Wireless Applications and Effect on IFE Ken Brady Chief Design Engineer Thales Avionics.
SPECIFICATION SUMMARY - ACJetexpert · 3/31/2018 · Display Unit Thales Avionics C19366AF05 6...
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SPECIFICATION SUMMARY Airbus A320-214 POS.# 2 Rev.: No. 3 Date: 31-MAR-2018 Confidentiality and Disclaimer: All rights reserved. This document is the sole property of t h e S e l l e r . This document has been drafted and distributed for information purposes only. This document may not be reproduced or (re) distributed or otherwise utilized in part or whole without the express prior written permission of t h e S e l l e r . While the information presented in this document is given in good faith based upon the most current information available to t h e S e l l e r , changes or modifications with respect to the subject aircraft and the associated records and documentation may be made at any time. No express or implied warranty or representation is made and this document may not be regarded as establishing any obligation on the part of t h e S e l l e r or any of its affiliates. It is expected that interested parties will conduct an independent physical inspection of the aircraft and associated records and documentation.
Transcript of SPECIFICATION SUMMARY - ACJetexpert · 3/31/2018 · Display Unit Thales Avionics C19366AF05 6...
SPECIFICATION SUMMARY
Airbus A320-214 POS.# 2
Rev.: No. 3 Date: 31-MAR-2018
Confidentiality and Disclaimer:
All rights reserved. This document is the sole property of t h e S e l l e r . This document has been drafted and distributed for information purposes only. This document may not be reproduced or (re) distributed or otherwise utilized in part or whole without the express prior written permission of t h e S e l l e r . While the information presented in this document is given in good faith based upon the most current information available to t h e S e l l e r , changes or modifications with respect to the subject aircraft and the associated records and documentation may be made at any time. No express or implied warranty or representation is made and this document may not be regarded as establishing any obligation on the part of t h e S e l l e r or any of its affiliates. It is expected that interested parties will conduct an independent physical inspection of the aircraft and associated records and documentation.
A320-214 MSN.TBA Page 2 of 12
WEIGHTS, OPERATIONAL Metric US Customary
Maximum Taxi Weight (MTW) 77`400 (Kg) 170`638 (Lbs)
Maximum Take Of Weight (MTOW) 77`000 (Kg) 169`760 (Lbs)
Maximum Landing Weight (MLW) 64`000 (Kg) 141`096 (Lbs)
Maximum Zero Fuel Weight (MZFW) 61`000 (Kg) 134`482 (Lbs)
Minimum Weight (MW) 38`296 (kg) 84`428 (Lbs)
Operator`s Empty Weight (OEW) * 43`842 (kg) 96`655 (Lbs)
Maximum Structural Payload * 20`100 (kg) 44 313` (Lbs)
Fuel Capacity (FC) 23`859 (Ltr) 6`303 (USG) * ESTIMATED
AIRFRAME STATUS Total Airframe Hours 34`823
