AIRCRAFT MANUAL SUPPLEMENT - ASL Airlines Belgium
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AIRCRAFT MANUAL SUPPLEMENT To support Instructions for Continued Airworthiness in accordance with Regulations EASA CS-25.1529/FAR 14 CFR-25.1529, Appendix H. 365 Aerospace Modification MDL-0321 Document No: AMS-0321-001 Intro Produced on behalf of 365 Aerospace Limited, UK. 365 Aerospace own the copyright of the format of this Manual Supplement, which is supplied in confidence. The contents must not be reproduced without permission In writing from the owner.
Transcript of AIRCRAFT MANUAL SUPPLEMENT - ASL Airlines Belgium
AIRCRAFT MANUAL SUPPLEMENT To support Instructions for Continued Airworthiness in accordance with Regulations EASA CS-25.1529/FAR 14 CFR-25.1529, Appendix H.
365 Aerospace Modification MDL-0321 Document No: AMS-0321-001
Intro Produced on behalf of 365 Aerospace Limited, UK. 365 Aerospace own the copyright of the format of this Manual Supplement, which is supplied in confidence. The contents must not be reproduced without permission In writing from the owner.
HL-00 Page 1 SEP 01/18
Produced on behalf of 365 Aerospace Limited, UK. 365 Aerospace own the copyright of the format of this Manual Supplement, which is supplied in confidence. The contents must not be reproduced without permission In writing from the owner.
HIGHLIGHTS Issue 2 Introduction – General – Page 1 MSNs 25097 & 28886 added Issue 3 Introduction – General – Page 1 MSNs 28892, 28893, & 29270 added
RR-00 Page 1 SEP 01/18
Produced on behalf of 365 Aerospace Limited, UK. 365 Aerospace own the copyright of the format of this Manual Supplement, which is supplied in confidence. The contents must not be reproduced without permission In writing from the owner.
RECORD OF REVISION
Issue Date Issue Date Initial (1) AUG 01/17
2 JUN 01/18 3 SEP 01/18
The Aircraft Manual Supplement (AMS) is to be used in conjunction with the related aircraft’s manuals. The information contained within this manual relates to various alterations/changes/modifications that have been carried out on the associated aircraft. A list of effective alterations/changes/modifications can be found in the Introduction pages to this manual. These alterations/changes/modifications are in addition to the initial design of the aircraft and are therefore detailed within this manual using appropriate and related convention. This manual complies with EASA Regulations CS-25.1529 and CS-25 Appendix H, which in turn mirror the FAA regulation 14 CFR 25.1529.
INTRO-00 Page 1 SEP 01/18
Produced on behalf of 365 Aerospace Limited, UK. 365 Aerospace own the copyright of the format of this Manual Supplement, which is supplied in confidence. The contents must not be reproduced without permission In writing from the owner.
INTRODUCTION
1. General A. This publication was prepared on behalf of 365 Aerospace Ltd and is in accordance with Air Transport Association of America
Specification No. 100, Specification for Manufacturers Technical Data. The data contained within is related to certain changes/modifications/alterations that are in addition to the associated airplane’s type design.
NOTE: THIS MANUAL IS PREPARED SPECIFICALLY TO COVER THE AIRPLANE LISTED IN THE "INTRODUCTION"
SECTION, FOR THE OWNER/OPERATOR NAMED ON THE TITLE PAGE.
THIS MANUAL IS NOT SUITABLE FOR USE, INCLUDING WITHOUT LIMITATION, GENERAL INSTRUCTIONS OR TRAINING, FOR ANY AIRPLANES NOT LISTED HEREIN.
B. The convention for the use of this publication is in the same convention (ATA 100) as the associated manufacturers AMM,
WDM, and IPC. Therefore, this publication is a SUPPLEMENT to the associated AMM, WDM, and IPC, and instructions on how to use this manual are equivalent to the instructions on how to use the manufacturers AMM, WDM and IPC.
