9 13-mar-08 see previously revision

JCAB, Japan Civil

Aviation Bureau

JCAB AD TCD-0518-68


JCAB AD TCD-0642-70

AFM revision regarding fuel spec. LFV LVA439 MITSUBISHI SB 112 Rev C 07-feb-70 16-jul-86 N/A by s/n



Dokumentnummer Sida

ange 179(195)

JCAB AD TCD-0643-70


JCAB AD TCD-

0652-70

Insp. of NLG bolts LFV LVA456 MITSUBISHI SB 119 25-mar-

70


JCAB AD TCD-

0653-70


of

25-mar-

70


JCAB AD TCD-

0660-70


nosegearstrut


1970


JCAB AD TCD-

0730-1-72


B

25-mar-

72

14-jul-04 N/A N/A by s/n.

JCAB AD TCD-

0730-2-86

Insp. and painting of maintanks MITSUBISHI SB 143 Rev B 10-dec-

86


JCAB AD TCD-

0859-72

Mod. of electrical system LFV LVA645 MITSUBISHI SB 156 04-sep-

72

10-sep-72 N/A N/A due to model.

JCAB AD TCD-

0866-72


1972

31-dec-72 N/A N/A due to model.

JCAB AD TCD-

0947A-74


A

12-nov-

74

06-Oct-1987 N/A N/A due to s/n.

JCAB AD TCD-

0948A-1-78

Inspection of Windshields MITSUBISHI SB 163 Rev B 22-dec-

78


JCAB AD TCD-

0948A-74


B

07-Oct-

1974

15-jul-86 N/A N/A due to s/n.



06-Oct-1976

16-jun-86




12-dec-84

16-jun-86


Insp. of wingflap controlsystem FAA, U.S AD 75-16-13 LFV LVA1011 Rev A MITSUBISHI SB 167 Rev D

06-sep-76

05-feb-02 N/A Ej tillämplig p.g.a. s/n.

JCAB AD TCD-1188-75


06-May-1975

10-nov-82

JCAB AD TCD-1202-75

Engine Cowling Latches FAA, U.S AD 78-03-05 LFV LVA1014 Rev A MITSUBISHI SB 171 Rev B MITSUBISHI SB

180 Rev A

20-sep-75

15-jul-04 Found SB 171 and SB 180 PCW.

JCAB AD TCD-

1209-75


locking


JCAB AD TCD-

1235-75


emerg.cables

LFV LVA1083 MITSUBISHI SB 170 Rev A 19-sep-

75

10-apr-78 N/A N/A due to model.

JCAB AD TCD-1272-75

Supp.,MLG Forward D. Actuating Mech.-I&M

MITSUBISHI SB 172 14-nov-75




Dokumentnummer Sida

ange 180(195)


Prevent failure of MLG. dragstrut MITSUBISHI SB 173 Rev A 31-mar-76

28-Oct-2009 N/A Due to S/N

JCAB AD TCD-

1328-76


compartment


JCAB AD TCD-

1353-76


Repl.

MITSUBISHI SB 175 16-aug-

76

26-mar-09

JCAB AD TCD-

1370-76


1976

06-Oct-1987 N/A by s/n

JCAB AD TCD-

1370A-81



MITSUBISHI SB 174 PART 1 Rev C 05-nov-

81


JCAB AD TCD-

1379-1-80


heatdamage


Rev B

06-feb-02 08-jun-87

JCAB AD TCD-

1520A-77

Latch link engine nacelle door MITSUBISHI SB 180 Rev A 12-dec-

77

24-mar-09 ref. SB 180

JCAB AD TCD-

1768-1-85


JCAB AD TCD-

1817-79

Modification of bagagecompartment LFV LVA1583 MITSUBISHI SB 182 05-feb-02 08-jun-87 N/A N/A due to s/n.

JCAB AD TCD-

2048-81


circuit

LFV LVA1740 MITSUBISHI SB 187 Rev B 05-feb-02 27-May-1981 N/A N/A due to s/n.

JCAB AD TCD-

2070-81

Inspect NLG downlock mechanism LFV LVA1753 MITSUBISHI SB 188 05-feb-02 16-May-1986

JCAB AD TCD-2113-82

Insp./replace engine electrical harness

LFV LVA1788 MITSUBISHI SB 191 06-feb-02 16-May-1986


Flap system torquetubes supersed TCD-2252-1-87

01-feb-89 24-mar-09 PCW

JCAB AD TCD-2252-83

Flapcontrolsystem torquetubes LFV LVA1873 MITSUBISHI SB 189 Rev C 04-feb-83 14-sep-95

JCAB AD TCD-2263-83

NLG. bracket attaching to drag strut 13-aug-83





JCAB AD TCD-2342-84



JCAB AD TCD-

2450A-87


JCAB AD TCD-

2451-1-87


1987


JCAB AD TCD- Add. seal/Tq. insp of flap flex. shaft LFV LVD2037 MITSUBISHI SB 198 30-sep- 16-May-1986



