2009 Airbus A330-200
AIRBUS A330-200
AIRCRAFT IDENTIFICATION
Aircraft Model
Manufacturer Serial Number
Manufacture Date
Aircraft Registration
Engines Model
Sharklets/Winglets
Noise Abatement Compliance
Approach Category
ETOPS
Over Water
AIRBUS A330-223
Q1 – 2009
TBA
PW4168A
YES
Stage IV iaw. ICAO Annex 16, Volume 1
CAT III Capable
180 min
YES
WEIGHTS, OPERATIONAL
Metric
Maximum Taxi Weight (MTW)
Maximum Take Off Weight (MTOW)
Maximum Landing Weight (MLW)
Maximum Zero Fuel Weight (MZFW)
Operator`s Empty Weight (OEW)
Maximum Payload
Maximum Fuel Capacity
Auxiliary Fuel Capacity
233`900 (kg)
233`000 (kg)
182`000 (kg)
170`000 (kg)
121`397 (kg)
48`632 (kg)
139`090 (Litres)
None
US Customary
515`661 (lbs.)
513`677 (lbs.)
401`241 (lbs.)
374`786 (lbs.)
267`635 (lbs.)
107`215 (lbs.)
36`746 (USG)
None
AIRFRAME STATUS
Total Airframe Hours 32`048
Total Cycles 6`525
Status Date 23-AUG-2017
NOTE: WV 022
MAINTENANCE STATUS
C - Check interval 24 MO
6Y - Check interval 72 MO
12Y - Check interval 144 MO
Last C - Check 5C on 26 – APR – 2017 at 32`043 FH & 6`524 FC
Last 6Y – Check 10 – NOV – 2014 at 26`331 FH & 4`937 FC
Last 12Y – Check NONE
Next C – Check APR – 2019
Next 6Y – Check NOV – 2020
Next 12Y - Check JAN – 2021
A330-200
MSN. TBA
Page 2 of 10
ENGINE / APU DETAILS
Manufacturer
Model
Thrust Rate
ENGINE / APU STATUS
Serial Number
Total Time Since New
Total Cycles Since New
Last Shop Visit
Hours Since Last Shop Visit
Cycles Since Last Shop Visit
Last Overhaul
Hours Since Last Overhaul
Cycles Since Last Overhaul
First LLP Limiter
Status Date
LDG DETAILS
Manufacturer
Part Number
Serial Number
Position
Cycles Since New
Last Overhaul Date
Cycles Since Overhaul
Remaining Cycles
Overhaul Due Date
Overhaul Interval
Engine 1
Engine 2
Pratt & Whitney
PW4168A
68`600 Lbf
Pratt & Whitney
PW4168A
68`600 Lbf
GTCP 331-350C
Engine 1
Engine 2
APU
TBA
27`336
5`424
MAR-2015
(EPR)
4`745
1`253
NONE
N/A
N/A
7`176
23-AUG-2017
TBA
27`016
5`413
SEP-2016
(EPR)
7
2
NONE
N/A
N/A
7`187
23-AUG-2017
TBA
5`746
6`739
NLG
D23581100-16
TBA
NLG
6`525
NONE
N/A
10`475
JAN-2019
17`000 CYC
or 10 Years
Brakes & Part Number
Wheels & Part Number BF Goodrich P/N: 3-1596
23-AUG-2017
Status Date
A330-200
MSN. TBA
LH MLG
APU
Honeywell
JAN-2016
6
14
JAN-2016
6
14
TBA
23-AUG-2017
RH MLG
Messier Dowty
10-210101-003
10-210201-003
TBA
TBA
LH MLG
RH MLG
6`525
6`525
NONE
NONE
N/A
N/A
10`475
10`475
JAN-2019
JAN-2019
17`000 CYC
17`000 CYC
or 10 Years
or 10 Years
BF Goodrich P/N: 2-1577-X
BF Goodrich P/N: 3-1546
