airbus a320-200thales c16221wb01 1 enhanced ground proximity warning computer honeywell 965-1676-002...
TRANSCRIPT
SPECIFICATION SUMMARY
Airbus A320-200
Rev.: No. 3 Date: 26-SEP-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.
A320-200 MSN. TBA Page 2 of 12
WEIGHTS, OPERATIONAL Metric US Customary
Maximum Taxi Weight (MTW) 77`400 (Kg) 170`637 (Lbs)
Maximum Take Off Weight (MTOW) 77`000 (Kg) 169`756 (Lbs)
Maximum Landing Weight (MLW) 66`000 (Kg) 145`505 (Lbs)
Maximum Zero Fuel Weight (MZFW) 62`500 (Kg) 137`789 (Lbs)
Minimum Weight (MW) 37`230 (kg) 82`079 (Lbs)
Operator`s Empty Weight (OEW) 42`571 (kg) 93`853 (Lbs)
Maximum Structural Payload * 20`200 (kg) 44`533 (Lbs)
Fuel Capacity (FC) 23`860 (Liters) 6`303 (USG) * ESTIMATED
AIRCRAFT IDENTIFICATION
Aircraft Model A320-214
Manufacturer Serial Number TBA
Manufacture Date MAY – 2007
Aircraft Registration TBA
Engines Model CFM56-5B4/P
APU Model GTCP-131-9[A]
DELIVERY SUMMARY
Certification: EASA
Airframe: Fresh from C, 6Y & 12Y-check
Engines: As IS, installed on the aircraft & within the limits of the manufacturer;
MPA Run and BSI to be performed
APU: Serviceable
Landing Gears: As IS, Serviceable & Airworthy
Components: Serviceable & Airworthy
Painting: Painted in White
Interior Conf.: Clean, Normal wear & tear
Airworthiness Directives:
In compliance on the delivery date
Documents & Records:
Up to date, in English
A320-200 MSN. TBA Page 3 of 12
AIRFRAME STATUS Total Airframe Hours 41`406
Total Cycles 17`822
Status Date 31-AUG-2018 NOTE: AVERAGE UTILISATION 300 FH & 130 FC PER MONTHS
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 28-OCT-2016 at 34`905 FH & 14`894 FC
Last 6Y – Check 24-JAN-2013 at 21`202FH & 8`713 FC
Last 12Y – Check N/A
Next C – Check 27-OCT-2018
Next 6Y – Check 23-JAN-2019
Next 12Y - Check 02-MAY-2019
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 Lbs 27`000 Lbfs
ENGINE / APU STATUS Engine 1 Engine 2 APU
Serial Number TBA TBA TBA
Total Time Since New 28`264 38`058 14`530
Total Cycles Since New 11`769 15`919 23`952
Last Shop Visit 20-APR-2018 26-JAN-2016 14-DEC-2016
Hours Since Last Shop Visit 1`490 7`218 2`131
Cycles Since Last Shop Visit 624 2`894 3`620
Last Overhaul NONE NONE NONE
Hours Since Last Overhaul N/A N/A N/A
Cycles Since Last Overhaul N/A N/A N/A
First LLP Limiter 8`231 4`081 21`704
Status Date 23-SEP-2018 23-SEP-2018 23-SEP-2018 NOTE: AVERAGE UTILISATION 300 FH & 130 FC PER MONTHS
A320-200 MSN. TBA Page 4 of 12
ENGINE Pos.#1 - LLP
ENGINE TYPE: TSN: 28.264 EFH TSLSV: 0 EFH DATE:
CFM56-5B6/P CSN: 11.769 EFC CSLSV: 0 EFC 23.sept.2018
NO. PART NAME PART NUMBER TOTAL HOURS
TOTAL CYCLES
LIFE LIMIT CYCLES
REMAINING CYCLES
LPC ROTOR ASSY
1 ) SHAFT, FAN 338-010-601-0 28`264 11`769 30`000 18`231
2 ) DISK STG.1, FAN 338-001-504-0 28`264 11`769 30`000 18`231
3 ) SPOOL, BOOSTER 338-001-906-0 28`264 11`769 30`000 18`231
HPC ROTOR ASSY
4 ) FRONT SHAFT, HPC 1386M56P03 28`264 11`769 20`000 8`231
5 ) HPC ROTOR SPOOL STG 1 & 2 1558M31G04 28`264 11`769 20`000 8`231
6 ) HPC ROTOR DISK STG 3 1590M59P01 28`264 11`769 20`000 8`231
7 ) HPCR SPOOL ASSY STG 4-9 1588M89G03 28`264 11`769 20`000 8`231