C. This Manual Supplement has been raised to give historic design information pertaining to the following related aircraft
manuals:
WDM – Wiring Diagram Manual IPC – Illustrated Parts Catalogue AMM – Aircraft Maintenance Manual
D. For information on the approval of the technical content of this document, please refer to the Change/Mod/Alteration listing E. Aircraft Effectivity Information:
MODEL/ TYPE
CUST EFFECT CODE
CUST EFFECT CODE
(IPC ONLY)
VARIABLE ENGR
NUMBER
ENGINE SET
NUMBER LINE
NUMBER
MFG SERIAL
NUMBER REGISTRY NUMBER
CUST ASSIGNED AIRPLANE
IDENT
B737-400 25097 25110 25111 28886 28892 28893 29270
INTRO-00 Page 2 SEP 01/18
Produced on behalf of 365 Aerospace Limited, UK. 365 Aerospace own the copyright of the format of this Manual Supplement, which is supplied in confidence. The contents must not be reproduced without permission In writing from the owner.
INTRODUCTION
2. Change/Modification/Alteration Listing
A. DOA Mod/STC information – Table 2.1
Mod/STC Ref: Title:
MDL-0321 Change to Install a Driessen ‘Combo’ Combination Water Boiler Hot Cup
B. Owner/Operator/Supplier Mod/STC Information – Table 2.2
Mod/STC Ref: Title: Supplier:
3. Approval
A. With reference to any Mod/STC indicated in Table 2.1 above, the technical content of the supplement information associated
with any listed Mod/STC above is approved under the authority of DOA No. EASA.21J.575. B. With reference to any Mod/STC indicated in Table 2.2 above, the technical content of the supplement information associated
with any listed Mod/STC above is approved under the authority of the named Owner/Operator/Supplier of the document. The Owner/Operator/Supplier of the document has given the compiler of this supplement rights to use their information in order to produce this manual supplement.
C. The Checking process will include a verification of technical consistency with the associated Mod/STC and Compliance
documentation which may relate to effectivity, description, effects on airworthiness and environmental protection especially when limitations are changed or affected.
Checked: Print Name:
Approved: Print Name:
Mitchellh
Typewritten Text
Mitchell Hills
Mitchellh
Typewritten Text
Daniel Jackson
WIRING
DIAGRAM
MANUAL
Contents
WDM-CONTENTS Page 1
Produced by 365 Aerospace Limited, UK. AeroDEC own the copyright of the format of this Manual Supplement, which is supplied in confidence. The contents must not be reproduced without permission in writing from the owner.
Chapter 11 PLACARD & MARKINGS
Chapter 21 AIR CONDITIONING
Chapter 22 AUTO FLIGHT
Chapter 23 COMMUNICATIONS
Chapter 24 ELECTRICAL POWER
Chapter 25 EQUIPMENT/FURNISHINGS
25-32-21 – HOTCUP WIRING – GALLEY G1
Chapter 26 FIRE PROTECTION
Chapter 27 FLIGHT CONTROLS
Chapter 28 FUEL
Chapter 29 HYDRAULIC POWER
Chapter 30 ICE AND RAIN PROTECTION
Chapter 31 INDICATING/RECORDING SYSTEMS
Chapter 32 LANDING GEAR
Chapter 33 LIGHTS
Chapter 34 NAVIGATION
Chapter 35 OXYGEN
Chapter 36 PNEUMATIC
Chapter 38 WATER/WASTE
Chapter 49 AIRBORNE AUXILIARY POWER
Chapter 52 DOORS
WDM-CONTENTS Page 2
Produced by 365 Aerospace Limited, UK. AeroDEC own the copyright of the format of this Manual Supplement, which is supplied in confidence. The contents must not be reproduced without permission in writing from the owner.
Chapter 53 FUSELAGE
Chapter 54 NACELLES / PYLONS
Chapter 55 STABILIZERS
Chapter 56 WINDOWS
Chapter 57 WINGS
Chapter 71 POWER PLANT
Chapter 73 ENGINE FUEL AND CONTROL
Chapter 74 IGNITION
Chapter 75 AIR
Chapter 77 ENGINE INDICATING
Chapter 78 EXHAUST
Chapter 79 OIL
Chapter 80 STARTING
Chapter 91 CHARTS
Chapter 93 PANELS
WDM-LEF Page 1
Produced by 365 Aerospace Limited, UK. AeroDEC own the copyright of the format of this Manual Supplement, which is supplied in confidence. The contents must not be reproduced without permission in writing from the owner.