Dokumentnummer Sida

ange 181(195)

2451-85 Superseeded by TCD-2451-1-87 85


Generator System LFV LVD2191 MITSUBISHI SB 201 Rev A 01-jul-88 24-mar-09 N/A by s/n



01-feb-97 22-nov-01


Bendix M4C Autopilot System MITSUBISHI SB 206 05-nov-97

28-Oct-2009 N/A Due to model

JCAB AD TCD-3378-90

Insp./mod. of rudder trimtab leadingedge

LFV LVD2338 MITSUBISHI SB 211 28-mar-91



Anti ice/De-ice system FINNISH AD M 2364/96 LFV LVD2347 Rev 1 MITSUBISHI SB 212 Rev A

25-May-1996

07-Oct-2010

JCAB AD TCD-3464-91


JCAB AD TCD-

3740A-98


MSB 216, 228 LVD 2898



17-aug-

98

18-nov-98

JCAB AD TCD-3901-93


10-sep-93

01-feb-94



28-nov-94

01-feb-94

JCAB AD TCD-3942-94

Change lockingpin ldg LFV LVD2538 MITSUBISHI SB 219 Rev A 01-feb-94 01-feb-94

JCAB AD TCD-4310-96

Fwd. Fitting Bolt FINNISH AD M 2351/96 LFV LVD2688 MITSUBISHI SB 225

01-apr-96

24-Oct-1996

JCAB AD TCD-

4311-95



01-nov-

95

07-Oct-2010

JCAB AD TCD-

4379-96

Feathering Valve/Linkage insp. FINNISH AD M 2352/96 LFV LVD2689 01-apr-

96

30-jul-96

JCAB AD TCD-

4552-96

Icing Limitation FAA, U.S AD 96-25-02 LFV LVD2749 27-dec-

96

12-nov-97

JCAB AD TCD-

4625-97


093/22-009

14-jul-97 09-feb-01

JCAB AD TCD-

4625A-2001


NYGE TDM01-45

16-mar-

01

13-mar-09 PCW

JCAB AD TCD-4626-97

De-ice system Modification FINNISH AD M 2461/97 LFV LVD2800 MITSUBISHI SB 232 Rev A

01-May-1997

14-jul-04 PCW

JCAB AD TCD-4684-97

Mod. of Bearing box Ldg. Act. FINNISH AD M 2495/97 LFV LVD2819 MITSUBISHI SB 230

01-jun-97 25-mar-99



Dokumentnummer Sida

ange 182(195)

JCAB AD TCD-4753-98

Ändring av flyghandbok LVD 2922,FAA AD 97-20-14, MHI SN 117A

FINNISH AD M 2518/98 LFV LVD2922 MITSUBISHI SN 117 Rev D


JCAB AD TCD-

4753A-2004

Icing-related incidents VIDEO FAA, U.S AD 2003-22-07 Rev 1 24-feb-04 11-dec-03

JCAB AD TCD-

4838-98


train


MITSUBISHI SB 235

04-aug-

98


JCAB AD TCD-

4889-2-2007


JCAB AD TCD-

4889-98





05-nov-

98

14-jul-04 PCW

JCAB AD TCD-

4890-98


SB 234

FINNISH AD M 2609/98 LFV LVD2925 04-nov-

98

11-Oct-2010

JCAB AD TCD-

5030-99


1999


JCAB AD TCD-

5432-2000

AFM revision LFV LVD3112 27-nov-

00

12-feb-02

JCAB AD TCD-

5547-2001

To prevent loss of airplane control LFV LVD3123 16-mar-

01

12-feb-02

JCAB AD TCD-

5747-2001

Inspection of Tip Tank Brackets LFV LVD3166 MITSUBISHI SB 236 12-sep-

01

10-Oct-2001

JCAB AD TCD-

5864-2001

Flap Drive Train Inspection LFV LVD3212 MITSUBISHI SB 237 27-dec-

01

17-jan-02


Pneumatic Line insp. LFV LVD3322 MITSUBISHI SB 239 17-mar-03

09-sep-03


Inspection of Wing Attachment Hardware

MITSUBISHI SB 241 Rev A 27-dec-06

17-jan-07 c/o in conjunction with wingstudie

LFV,

Luftfartsverket



05-feb-02 A 05-feb-02 N/A Ej tillämplig p.g.a. s/n.



05-feb-02 05-feb-02 N/A Ej tillämplig p.g.a. s/n.