Total Cycles 17`682
Status Date 31-AUG-2017 NOTE: AIRCARFT IS IN STORAGE SINCE NOVEMBER 2017
MAINTENANCE STATUS C - Check interval 7`500 FH / 5`000 FC / 24 MO
6Y - Check interval 72 MO
12Y - Check interval 144 MO
Last C - Check 09-JAN-2016 at 30`040 FH & 15`335 FC
Last 6Y – Check FEB-2012
Last 12Y – Check NONE
Next C – Check JAN-2018
Next 6Y – Check FEB-2018
Next 12Y - Check FEB-2018
AIRCRAFT IDENTIFICATION
Aircraf Model A320-214
Manufacturer Serial Number TBA
Manufacture Date FEB – 2006
Aircraf Registraton TBA
Engines Model CFM56-5B
APU Model GTCP 131-9 [A]
A320-214 MSN.TBA Page 3 of 12
ENGINE / APU DETAILS Engine 1 Engine 2 APU
Manufacturer CFMI CFMI Honeywell
Model CFM56-5B4/P CFM56-5B4/P GTCP 131-9 [A]
Thrust Rate 27`000 Lbf 27`000 Lbf
ENGINE / APU STATUS Engine 1 Engine 2 APU
Serial Number TBA TBA TBA
Total Time Since New 35`828 33`847 16`585
Total Cycles Since New 19`951 18`660 27`921
Last Shop Visit NONE NONE TBA
Hours Since Last Shop Visit N/A N/A TBA
Cycles Since Last Shop Visit N/A N/A TBA
Last Overhaul NONE NONE TBA
Hours Since Last Overhaul N/A N/A TBA
Cycles Since Last Overhaul N/A N/A TBA
First LLP Limiter 49 1`340 TBA
Status Date 27-NOV-2017 27-NOV-2017 01-SEP-2017
A320-214 MSN.TBA Page 4 of 12
ENGINE Pos.#1 - LLP Status
NO. PART NAME PART NUMBER TOTAL HOURS
TOTAL CYCLES
LIFE LIMIT CYCLES
REMAINING CYCLES
LPC ROTOR ASSY 1 ) DISK, FAN STG.1 338-001-504-0 35`828 19`951 30`000 10`049 2 ) SPOOL, BOOSTER 338-001-906-0 35`828 19`951 30`000 10`049 3 ) SHAFT, FAN 338-010-601-0 35`828 19`951 30`000 10`049 HPC ROTOR ASSY
4 ) FRONT SHAFT, HPC 1386M56P03 35`828 19`951 20`000 `49 5 ) HPC ROTOR SPOOL STG 1 & 2 1558M31G04 35`828 19`951 20`000 `49 6 ) HPC ROTOR DISK STG 3 1590M59P01 35`828 19`951 20`000 `49 7 ) HPCR SPOOL ASSY STG 4-9 1588M89G03 35`828 19`951 20`000 `49 8 ) CDP ROTATING REAR AIR SEAL 1523M35P01 35`828 19`951 20`000 `49 HPT ROTOR ASSY
9 ) HPT FRONT ROTATING AIR SEAL 1795M36P02 35`828 19`951 20`000 `49 10 ) HPT ROTOR FRONT SHAFT 1873M73P01 35`828 19`951 20`000 `49 11 ) DISK - HPT ROTOR 1498M43P06 35`828 19`951 20`000 `49 12 ) HPT REAR SHAFT 1864M90P05 35`828 19`951 20`000 `49
LPT ROTOR ASSY 13 ) LPT ROTOR DISK STG 1 336-001-804-0 35`828 19`951 25`000 5`049 14 ) LPT ROTOR DISK STG 2 336-001-909-0 35`828 19`951 25`000 5`049 15 ) LPT ROTOR DISK STG 3 336-002-006-0 35`828 19`951 25`000 5`049 16 ) LPT ROTOR DISK STG 4 336-002-105-0 35`828 19`951 25`000 5`049 17 ) LPT SHAFT 338-010-005-0 35`828 19`951 25`000 5`049 18 ) LPT ROTOR SUPPORT 338-077-502-0 35`828 19`951 25`000 5`049 Status Date: 27-Nov-2017
A320-214 MSN.TBA Page 5 of 12
ENGINE Pos.#2 - LLP Status
NO. PART NAME PART NUMBER TOTAL HOURS
TOTAL CYCLES
LIFE LIMIT CYCLES
REMAINING CYCLES
LPC ROTOR ASSY 1 ) DISK, FAN STG.1 338-001-504-0 33`847 18`660 30`000 11`340 2 ) SPOOL, BOOSTER 338-001-906-0 33`847 18`660 30`000 11`340 3 ) SHAFT, FAN 338-010-601-0 33`847 18`660 30`000 11`340 HPC ROTOR ASSY