LIST OF EFFECTIVE PAGES
Description Page No. Date Description Page No. Date
WDM Front Page WDM Contents 1 WDM Contents 2 WDM-List of Effective Pages 1 Chapter 25 Front Page 25-32-21 1 AUG 01/17
CHAPTER
25 EQUIPMENT/
FURNISHINGS
B737-300/400/500 WIRING DIAGRAM MANUAL
HOT CUP WIRING – GALLEY G1 25-32-21 INCORPORATES: 25-32-21 365 AEROSPACE MDL-0321
Page 1 TO BE READ IN CONJUNCTION WITH DRIESSEN GALLEY G1 COMPONENT Page 1 MAINTENANCE MANUAL 25-32-21
AUG 01/17 AUG 01/17 Page produced by 365 Aerospace Limited, UK. Copyright ©. See Manual Supplement Introduction pages for information.
ILLUSTRATED
PARTS
CATALOGUE
Contents
IPC-CONTENTS Page 1
Chapter 11 PLACARD & MARKINGS
Chapter 21 AIR CONDITIONING
Chapter 22 AUTO FLIGHT
Chapter 23 COMMUNICATIONS
Chapter 24 ELECTRICAL POWER
Chapter 25 EQUIPMENT/FURNISHINGS
25-31-11-99Z – HOTCUP INSTL – GALLEY G1
Chapter 26 FIRE PROTECTION
Chapter 27 FLIGHT CONTROLS
Chapter 28 FUEL
Chapter 29 HYDRAULIC POWER
Chapter 30 ICE AND RAIN PROTECTION
Chapter 31 INDICATING/RECORDING SYSTEMS
Chapter 32 LANDING GEAR
Chapter 33 LIGHTS
Chapter 34 NAVIGATION
Chapter 35 OXYGEN
Chapter 36 PNEUMATIC
Chapter 38 WATER/WASTE
Chapter 49 AIRBORNE AUXILIARY POWER
IPC-CONTENTS Page 2
Chapter 52 DOORS
Chapter 53 FUSELAGE
Chapter 54 NACELLES / PYLONS
Chapter 55 STABILIZERS
Chapter 56 WINDOWS
Chapter 57 WINGS
Chapter 71 POWER PLANT
Chapter 73 ENGINE FUEL AND CONTROL
Chapter 74 IGNITION
Chapter 75 AIR
Chapter 77 ENGINE INDICATING
Chapter 78 EXHAUST
Chapter 79 OIL
Chapter 80 STARTING
Chapter 91 CHARTS
Chapter 93 PANELS
IPC-LEF Page 1
LIST OF EFFECTIVE PAGES
Description Page No. Date Description Page No. Date
IPC Front Page IPC Contents 1 IPC Contents 2 IPC-List of Effective Pages 1 Chapter 25 Front Page 25-31-11-99Z 0 AUG 01/17 25-31-11-99Z 1 AUG 01/17
CHAPTER
25 EQUIPMENT/
FURNISHINGS
B737-300/400/500 ILLUSTRATED PARTS CATALOGUE
25-31-11-99Z 25-31-11 MDL-0321 Fig 99Z AUG 01/17 Page 0
Page produced by 365 Aerospace Limited, UK. Copyright ©. See Manual Supplement Introduction pages for information.
HOT CUP INSTL – GALLEY G1 FIGURE 99Z
B737-300/400/500 ILLUSTRATED PARTS CATALOGUE
25-31-11-99Z 25-31-11 MDL-0321 Fig 99Z AUG 01/17 Page 1
Page produced by 365 Aerospace Limited, UK. Copyright ©. See Manual Supplement Introduction pages for information.