LFV LVA 1013 Kontr. och mod. av låsning på nosställ JCAB AD TCD-1209-75 MITSUBISHI SB 169 Rev B

05-feb-02 08-jun-87


låsanordning



05-feb-02 A 10-apr-87



Dokumentnummer Sida

ange 183(195)


05-feb-02 10-apr-78 N/A N/A due to s/n

LFV LVA 1196 Isolering av strobe light från bränsle JCAB AD TCD-1370-76 MITSUBISHI SB 174

PART 1 Rev C

06-feb-02 06-Oct-1987 N/A by s/n


bak.motorpl.


177 Rev B

06-feb-02 A 08-jun-87


trimrod




06-feb-02 08-jun-87

LFV LVA 1583 Modifiering av bagageutrymme JCAB AD TCD-1817-79 MITSUBISHI SB 182 05-feb-02 08-jun-87 N/A N/A due to s/n.




LFV LVA 1753 Kontroll av låsmekanism i nosställ JCAB AD TCD-2070-81 MITSUBISHI SB 188 05-feb-02 16-May-1986


JCAB AD TCD-2113-82 MITSUBISHI SB 191 06-feb-02 02-aug-82

LFV LVA 1873 Insp./utbyte av infäst.till torsionsrör JCAB AD TCD-2252-83 MITSUBISHI SB 189 Rev C

06-feb-02 14-sep-95


varmlufts


Rev A

06-feb-02 16-jun-87

LFV LVA 438 Justering av bränslemängdsmätare JCAB AD TCD-0643-70 MITSUBISHI SB 114 05-feb-02 16-jul-86 N/A N/A by s/n

LFV LVA 439 Rev. av flyghandbok betr. bränslespec.

JCAB AD TCD-0642-70 MITSUBISHI SB 112 Rev C

05-feb-02 16-jul-86 N/A by model





LFV LVA 664 Nosställsväxellåda och struktur JCAB AD TCD-0866-72 05-feb-02 31-aug-09 N/A by s/n & model


162 Rev A

05-feb-02 A 06-Oct-1987 N/A N/A due to s/n.



163 Rev B

05-feb-02 A 15-jul-86 N/A N/A due to s/n.

LFV LVA 886 A Kontroll/byte av höjdtrimroderarmar JCAB AD TCD-1001A-76 05-feb-02 A 16-jun-86



Dokumentnummer Sida

ange 184(195)

LFV LVD 1238 Kontr./byte infästn.det. höjdtrimroder

15-apr-77

27-mar-09 N/A se LVA 886A & FAA AD 84-25-02

LFV LVD 1971 Elevator Trim Tab MU2 SB 176E JCAB AD TCD-1001B-2-84 18-jan-85 16-jun-86

LFV LVD 2015 B Pitot Tube Wiring MAI SR 020/34-005 Rev A, MHI SR 53

FAA, U.S AD 86-20-01 JCAB AD TCD-2450A-87 MAI SR 020/34-005 MITSUBISHI

SR 053A

24-May-1985

B 29-jan-87

LFV LVD 2037 Flap Flexible Shaft MU2 SB 198 JCAB AD TCD-2451-85 MITSUBISHI SB 198 30-sep-85

16-May-1986

LFV LVD 2069 Altimeter 25-mar-86

18-aug-87 N/A N/A by p/n & s/n


26-jan-87 06-Oct-1987



19-aug-88

03-mar-88


19-aug-88


LFV LVD 2202 Kontr. av koppl. för tors.rör till klaff FAA, U.S AD 88-23-01 JCAB AD TCD-2252-1-87 MAI SB 067/27-008 Rev A


08-dec-88

14-sep-95


12-feb-02


211

JCAB AD TCD-3378-90 MITSUBISHI SB 211 28-mar-91



212A


212 Rev A

29-May-

1996

1 07-Oct-2010


CHPT 9

23-May-

1991



216


216

03-dec-

92

08-apr-93



LFV LVD 2512 TIP TANK INST. (NXT 100H) JCAB AD TCD-3901-93 MITSUBISHI SB 221 02-dec-93

16-nov-94


216

FAA, U.S AD 94-04-16 MITSUBISHI SB 216 07-apr-94

08-apr-93


219


Rev A

07-apr-

94

01-feb-94



Dokumentnummer Sida

ange 185(195)