23-AUG-2017
23-AUG-2017
Page 3 of 10
ENGINE Pos.#1 - LLP
STAGE
LP COMRESSOR / FAN MODULE
LPC - DRUM ROTOR (1.3,1.6,2,3,4 STAGES)
LPC - FRONT HUB
LPC -/LPT TURB SHAFT COUPLING
HP COMRESSOR MODULE
HPC - 5TH STAGE DISK
HPC - DRIVE SHAFT
HPC - DRUM ROTOR (13-15 STAGES)
HPC - DRUM ROTOR (6-12 STAGES)
HPC - FRONT HUB
HPC - INLET/DIFFUSER AIRSEAL (REF 1435)
HP TURBINE MODULE
HPT - FRONT T1 HUB
HPT - REAR INTERMEDIATE T2 HUB
HPT - T1 AIRSEAL OUTER ROTATING (REF 1752)
HPT - T1 RING AIRSEAL (REF 1756)
HPT - T2 AIRSEAL (ROTATING)
HPT - T2 BLADE RETAINING PLATE
LP TURBINE MODULE
LPT - 3RD STAGE AIRSEAL (REF 1224)
LPT - 3RD STAGE DISK
LPT - 4TH STAGE AIRSEAL
LPT - 4TH STAGE DISK
LPT - 5TH STAGE AIRSEAL
LPT - 5TH STAGE REAR HUB
LPT - 6TH STAGE DISK
LPT - 3RD STAGE AIRSEAL
LPT - 7TH STAGE DISK
LPT - SHAFT - FRONT COMPR DRIVE
A330-200
PART NO.
SERIAL NO.
LIMIT
50B882-01
52B021
51A275
CBDUCM1775
CBDUCM9715
CLDLDC1527
15`000
15`000
15`000
9`576
9`576
9`576
54H405
54H767
58H236-01
50S106-01
51H572
54H792
CENCBE4263
CENCC25668
CENCDM3907
CLDLDF3876
CENCCY6561
CENCDG6899
15`000
15`000
15`000
15`000
15`000
15`000
9`576
9`576
10`259
9`576
9`576
9`576
51L901
52L002
50L879
50L664
53L030
50L242
CKLBKC9994
CKLBKE8584
CKLBJS5808
CKLBKD8629
CKLBJ68385
CKLBJ59293
15`000
15`000
12`600
15`000
13`900
15`000
9`576
9`576
7`176
9`576
8`476
9`576
50N521
50N803
51N038
51N404
50N419
51N505
50N886
50N420
50N587
52A519-01
CLDLC19097
CLDLDF9006
CLDLC57216
CLDLDG2564
CLDLC89141
CLDLDB4462
CLDLDG0906
CLDLDE6028
CLDLDB5387
CLDLDF9493
15`000
15`000
15`000
15`000
15`000
15`000
15`000
15`000
15`000
15`000
9`576
9`576
9`576
9`576
9`576
9`576
9`576
9`576
9`576
9`576
MSN. TBA
REMAIN
Page 4 of 10
ENGINE Pos.#2 - LLP
STAGE
LP COMRESSOR / FAN MODULE
LPC - DRUM ROTOR (1.3,1.6,2,3,4 STAGES)
LPC - FRONT HUB
LPC -/LPT TURB SHAFT COUPLING
HP COMRESSOR MODULE
HPC - 5TH STAGE DISK
HPC - DRIVE SHAFT
HPC - DRUM ROTOR (13-15 STAGES)
HPC - DRUM ROTOR (6-12 STAGES)
HPC - FRONT HUB
HPC - INLET/DIFFUSER AIRSEAL (REF 1435)
HP TURBINE MODULE
HPT - FRONT T1 HUB
HPT - REAR INTERMEDIATE T2 HUB
HPT - T1 AIRSEAL OUTER ROTATING (REF 1752)
HPT - T1 RING AIRSEAL (REF 1756)
HPT - T2 AIRSEAL (ROTATING)
HPT - T2 BLADE RETAINING PLATE
LP TURBINE MODULE
LPT - 3RD STAGE AIRSEAL (REF 1224)
LPT - 3RD STAGE DISK
LPT - 4TH STAGE AIRSEAL
LPT - 4TH STAGE DISK
LPT - 5TH STAGE AIRSEAL
LPT - 5TH STAGE REAR HUB
LPT - 6TH STAGE DISK
LPT - 7TH STAGE DISK
LPT - SHAFT - FRONT COMPR DRIVE
LPT - THRUST BALANCE AIRSEAL
A330-200
PART NO.