FIG ITEM PART NUMBER NOMENCLATURE EFF
CODE UNITS PER
ASSY 1234567
99Z --1 EO-0321-001 CHANGE TO INSTALL COMBO WATER BOILER HOT CUP RF --1 365-25-0311 INSTL OF DRIESSEN COMBO ASSY (365 AEROSPACE DRAWING) RF
10 JF003001 • COMBO ASSY 1 20 34-00318 • BRACKET 1 30 9-028-13 • SCREW 1 40 365-25-0072-001 • BRACKET 1 50 NAS514P1032-6 • SCREW 2 60 NAS1149D0332J • WASHER 4 70 NAS603-6 • SCREW 4 90 NAS514P632-12 • SCREW 4
100 NAS1149D0616J • WASHER 4 110 MS35649-262 • NUT 4 120 AC16707 • CONNECTOR 1 130 365-11-0007-101 • PLACARD – USER INSTRUCTIONS 1 140 AN935-6 • WASHER 4 150 NAS514P428-22 • SCREW 4 160 365-25-0103-101 • ADAPTER PANEL 1 170 NAS43DD1-10FC • SPACER 4
--180 TC342A-X • CLIP 1 --190 365-11-0005-001 • PLACARD – MODIFICATION 1
-- ITEMS NOT ILLUSTRATED
AIRCRAFT
MAINTENANCE
MANUAL
Contents
AMM-CONTENTS Page 1
Chapter 11 PLACARD & MARKINGS
Chapter 21 AIR CONDITIONING
Chapter 22 AUTO FLIGHT
Chapter 23 COMMUNICATIONS
Chapter 24 ELECTRICAL POWER
Chapter 25 EQUIPMENT/FURNISHINGS
25-32-00 – DRIESSEN COMBO / COMBINATION WATER BOILER HOT CUP
PAGE BLOCK 501 – ADJUSTMENT/TEST
Chapter 26 FIRE PROTECTION
Chapter 27 FLIGHT CONTROLS
Chapter 28 FUEL
Chapter 29 HYDRAULIC POWER
Chapter 30 ICE AND RAIN PROTECTION
Chapter 31 INDICATING/RECORDING SYSTEMS
Chapter 32 LANDING GEAR
Chapter 33 LIGHTS
Chapter 34 NAVIGATION
Chapter 35 OXYGEN
Chapter 36 PNEUMATIC
Chapter 38 WATER/WASTE
Chapter 49 AIRBORNE AUXILIARY POWER
AMM-CONTENTS Page 2
Chapter 52 DOORS
Chapter 53 FUSELAGE
Chapter 54 NACELLES / PYLONS
Chapter 55 STABILIZERS
Chapter 56 WINDOWS
Chapter 57 WINGS
Chapter 71 POWER PLANT
Chapter 73 ENGINE FUEL AND CONTROL
Chapter 74 IGNITION
Chapter 75 AIR
Chapter 77 ENGINE INDICATING
Chapter 78 EXHAUST
Chapter 79 OIL
Chapter 80 STARTING
Chapter 91 CHARTS
Chapter 93 PANELS
AMM-LEF Page 1
LIST OF EFFECTIVE PAGES
Description Page No. Date Description Page No. Date
AMM Front Page AMM Contents 1 AMM Contents 2 AMM-List of Effective Pages 1 Chapter 25 Front Page 25-32-00 501 AUG 01/17
CHAPTER
25 EQUIPMENT/
FURNISHINGS
B737-300/400/500 AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
25-32-00 AIRPLANES WITH DRIESSEN COMBO Page 501 MDL-0321 AUG 01/17
Page produced by 365 Aerospace Limited, UK. Copyright ©. See Manual Supplement Introduction pages for information.
DRIESSEN COMBO / COMBINATION WATER BOILER HOT CUP – ADJUSTMENT/TEST
1. General
A. This procedure has one task, to carry out an Operational Test of the Driessen Combo (Combination Water Boiler Hot Cup).
2. Operational Test
A. Procedure
1) Make sure that power is supplied to the aircraft (AMM Chapter 24).
2) On the unit, check to see if the orange "empty" LED, on the control panel, glows faintly. This indicates that the power is on and that the COMBO is ready to use.
3) Place an empty kettle in the combo holder and set both retainers in the
upright position.
4) Switch the COMBO on by pressing the "ON" switch. The "on" LED will light up green.
5) After a while the "hot" LED will start burning red, telling that the heating
plate of the combo holder is warmer than ±45°C (113°F).
6) Disengage one of the retainers and check to see if the COMBO stops heating. The green "on" LED stops burning. The red "hot" LED keeps burning as long as the hot plate is hot. Check both retainers one after the other.
7) Switch the COMBO on by pressing the "ON" switch. After several minutes the
orange "empty" LED starts blinking and the green "on" LED stops burning. This tells you that the kettle is empty and the heating process is stopped.
8) After the COMBO is sufficiently cooled down, the heating process can be
started again by pressing the "ON" switch. 9) Remove power from the aircraft if it is no longer required (AMM Chapter 24).