09-feb-95 01-feb-94

LFV LVD 2678 Kontr. av vindrutor och fönster MHI SB 224 Rev A

FAA, U.S AD 2003-17-04 JCAB AD TCD-4311-95 MITSUBISHI SB 224 Rev C

12-mar-96

07-Oct-2010

LFV LVD 2688 Kontr/byte av infästn.bult för tiptank MU-2 SB 225

FAA, U.S AD 98-20-39 JCAB AD TCD-4310-96 MITSUBISHI SB 225

09-May-1996

24-Oct-1996

LFV LVD 2689 Kontroll av linkage för prop.flöjning MU-2 SB 229

JCAB AD TCD-4379-96 MITSUBISHI SB 229 09-May-1996

30-jul-96

LFV LVD 2732 Inspection/ Replacement of Prop Hub. FAA AD 96-18-14, Hz SB 136H

FAA, U.S AD 96-18-14 HARTZELL SB 61-261 Rev 1

27-sep-96

01-sep-99 Prop. utbytt mot BVA

LFV LVD 2749 Revision av flyghandbok AFM TCD-4552-96


21-jan-97 12-nov-97

LFV LVD 2757 Sprickkontr. av landst,l.Side Brace

Stud AD 97-01-01

FAA, U.S AD 97-01-01 Rev 1 14-feb-97 12-nov-97


TCD-2679A-97


226 Rev E

14-feb-97 29-mar-99

LFV LVD 2769 Demont.av backventil i

bränslesystemets MU-2 SB 130A


Rev A

18-mar-

97

05-May-1997 N/A N/A due to s/n.

LFV LVD 2799 **RECOVERED RECORD** 09-feb-01




Rev A

28-aug-

97

12-May-1998

LFV LVD 2819 Mod.av lagerboxar för

landställssystem Mitsubishi SB 230

JCAB AD TCD-4684-97 MITSUBISHI SB 230 18-nov-

97

12-jun-98


nödutgång

23-mar-

98

07-Oct-2010

LFV LVD 2897 Kontroll av landst,llets drivsystem

TCD-4838-98, SB 235

JCAB AD TCD-4838-98 MITSUBISHI SB 235 02-aug-

98




27-aug-98

18-nov-98



12-nov-98

02-dec-98 FAA AD utförd.



01-dec-98

23-feb-00

LFV LVD 2925 Kontr/just av mot bränsleflöde Flight Id MHI SB 234

JCAB AD TCD-4890-98 MITSUBISHI SB 234 01-dec-98

11-Oct-2010

LFV LVD 2988 Sprickkontroll av kroppsspant JCAB AD TCD-5030-99 MITSUBISHI SB 209 Rev B




Dokumentnummer Sida

ange 186(195)


LFV LVD 3122 Modifiering av autopilotsystemet JCAB AD TCD-4625A-2001 MAI SB 093/22-009 MITSUBISHI SB 231 Rev B NYGE

TDM01-45

02-apr-01

09-feb-01

LFV LVD 3123 Ändring av flyghandbok JCAB AD TCD-5547-2001 02-apr-

01

12-feb-02



20-sep-01

10-Oct-2001


09-jan-02 17-jan-02


21-mar-03

09-sep-03

MAI, Mitsubishi

Aircraft

International

MAI SB 047/30-

001

A Torque of Bleed Air Tube Coupling

Nuts AD 84-12-04,SB 196A


Rev A

19-jul-84 A 16-jun-87

MAI SB 051/27-

007


Torque AD 87-04-03, SB 198

FAA, U.S AD 87-04-03 01-feb-85 16-May-1986

MAI SB 066/22-

006

A Bendix Autopilot Disengagement AD

88-13-01, AD 88-21-01 R1

FAA, U.S AD 88-13-01 FAA, U.S AD 88-21-

01 Rev 1 LFV LVD2190 MAI SB 069/24-006

06-jun-89 03-mar-89 Data transferred/updated on WO C05770

MAI SB 067/27-

008



FAA, U.S AD 88-23-01 LFV LVD2202 29-mar-

95

A 14-sep-95

MAI SB 069/24-006

Split Radio Bus Inspection and Rework

MAI SB 066/22-006 Rev A 17-nov-88

03-mar-88 N/A N/A due to Aircraft s/n

MAI SB 086/74-002


05-Oct-2000


MAI SB 089/57-002

A Insp/Repl. of Bolts for Wing Tip Tank FAA, U.S AD 98-20-39 05-nov-96

A 24-Oct-1996 N/A N/A due to s/n.

MAI SB 093/22-009

Trim-In-Motion Alert System FAA, U.S AD 2000-09-15 Rev 1 FINNISH AD M 2460/97 UPPHÄVD JCAB AD TCD-4625-

97 LFV LVD3122 MITSUBISHI SB 231 Rev B

08-jul-97 09-feb-01

MAI SN 110/00-

017A


MAI SN 111/77-004

Torque Indicating System Shift Potential

20-nov-08

11-mar-09 SB 233 considered

MAI SR 020/34- Anti Ice Capability AD 86-20-01, SR FAA, U.S AD 86-20-01 LFV LVD2015 Rev B 06-Oct- 15-feb-00 N/A N/A due to s/n.