SERIAL NO.
LIMIT
50B882-01
52B001
51A274
CBDUCM1776
CBDUCN0661
CLDLDC1537
15`000
15`000
15`000
9`587
9`587
9`587
54H405
54H767
58H236-01
50S106-01
51H572
54H792
CENCBE4258
CENCDL8184
CENCDM3917
CLDLDF3882
CENCCY6546
CENCDG6901
15`000
15`000
15`000
15`000
15`000
15`000
9`587
9`587
9`587
9`587
9`587
9`587
51L901
52L002
50L879
50L664
53L030
50L242
CKLBKE8188
CKLBKE8437
CKLBJS5815
CKLBKD8631
CKLBJ68380
CKLBJ59303
15`000
15`000
12`600
15`000
13`900
15`000
9`587
9`587
7`187
9`587
8`487
9`587
50N521
50N803
51N038
51N404
50N419
51N505
50N886
50N587
52A519-01
50N420
CLDLC19088
CLDLDF0486
CLDLC57162
CLDLDG2568
CLDLC89118
CLDLDH0002
CLDLDG0908
CLDLDB5370
CLDLDF9499
CLDLDE6029
15`000
15`000
15`000
15`000
15`000
15`000
15`000
15`000
15`000
15`000
9`587
9`587
9`587
9`587
9`587
9`587
9`587
9`587
9`587
9`587
MSN. TBA
REMAIN
Page 5 of 10
MAJOR AVIONICS EQUIPMENT
DESCRIPTION
ATA 22 – Automatic Flight Controls
Flight Management Guidance Computer
MCDU (Multifunction Control Display Unit)
MANUFACTURER
PART NUMBER
QTY
Thales Avionics
Thales Avionics
C13039CA01
C19266BA01
3
Thales Avionics
Rockwell Collins
Rockwell Collins
L3-COMM.
C12848CA01
822-1250-020
822-0330-020
2100-1020-02
3
3
2
1
Thales Avionics
S1821502-02
1
AIRBUS SAS
L3-COMM.
LA2E20202T40000
2100-4043-02
2
1
Litton Aero Products
L3-COMM.
Thales Avionics
ACSS
Rockwell Collins
Thales Optronique
Rockwell Collins
Rockwell Collins
Honeywell
465020-03030316
7517800-10005
C12404AB02
9000000-11414
822-1710-203
9599-607-19502
822-0297-020
822-0329-020
066-50014-0202
3
2
1
1
2
2
2
2
1
2
ATA 23 – Communications
RADIO Management Panel
VHF COMM. Transceivers (Incl. 8.33 & FM imm.)
HF COMM. Transceivers
SSCVR (Cockpit Voice Recorder) (120 min)
ATA 25 – Furnishings
ELT – Emergency Locator Transmitter Fixed
(121.5 / 243 / 406 MHz)
ATA 31 - Indication and Recording System
FWC (Flight Warning Computer)
SSFDR (Solid State Flight Data Recorder) (25 Hr&256 Words/sec)
ATA 34 – Navigation
ADIRU (Air Data Inertial Reference Unit)
ATC Transponder (Mode S – ELS & EHS Compliant)
ATC / TCAS Control Unit
T2CAS Computer (TAWS)
WR (Weather Radar) Transceiver
RA (Radio Altimeter) Transceiver
VOR (VHF Omnidirectional Range) (Incl. FM imm.)