8 ) CDP ROTATING REAR AIR SEAL 1523M35P01 28`264 11`769 20`000 8`231
HPT ROTOR ASSY
9 ) HPT ROTOR FRONT SHAFT 1873M73P01 28`264 11`769 20`000 8`231
10 ) HPT FRONT ROTATING AIR SEAL 1795M36P02 1`490 `624 20`000 19`376
11 ) DISK - HPT ROTOR 1498M43P06 28`264 11`769 20`000 8`231
12 ) HPT REAR SHAFT 1864M90P05 28`264 11`769 20`000 8`231
LPT ROTOR ASSY
13 ) LPT SHAFT 338-010-005-0 28`264 11`769 25`000 13`231
14 ) LPT ROTOR DISK STG 1 336-001-804-0 28`264 11`769 25`000 13`231
15 ) LPT ROTOR DISK STG 2 336-001-909-0 28`264 11`769 25`000 13`231
16 ) LPT ROTOR DISK STG 3 336-002-006-0 28`264 11`769 25`000 13`231
17 ) LPT ROTOR DISK STG 4 336-002-105-0 28`264 11`769 25`000 13`231
18 ) LPT ROTOR SUPPORT 338-077-502-0 28`264 11`769 25`000 13`231
NOTE: AVERAGE UTILISATION 300 FH & 130 FC PER MONTHS
A320-200 MSN. TBA Page 5 of 12
ENGINE Pos.#2 - LLP
ENGINE TYPE: TSN: 38.058 EFH TSLSV: 0 EFH DATE:
CFM56-5B4 CSN: 15.919 EFC CSLSV: 0 EFC 23.sept.2018
NO. PART NAME PART NUMBER TOTAL HOURS
TOTAL CYCLES
LIFE LIMIT CYCLES
REMAINING CYCLES
LPC ROTOR ASSY
1 ) SHAFT, FAN 338-010-601-0 38`058 15`919 30`000 14`081
2 ) DISK STG.1, FAN 338-001-504-0 38`058 15`919 30`000 14`081
3 ) SPOOL, BOOSTER 338-001-906-0 38`058 15`919 30`000 14`081
HPC ROTOR ASSY
4 ) FRONT SHAFT, HPC 1386M56P03 38`058 15`919 20`000 4`081
5 ) HPC ROTOR SPOOL STG 1 & 2 1558M31G04 38`058 15`919 20`000 4`081
6 ) HPC ROTOR DISK STG 3 1590M59P01 38`058 15`919 20`000 4`081
7 ) HPCR SPOOL ASSY STG 4-9 1588M89G03 38`058 15`919 20`000 4`081
8 ) CDP ROTATING REAR AIR SEAL 1523M35P01 38`058 15`919 20`000 4`081
HPT ROTOR ASSY
9 ) HPT ROTOR FRONT SHAFT 1873M73P01 38`058 15`919 20`000 4`081
10 ) HPT FRONT ROTATING AIR SEAL 1795M36P02 38`058 15`919 20`000 4`081
11 ) DISK - HPT ROTOR 1498M43P06 38`058 15`919 20`000 4`081
12 ) HPT REAR SHAFT 1864M90P05 38`058 15`919 20`000 4`081
LPT ROTOR ASSY
13 ) LPT SHAFT 338-010-005-0 38`058 15`919 25`000 9`081
14 ) LPT ROTOR DISK STG 1 336-001-804-0 38`058 15`919 25`000 9`081
15 ) LPT ROTOR DISK STG 2 336-001-909-0 38`058 15`919 25`000 9`081
16 ) LPT ROTOR DISK STG 3 336-002-006-0 38`058 15`919 25`000 9`081
17 ) LPT ROTOR DISK STG 4 336-002-105-0 38`058 15`919 25`000 9`081
18 ) LPT ROTOR SUPPORT 338-077-502-0 33`410 18`325 25`000 6`675
NOTE: AVERAGE UTILISATION 300 FH & 130 FC PER MONTHS
A320-200 MSN. TBA Page 6 of 12
LDG DETAILS NLG LH MLG RH MLG Part Number NA28008-10 201581001 201581002
Serial Number TBA TBA TBA
Position NLG LH MLG RH MLG
Hours Since New 43`390 43`390 43`390
Cycles Since New 20`362 20`362 20`362
Last Overhaul Date 08-APR-2017 08-APR-2017 08-APR-2017
Cycles Since Overhaul 2`259 2`259 2`259
Remaining Cycles 17`741 17`741 17`741
Overhaul Due Date 08-APR-2027 08-APR-2027 08-APR-2027
Overhaul Interval 20`000 CYC
or 10 Years
20`000 CYC
or 10 Years
20`000 CYC
or 10 Years
Brakes & Part Number Messier C202255XX
Status Date 12-AUG-2018 12-AUG-2018 12-AUG-2018 NOTE: AVERAGE UTILISATION 300 FH & 130 FC PER MONTHS
A320-200 MSN. TBA Page 7 of 12
MAJOR AVIONICS EQUIPMENT DESCRIPTION MANUFACTURER PART NUMBER QTY
ATA 22 - Automatic Flight Controls FMGC Thales Avionics C13043AA06 2 FAC Thales Avionics B397BAM0624 2 FCU Thales Avionics C12850AC03 1 MCDU Thales Avionics C19266DA01 2