Dokumentnummer Sida

ange 187(195)

005 053A MITSUBISHI SR 053A 1986

MITSUBISHI,

Mitsubishi Heavy

Industries Ltd

MITSUBISHI MSB

24-002

A **RECOVERED RECORD** A 18-jul-86 N/A

MITSUBISHI MSB

24-004


MITSUBISHI MSB

27-001


MITSUBISHI MSB

27-003


















MITSUBISHI MSB

34-004


MITSUBISHI MSB

34-007


MITSUBISHI MSB

54-001


MITSUBISHI MSB

54-002


MITSUBISHI MSB B **RECOVERED RECORD** B 18-jul-86 N/A



Dokumentnummer Sida

ange 188(195)

71-003



MITSUBISHI MSR 066

B **RECOVERED RECORD** B 06-Oct-1987

MITSUBISHI SB 066

Bendix M4D 18-dec-87

06-mar-89 Info transfererad till SB 066/222-006 ref C05770

MITSUBISHI SB 076/22-008

M-4() Autop.Engage Switch Guard Install.

11-apr-91

16-nov-94

MITSUBISHI SB 112

C Anti-Ice Additive in Fuel -Usage of JCAB AD TCD-0642-70 LFV LVA439 09-Oct-1971

C 16-jul-86

MITSUBISHI SB 114


MITSUBISHI SB

119

The Bolt and Bolt Hole Diam. of Nose

L.G

JCAB AD TCD-0652-70 LFV LVA456 10-mar-

70


MITSUBISHI SB

123

Bearing,Oleo Strut,Nose L.G. -Repl. of JCAB AD TCD-0660-70 LFV LVA457 01-apr-

70


MITSUBISHI SB

124

Scissors Switch,Nose L.G. -Install. of 31-aug-

70

17-jul-86 N/A

MITSUBISHI SB

128


MITSUBISHI SB

143

B Top Coating, Wing Integral Main F.T.-

SIo


0730-2-86


MITSUBISHI SB 162

A Flex. Shafts, Flap Control Sys.-Insp. of (AD750201)


A 06-Oct-1987 N/A

MITSUBISHI SB 163

B Insp. of Outer Pane, Front Winds. & Inst

FAA, U.S AD 74-11-01 JCAB AD TCD-0948A-1-78 JCAB AD TCD-0948A-74 LFV

LVA829 Rev A

16-nov-78

15-jul-86 N/A

MITSUBISHI SB

165

A Lubr. Interval,Wheel Bearing,Main &

Nose

24-jul-80 03-mar-77 N/A

MITSUBISHI SB

167

D Flap M.Jack Screw-Insp. of and/or

Main G



24-jul-80 D 05-feb-02 N/A Ej tillämplig p.g.a. s/n.

MITSUBISHI SB

168


(AD761620)


75 LFV LVA1012

24-jul-80 A 10-nov-82

MITSUBISHI SB 169

B Shimmy Damper-Insp. and Modification of


MITSUBISHI SB 170


JCAB AD TCD-1235-75 LFV LVA1083 24-mar-77

A 17-jul-86 N/A N/A due to s/n



Dokumentnummer Sida

ange 189(195)

MITSUBISHI SB 171



17-nov-77

B 10-apr-78

MITSUBISHI SB

173

A Drag Strut, Main L.G.-Modification of JCAB AD TCD-1284-1-76 24-jul-80 A 06-feb-06 N/A N/A due to s/n

MITSUBISHI SB

174 PART 1


Rew.of (AD830902)


1370A-81 LFV LVA1196

02-Oct-

1981

C 06-Oct-1987 N/A by s/n

MITSUBISHI SB

174 PART 2

C Tip Tank Conduit Tube Rework 02-Oct-

1981

C 06-Oct-1987 N/A N/A by A/C S/N

MITSUBISHI SB

175


Repl.

JCAB AD TCD-1353-76 26-jun-76 24-aug-76

MITSUBISHI SB

176

E Elevator Trim Tab Bracket-Repl. of

LVD1971, AD 84-25-02, SB 031/27-005R1



26-sep-

84

E 16-jun-86

MITSUBISHI SB 177

B Mod. of Engine Nacelle Tail Area (AD810601)

JCAB AD TCD-1379-1-80 LFV LVA1197 Rev A

11-sep-80

B 08-jun-87

MITSUBISHI SB 179


27-May-1977

08-jun-78

MITSUBISHI SB

180

A Link, Engine Nacelle Upper D.-Repl. of

(AD780305)



17-nov-

77

A 10-apr-78




08-apr-85

B 18-aug-87

MITSUBISHI SB 182

Add. of Ceiling Cover, Rear Bagg. Comp.

JCAB AD TCD-1817-79 LFV LVA1583 16-nov-79

08-jun-87 N/A N/A due to s/n.