DME (Distance Measurement Equipment) Interrogator
ADF Receiver
CAA REQUIREMENTS
EASA TCDS
EGPWS
Area Navigation
Elementary Surveillance (ELS)
Enhanced Surveillance (EHS)
Predictive Windshear
GPS Installed
SATCOM Installed
ELT 121.5 / 406 MHz
RVSM / FM Immunity & 8.33 KHz Chanel spacing
TCAS
Cockpit Door Surveillance System
A330-200
COMPLIANCE
EASA.A.004
Yes
Yes
Yes
Yes
Yes
Yes
Yes
Yes
Yes
Yes
Yes
MSN. TBA
NOTEs
BRNAV & PRNAV
Change 7.1
Page 6 of 10
INTERIOR CONFIGURATION
Galleys 5 (G1; G2; G5; G6; G7)
7 (1+4+2)
Lavatories
11
Attendant Seats
In Flight Entertainment Yes (Panasonic eX2 ISV)
Seats
Business Class
Economy Class
A330-200
Catering Standard
Cargo Configuration
Cockpit Configuration
CREW Rest
ATLAS
Semi-Auto CLS + Bulk
Standard (2+2)
2 Bunks (FWD)
Quantity
Manufacturer
Part Number
24
259
SICMA
WEBER AIRCRAFT
14052XX-XXX
862082-XXX
MSN. TBA
Page 7 of 10
CARGO CONFIGURATION
Cargo Configuration
Cargo Volume
Load Limitation
A330-200
CLS + Bulk
132.4 3Metres
37`578 Kg
Designee (Fire Detection/Protection) class
ULDs
Main Cargo Door(s)
MSN. TBA
C
26 x LD-3
106” x 66”
Page 8 of 10
PERFORMANCE
A330-200
MSN. TBA
Page 9 of 10
DELIVERY CONDITIONS
The Aircraft will be delivered at an EASA or FAA approved maintenance facility in a location to be advised.
Airframe:
In January 2017, the Aircraft shall be fresh out of a C-Check. At delivery, there shall
be no scheduled tasks accomplishment required before January 2019, 6,000 flight
hours and 1,500 cycles, whichever is the most limiting factor.
Engines:
Each Engine shall have no more than 5,000 flight hours and 1,500 cycles since last
performance restoration shop visit and sufficient EGT margin, with no defect
present, to allow at least 6,000 flight hours and 1,500 cycles until next expected
removal.
Each engine LLP shall have no less than 1,500 cycles life remaining until removal.
APU:
The APU shall have no more than 2,000 APU hours since last APU performance
restoration.
Landing Gear:
Landing gear shall not be due restoration before January 2019, or within 4,000
cycles, according to the manufacturer MPD.
Components:
Each component installed on the Aircraft shall be serviceable and be supported by
an EASA Form 1 or FAA Form 8130.
Each component installed on the Aircraft that has a flight hour, cycle or calendar
limit, shall not be due removal before April 2018, 6,000 flight hours, 1,500 cycles,
whichever is the most limiting factor.
Paint:
Aircraft shall be painted white.
Interior Configuration:
Aircraft shall be in 24 B/C 259 Y/C configuration.
Airworthiness Directives:
All airworthiness directives issued by EASA and / or the FAA which require
compliance before January 2018, 1,450 flight hours or 275 cycles, whichever is
most limiting, from delivery of the Aircraft shall have been complied with.
Aircraft Documents:
Aircraft shall have complete, up to date technical records, documentation and
manuals and shall include full back to birth traceability for life limited parts.
Certification:
Aircraft shall meet all the requirements for, and be eligible for an immediate
certificate of airworthiness issued by, and registration with, an EASA member state
and immediate operation in an EASA member state in full compliance with EASAOPS regulation.
Aircraft shall have either a certificate of airworthiness or an export certificate of
airworthiness.
Inspection:
A330-200
At Buyer’s cost, the Seller will perform a maximum power assurance run on each
Engine and at Bayer’s cost the Seller will perform an acceptance flight, of a
duration not more than 2 hours as necessary to demonstrate the satisfactory
operation of the Aircraft, with the Buyer or Buyer’s representative as observer.
Following such acceptance flight, a representative of the Buyer, at Buyer’s cost, will
perform a complete hot and cold section video borescope on each Engine. Buyer
shall not be obliged to accept delivery of the Aircraft unless any defects or
deficiencies found during such inspections have been rectified at Seller’s cost.
MSN. TBA
Page 10 of 10