ATA 23 – Communication HF Transceiver Honeywell 964-0452-012 1 VHF Transceiver Honeywell 064-50000-0505 3 Cockpit Voice Recorder Honeywell 980-6022-001 1 PRAM / iPRAM (Integrated PRAM) Panasonic RD-AX7675-51 1 Tape Reproducer or CD Player (Audio Entertainment)
Panasonic RD-AX7095-01 1
Tape Reproducer or DVD Player (Video Entertainment)
Panasonic RD-AV1216-01 1
Audio Management Unit TEAM AMU4031SA140204 1 ATA 31 - Indication and Recording System FDR –Flight Data Recorder Honeywell 980-4700-042 1 FDIU – Flight Data Interface Unit Thales Avionics C12860AA02 1 FDIMU – Flight Data Interface and Management Unit
sfim ED48A100 1
Multi-Use Printer Honeywell 8055515-4501 1
ATA 34 – Navigation ADIRU – Air Data Inertial Reference Unit Northrop Grumman 465020-03030316 3 ISIS – Integrated Standby Instrument System
Thales C16221WB01 1
Enhanced Ground Proximity Warning Computer
Honeywell 965-1676-002 1
Weather Radar Transceiver Honeywell 066-50008-0409 1 TCAS Computer Honeywell 940-0351-001 1 ATC Mode S Transponder Honeywell 066-01127-1402 2 DME Interrogator Honeywell 066-50013-0202 2 VOR Receiver Honeywell 066-50012-0212 2 MMR – Multi-Mode Receiver Thales TLS755-01-0101B 2 Radio Altimeter Transceiver Honeywell 066-50007-0232 2 ADF Receiver Rockwell Collins 822-0299-020 1
A320-200 MSN. TBA Page 8 of 12
MODIFICATION STATUS COMPLIANCE NOTEs AIRBUS STD. SPEC. D000 02000 / ISSUE Yes
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 Yes 90 min
Over Water capability Yes
Sharklets/Winglets No
Auxiliary Fuel Capacity No
Fuel Tank Inerting 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 Yes
Cargo Fire Suppression Yes
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 Yes
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
Predictive Windshear Yes
Head Up Display (HUD) No EASA / FAA – Not mandatory
CAAC – R - 10% Fleet by 2015 & R - 100% by 2025
Area Navigation (BRNAV & PRNAV) Yes BRNAV = +/- 5 NM RNAV5 & PRNAV = +/- 1 NM RNAV1
Aircraft Performance Based Navigation (PBN) Capability
A/C PBN APPROVAL = RNP APCH (to LNAV/VNAV) Yes
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 & Activated No EASA & FAA on NAT between FL350-390
FANS B+ Installed & Activated No
ATN B1 Data Link (CPDLC) Installed Yes 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 Yes 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 Yes
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
A320-200 MSN. TBA Page 9 of 12
INTERIOR CONFIGURATION Galleys 2 (G1; G5) Catering Standard ATLAS
Lavatories 3 (A; D; E) Ovens/Water Boilers/Coffey Makers 3+5+0
Attendant Seats 6 (2+4) Cargo Configuration Bulk
In Flight Entertainment Yes Cockpit Configuration Standard (2+2)
Seats Quantity Manufacturer Part Number
Economy Class 174 B/E Aerospace 1013165-XXX
A320-200 MSN. TBA Page 10 of 12
CARGO CONFIGURATION Cargo Configuration Bulk Designee (Fire Detection/Protection) class TBA
Cargo Volume 37.42 3Metres Containers No
Load Limitation 9`435 Kg Main Cargo Door(s) 71” x 48”
A320-200 MSN. TBA Page 11 of 12
EMERGENCY EQUIPMENT
A320-200 MSN. TBA Page 12 of 12
PERFORMANCE
AIRCRAFTFINANCEGERMANY.COM