MITSUBISHI SB 184

Turnbuckle, Control Cables -Repl. of 04-apr-80

14-nov-86

MITSUBISHI SB 188

Down Lock Mech., Nose L.G.-Insp. of JCAB AD TCD-2070-81 LFV LVA1753 13-jul-81 16-May-1986

MITSUBISHI SB 189

C Flap Control Torque Tube AD 88-23-01, SB 067/27-008

FINNISH AD M 2722/00 JCAB AD TCD-2252-1-87 JCAB AD TCD-2252-83 LFV LVA1873 LFV LVD2202

28-jun-94 C 14-sep-95

MITSUBISHI SB 191

Engine El. Wire-Insp. and Replacement of (AD820802)

JCAB AD TCD-2113-82 LFV LVA1788 21-dec-81

02-aug-82

MITSUBISHI SB 193

B Landing Gear Warning Horn Syst.Modif.


MITSUBISHI SB 194

Master Cauting Light Visibility-Impr. of

23-aug-82

16-May-1986

MITSUBISHI SB 196

A Ret. of coupling nut on the bleed air tu AD 84-12-04, SB 047/30-001

FAA, U.S AD 84-12-04 JCAB AD TCD-2342-1-84 JCAB AD TCD-2342-84 LFV LVA1942

12-apr-84

A 16-jun-87



Dokumentnummer Sida

ange 190(195)

MAI SB 047/30-001 Rev A

MITSUBISHI SB 198

Add. Seal & Torque Insp. of Flap Flex.Sh LVD2037, AD 87-04-03, SB

051/27-007


13-feb-85 16-May-1986

MITSUBISHI SB

199


Protec


MITSUBISHI SB 200

B Insp of Nose Ldg Gear Drag Strut Link 24-jun-94 A 19-Mar-12

MITSUBISHI SB 201

A Generator Circuit Wires Insp. and Mod.


02-mar-88

A 24-mar-09 N/A by s/n

MITSUBISHI SB 204

Speed Placard Change 03-mar-87

14-apr-89

MITSUBISHI SB 206

Bendix Autop.Disengagement Method Stand

FAA, U.S AD 88-13-01 , JCAB AD TCD-2856-1-97, LFV LVD2190

13-Oct-1987

28-Oct-2009 N/A Due to model

MITSUBISHI SB 207

Rudder T.T. & Elevator T.T. Insp. & Rep.

20-May-1988

07-Oct-2010

MITSUBISHI SB 209

B Fuselage inspection JCAB AD TCD-5030-99 LFV LVD2988 19-apr-99

B 24-mar-09 N/A by model

MITSUBISHI SB 210

A Engine Ignition Unit Replacement 12-nov-96

06-mar-98

MITSUBISHI SB 211

Rudder Trim Tab Modification (LVD 2338)

JCAB AD TCD-3378-90 LFV LVD2338 20-nov-90


MITSUBISHI SB 212

A Insp of Anti-ice/Deice Systems (LVD 2347),


25-apr-96

A 07-Oct-2010

MITSUBISHI SB

214

Engine Control Rod Inspection 06-dec-

91

08-May-1992

MITSUBISHI SB

215

Removel of Prop. Governor Speed

Signal

23-Oct-

1991

08-May-1992

MITSUBISHI SB

216

Elevator Trim Tab Installation (LVD

2450

FAA, U.S AD 2007-17-09 FAA, U.S AD 94-

04-16 JCAB AD TCD-3740A-98 LFV LVD2450 LFV LVD2537 LFV LVD2898

11-sep-

92

08-apr-93

MITSUBISHI SB 218

A Propeller Feathering Linkage Inspection

17-jan-94 A 01-feb-94

MITSUBISHI SB 219

A Emergency Gear Down G.box Lower Pin Repl


24-Oct-1994

A 01-feb-94

MITSUBISHI SB

221

Tip Tank Conduit Tube Insp. and Rep. JCAB AD TCD-3901-93 LFV LVD2512 10-aug-

93

01-feb-94

MITSUBISHI SB

223

Pitot/Static System Improvement SR

064

MITSUBISHI SR 053A MITSUBISHI SR 064 28-jun-94 15-feb-00



Dokumentnummer Sida

ange 191(195)

MITSUBISHI SB 224

C Acrylic Windsheild/Window glass Insp. UHB

FAA, U.S AD 2003-17-04 FINNISH AD M 3076 JCAB AD TCD-4311-95 LFV LVD2678

30-apr-98

C 07-Oct-2010

MITSUBISHI SB

225

Forward fitting bult of wingtip tank

LVD 2688



29-sep-

95

24-Oct-1996

MITSUBISHI SB 226



FINNISH AD M 2786/00 JCAB AD TCD-2679A-97 LFV LVD2761 MAI SB 086/74-002 Rev A

18-sep-01

E 22-nov-01 PCW no further action (rev.E) required due to s/n.