4 ) FRONT SHAFT, HPC 1386M56P03 33`847 18`660 20`000 1`340 5 ) HPC ROTOR SPOOL STG 1 & 2 1558M31G04 33`847 18`660 20`000 1`340 6 ) HPC ROTOR DISK STG 3 1590M59P01 33`847 18`660 20`000 1`340 7 ) HPCR SPOOL ASSY STG 4-9 1588M89G03 33`847 18`660 20`000 1`340 8 ) CDP ROTATING REAR AIR SEAL 1523M35P01 33`847 18`660 20`000 1`340 HPT ROTOR ASSY
9 ) HPT FRONT ROTATING AIR SEAL 1795M36P02 33`847 18`660 20`000 1`340 10 ) HPT ROTOR FRONT SHAFT 1873M73P01 33`847 18`660 20`000 1`340 11 ) DISK - HPT ROTOR 1498M43P06 33`847 18`660 20`000 1`340 12 ) HPT REAR SHAFT 1864M90P05 33`847 18`660 20`000 1`340
LPT ROTOR ASSY 13 ) LPT ROTOR DISK STG 1 336-001-804-0 33`847 18`660 25`000 6`340 14 ) LPT ROTOR DISK STG 2 336-001-909-0 33`847 18`660 25`000 6`340 15 ) LPT ROTOR DISK STG 3 336-002-006-0 33`847 18`660 25`000 6`340 16 ) LPT ROTOR DISK STG 4 336-002-105-0 33`847 18`660 25`000 6`340 17 ) LPT SHAFT 338-010-005-0 33`847 18`660 25`000 6`340 18 ) LPT ROTOR SUPPORT 338-077-502-0 33`847 18`660 25`000 6`340 Status Date: 27-Nov-2017
A320-214 MSN.TBA Page 6 of 12
LDG DETAILS NLG LH MLG RH MLG Manufacturer MESSIER-BUGATTI-DOWTY
Part Number D237575500-8 201582001-30 201582002-30
Serial Number TBA TBA TBA
Positon NLG LH MLG RH MLG
Hours Since New TBA TBA TBA
Cycles Since New 18`507 18`507 18`507
Last Overhaul Date 28-JAN-2016 28-JAN-2016 28-JAN-2016
Cycles Since Overhaul 2`329 2`329 2`329
Remaining Cycles 17`671 17`671 17`671
Overhaul Due Date 27-JAN-2026 27-JAN-2026 27-JAN-2026
Overhaul Interval 20`000 CYC
or 10 Years
20`000 CYC
or 10 Years
20`000 CYC
or 10 Years
Life (Scrap) Limit 60`000 CYC 60`000 CYC 60`000 CYC
Brakes & Part Number SAFRAN: C20225510
Wheels & Part Number GOODRICH/3-1531/3 SAFRAN/C20195162 SAFRAN/C20195162
Status Date 29-AUG-2017 29-AUG-2017 29-AUG-2017
A320-214 MSN.TBA Page 7 of 12
MAJOR AVIONICS EQUIPMENT DESCRIPTION MANUFACTURER PART NUMBER QTY
ATA 22 - Automati Flight Controls Flight Control Computer MCDU Thales Avionics C19266AA01 2 Mode Control Panel Thales Avionics C12850AC02 1 Flight Management Computer Northrop Grumman 87232329V03 8
ATA 23 – Communiiaton VHF Transceiver Thales Avionics EVR750-04-0100A 3 RADIO Tuning Panel TEAM ACP2788AB05 3
ATA 31 - Indiiaton and Reiording System Display Unit Thales Avionics C19366AF05 6 Display Management Computer Thales Avionics C1982660116 3 CFDIU Thales Avionics C12860AA02 1 CVR-Solid State L-3 Communicatons 2100-1025-02 1 FDR-Solid State L-3 Communicatons 2100-4043-02 1
ATA 34 – Navigaton MMR – Mult Mode Receiver ILS/GPS Thales Avionics TLS755-01-0101B 2 ADIRU (Air Data Inertal Reference Unit) Northrop Grumman 465020-03030315 3 CDU Northrop Grumman 465010-0300-300 1 Weather Radar (WRX) Rockwell Collins 822-1710-202 1 Radio Altmeter Transceiver (RA) Thales Optronic 9599-607-14942 2 ATC-Mode S Transponder L-3 Communicatons 7517800-10005 2 TCAS II 7.0 Computer Thales Avionics C12404AB02 1 VOR Receiver Rockwell Collins 822-0297-020 2 DME Interrogator Rockwell Collins 822-0329-020 2 ADF Receiver Rockwell Collins 822-0299-020 1