MITSUBISHI SB 227

Rudder Torque Tube Modification 20-dec-96

08-sep-97

MITSUBISHI SB 228



LVD2898

13-jul-98 18-nov-98

MITSUBISHI SB

229

Feathering Valve/Linkage Insp. FAA, U.S AD 2006-15-07 JCAB AD TCD-

4379-96 LFV LVD2689

20-feb-96 30-jul-96

MITSUBISHI SB

230

Mod.of Bearing Box Ldg. Gear Act.

LVD 2819

JCAB AD TCD-4684-97 LFV LVD2819 05-mar-

97

12-jun-98

MITSUBISHI SB 231

B Inst.of Trim-In-Motion Alert System FAA, U.S AD 2000-09-15 Rev 1 FINNISH AD M 2460/97 UPPHÄVD FINNISH AD M

2786/00 JCAB AD TCD-4625A-2001 LFV LVD3122 MAI SB 093/22-009 NYGE

TDM01-45

11-dec-02

B 03-mar-03 SL 079 performed earlier.

MITSUBISHI SB

232

A De-Ice System Modification LVD

2800, TCD-4626-97


M 2786/00 JCAB AD TCD-4626-97 LFV

LVD2800 MAI SB 096/30-004


MITSUBISHI SB

233

B Insp.of Engine Torque Indication



2608/98 JCAB AD TCD-4889-2-2007 JCAB AD TCD-4889-98 LFV LVD2924

08-mar-

07

B 18-apr-07 Checked, previously carried out

MITSUBISHI SB 234



07-Oct-1998

11-Oct-2010

MITSUBISHI SB 235

Inspection of landing gear power train

JCAB AD TCD-4838-98 LFV LVD2897 04-aug-98


MITSUBISHI SB

236

Inspection of Tip Tank Brackets JCAB AD TCD-5747-2001 LFV LVD3166 28-aug-

01

10-Oct-2001

MITSUBISHI SB

237

Inspection of Flap Drive Train JCAB AD TCD-5864-2001 LFV LVD3212 13-dec-

01

17-jan-02

MITSUBISHI SB

238

Main Landing Gear Door Safety Pin 05-dec-

02

09-jan-03 Perf. at each 600 h. insp.



Dokumentnummer Sida

ange 192(195)

MITSUBISHI SB 239

Pneumatic Line Insp. and Modification

JCAB AD TCD-6127-2003 26-dec-02

09-sep-03

MITSUBISHI SB

240

Inst.of Trottle Quadrant Placard 26-feb-03 02-jun-03

MITSUBISHI SB

241


Hardware


7030-2006

21-nov-

06

A 17-jan-07 c/o in conjunction with wingstudie

MITSUBISHI SL 060 System 17-feb-89 24-jul-91

MITSUBISHI SL 078 Automatic Autopilot Disconnect System

28-jan-02 07-Oct-2010

MITSUBISHI SL 079 Diode inst.in Flap Position Ind.Curcuit 28-jan-02 09-feb-01 Carried out by Mitsubishi (manufacturing-made)

MITSUBISHI SL 080 Hartzell Propeller Mounting Bolt Insp. HARTZELL SB 61-256 05-apr-02

26-aug-02 Compliance in according to HC-SB-61-256.

MITSUBISHI SL 084 Pneumatic De-Ice Monitoring System 14-jun-04 07-Oct-2010

MITSUBISHI SL 085 Hartzell prop. mount. bolt insp. HARTZELL SB 61-279 ALERT Rev 4 17-May-2005

14-sep-05

MITSUBISHI SN 053


05-nov-86

B 26-Oct-1987

MITSUBISHI SN 117

D Icing Awareness Training Video FAA, U.S AD 2003-22-07 Rev 1 JCAB AD TCD-4753-98 LFV LVD2922

14-jun-04 D 11-dec-03

MITSUBISHI SN 146

Water Ingress into Vertical Stabilizer 19-dec-03

30-apr-04

MITSUBISHI SN 148

Reminders for safe operation 18-nov-05

22-mar-06 Genomförs enl. AMP MU-2 & DHB

MITSUBISHI SN

156A


MITSUBISHI SN

157


Potential

20-nov-

08

11-mar-09 SB 233 considered

MITSUBISHI SN

161

Repl Air Filter for Vacuum System MITSUBISHI STCSA01913SE 09-dec-

09

11-mar-10 Ref STC SA01913SE

MITSUBISHI SR

053A



23-Oct-

1984

12-May-1998

MITSUBISHI SR 064

Pitot & Static System MITSUBISHI SB 223 30-apr-85

15-feb-00

MITSUBISHI SR 065

Warning Horn 20-jan-86 13-Oct-1987

MITSUBISHI SR

067

Emergency Exit Placard 17-sep-

85

18-aug-87



Dokumentnummer Sida

ange 193(195)

MITSUBISHI SR 072

Air Filter Replacement for Vacuum Syst.