A320-214 MSN.TBA Page 8 of 12
MODIFICATION STATUS COMPLIANCE NOTEs AIRBUS STD. SPEC. J000 0100 / ISSUE 05 TBA
EASA TCDS EASA.A.064
NOISE Abatement Compliance Yes Stage IV iaw. ICAO Annex 16, Volume I, Part II
Approach Category Yes CAT III B
ETOPS No
Over Water capability No
Sharklets/Winglets No
Auxiliary Fuel Capacity No
Fuel Tank Inertng System (AIRBUS) No EASA – P by 01-JAN-2012; R – Not required FAA – P by 28-DEC-2010 / R 100% Fleet by 26-DEC-2017
Nitrogen Gas System (BOEING) N/A
Reinforced Cockpit Door Yes
Cockpit 4th occupant seat TBA
Cargo Fire Suppression TBA
Cargo Loading System No
Cockpit Door Surveillance System Yes
EGPWS Yes
RVSM Yes
TCAS 7.1 Yes EASA – P on 12-MAR-2014 / R on 01-DEC-2015 FAA – Not required
Enhanced Surveillance (EHS) Mode S, ATC Transponder TBA
Elementary Surveillance (ELS) Yes
ATC Mode S Transponder ADS-B Out DO 260B capability No EASA – P on 08-JUN-2016 & R on 07-JUN-2020 FAA – P & R on 01-JAN-2020
Predictve Windshear TBA
Head Up Display (HUD) No EASA / FAA – Not mandatory CAAC – R - 10% Fleet by 2015 & R - 100% by 2025
Area Navigaton (BRNAV & PRNAV) Yes BRNAV = +/- 5 NM RNAV5 & PRNAV = +/- 1 NM RNAV1
Aircraf Performance Based Navigaton (PBN) Capability
A/C PBN APPROVAL = RNP APCH (to LNAV/VNAV) TBA
EASA – 3 Phase Approach – Various dates FAA – Not required
GPS Installed Yes
FM Immunity Yes
VHF 8.33 kHz Chanel spacing Yes EASA – Mandatory above FL195 FAA – Not mandatory
FANS 1/A Installed & Actvated TBA EASA & FAA on NAT between FL350-390
FANS B – ADS-B/ADS-C Yes
ATN B1 Data Link (CPDLC) Installed TBA EASA – P & R on 05-FEB-2020 for AC > JAN-2003 and R on 01-JAN-2023 for AC < JAN-2003 FAA – Not required
SATCOM Installed No EASA – Not mandatory FAA – Mandatory, if ETOPS > 180 Mins CAAC – R - 50% Fleet by 2015 & R - 100% by 2017
CVR with Data Link Recording Yes EASA – P on 08-APR-2014 / R on 01-JAN-2016 CAT.IDE.A195 FAA – P & R on 12-DEC-2010
SSCVR 2Hrs + ULB 90 Days No EASA – P & R by 01-JUN-2018 FAA – ULB < 30 Days by 01-DEC-2015 & < 90 Days by 01-DEC-2015
SSFDR + ULB 90 Days No
Low Frequency Underwater Locator Device (ULD) No EASA – P & R by 01-JAN-2019 CAT.IDE.A190 FAA / CAAC – Not required
ELT 121.5 / 406 MHz - Fixed Yes
ELT 121.5 / 243 / 406 MHz - Portable Yes
NOTE: P – PRODUCTION & R - RETROFIT
A320-214 MSN.TBA Page 9 of 12
INTERIOR CONFIGURATION Galleys 2 (G1; G5) Catering Standard ATLAS
Lavatories 3 (A; D; E) Ovens/Water Boilers/Cofey Makers 4/0/4
Atendant Seats 6 (2+4) Cargo Confguraton All Bulk – No CLS
In Flight Entertainment Yes (Panasonic) Cockpit Confguraton Standard
Seats Quantty Manufaiturer Part Number
Economy Class 180 RECARO 3510A
A320-214 MSN.TBA Page 10 of 12
EMERGENCY EQUIPMENT
A320-214 MSN.TBA Page 11 of 12
CARGO CONFIGURATION Cargo Confguraton All Bulk-No CLS Designee (Fire Detecton/Protecton) class C
Cargo Volume 37.42 3Metres Containers No
Load Limitaton 9`435 Kg Main Cargo Door(s) 71” x 48”
A320-214 MSN.TBA Page 12 of 12
PERFORMANCE