25-apr-00

14-dec-01

MITSUBISHI SR

075

Inst. tip tank placard 29-Oct-

2004

29-apr-05

MITSUBISHI STC

SA01913SE

Inst of a Vacuum System Air Filter MITSUBISHI SN 161 10-dec-

09

11-mar-10 See MU-2B AMP Chpt 3 100h/1y inspection

NARCO, Narco

NARCO SB ELT10-16

ELT ASSY 18-apr-88

19-jun-91 N/A

NYGE, Saab

Aerotech Aircraft

Services

NYGE TDM 00-18 Förstärkning av tidigare utförd skarv-

reparation kroppsida

19-Oct-

2000

27-Oct-2000 Reparation utförd

NYGE TDM 00-21 Domkraftskada 12-dec-

00

09-feb-01

NYGE TDM 00-23 Wiring Left Wing ADRIAN 22-dec-00

25-jan-00


18-dec-02

NYGE TDM 02-32 Installation EMI film 10-dec-02

10-jan-04


04-mar-03

8 16-Oct-2008

NYGE TDM 03-28 F Nav Demo Pod 19-dec-03

F 21-jan-10 Doubler/Grommet/Connector remain to install. Ref. defectlog No:869 Original compliance by Rev D. Not

affected by rev F.

NYGE TDM 05-16 Viktor Counter Weight Pod 18-nov-05

18-nov-05

NYGE TDM 06-41 A Darts (to carry on MU-2B-20/26) 20-nov-06

A 07-feb-08

NYGE TDM 06-42 A Barlast DARTS MU-2B 04-dec-07

A 07-feb-08


NYGE TDM 08-03 A Enhanced Surveillance MU-2B 28-feb-08 A 07-sep-09



Dokumentnummer Sida

ange 194(195)

NYGE TDM 08-28 B ELT 406 MU-2B 29-sep-08

B 16-Oct-2008 Original compliance with TDM rev A. Rev B does not affect previous complaiance.

NYGE TDM 09-32 A GPS Splitter 12-nov-

09

A 21-jan-10

NYGE TDM 10-02 A Target surveillance camera 03-jun-10 A 15-jun-10

NYGE TDM 10-03 A Pressure Bulkhead Feed Through 04-May-2010

A 15-jun-10

NYGE TDM 10-25 A MU-2B Terminating Resistor 08-apr-10

A 18-May-2010 C/W

NYGE TDM 11-35 A Terminating resistor 30-Jan-12

NYGE TDM 12-21 A Avinstalltion IK 14-Aug-12

NYGE TDM 95-04 4 Vingstudie 20-sep-98

31-mar-08

NYGE TDM 99-12 Avionic Modification SE-IUA 14-dec-99

07-feb-00

NYGE TVO 1/09 Inspektion av Stringers & struktur vinge

25-feb-09 02-mar-09 Inspected u/a

NYGE TVO 1/93 Low Volt Warning Light (BCL) 22-jan-93 08-apr-93

NYGE TVO 1/96 Slitage Flap Guide Rail 12-apr-

96

09-feb-00


korrosionskontroll

12-feb-97 10-mar-97

NYGE TVO 2/00 Märkning av infästning domkraft Mu2 01-dec-

00

09-feb-01


06-feb-07 A 02-mar-07

NYGE TVO 2/10 1 Visual inspection of center wing 19-apr-10

1 09-jul-10

NYGE TVO 2/91 A/C Elecrical System 10-jan-91 08-May-1992

NYGE TVO 3/06 Inspect lower rudder hinge bracket 07-dec-06

07-Oct-2010

NYGE TVO 3/96 3 Wing Spar Flange Inspection. 24-feb-05 3 01-jun-09

NYGE TVO 4/11 A Static inverter control 15-Dec-12

NYGE TVO 4/86 2 Wing Pod Inspection 06-apr-92

2 07-Oct-2010



Dokumentnummer Sida

ange 195(195)

NYGE TVO 4/91 Special Inspection (next E6.) 19-feb-91 08-May-1992

NYGE TVO 4/92 Engine Install. Kontr. rörledningar 29-apr-92

09-nov-92

NYGE TVO 4/94 3 Fwd. Wing Tiptank Attachment 28-sep-94

3 07-Oct-2010


25-Oct-1996

19-aug-97 Utförd tidigare (ref. Ove N. lista)

NYGE TVO 6/88 Allm. instruktion för metallpropeller 13-jun-88 09-jul-10


09-nov-92

NYGE TVO 7/05 RMI-nål park. ej / ILS frekvens är vald 11-nov-05

01-nov-05

NYGE TVO 7/93 Starter Drive Splines 01-nov-93

16-nov-94

NYGE TVO 8/04 Kontr. av Spant vid bakre feninfästning

08-dec-04

30-nov-09


08-apr-93

Enclosure 2 - Description of GFE Aircrafts

Documents

Transcript of Enclosure 2 - Description of GFE Aircrafts