AIRCRAFT TECHNICAL SPECIFICATION SHEET
YR-MDL (MSN: 48079)
-Specification IAW ATA 100 Chapters-
Registration:
Date of Report:
YR-MDL
Serial Number:
48079
03 Dec 2008
Model/Series:
MD-82
Chapter 1. GENERAL DESCRIPTION
Model Designation:
Year of Manufacture:
Engine Model:
Noise Certification Status (EPNdb) (Stage 3)
Cabin Crew Accommodation:
Passenger Accommodation:
Approach Category:
Line Number:
Country of Registration:
Registration Authority:
Galley Configuration
Cargo configuration
Current Operator:
MD-82
Nov. 13, 1981
PW JT8D-217A
T T/O: 90.6 Sideline: 95.4 Appr: 93.1
1 CAPT/1 F.O.
160Y
CAT II/III
1016
ROMANIA
ROMANIAN CAA
2 FWD, 4 AFT
FWD-MID-AFT
JETRAN AIR
Chapter 3. DESIGN WEIGHTS & MAIN DIMENSION
Maximum Gross Taxi Weight:
Maximum Take-off Weight:
Maximum Landing Weight:
Maximum Zero Fuel Weight:
Operating Empty Weight:
Fuel Capacity: (volume)
Wing Span
Length Overall
Height Overall
150.500lbs
149.500lbs
130.000lbs
120.000lbs
83.700lbs
5.836 US Gallons(22.092 lt.)
107.8 ft(32.8m)
147.8 ft(45.05m)
29.6 ft(9.02m) @ top VS
AIRCRAFT TECHNICAL SPECIFICATION SHEET
YR-MDL (MSN: 48079)
Chapter 5. MAINTENANCE SCHEDULE AND STATUS
Date
03 Dec 2008
Total Hours
79117:56
Total Cycles
44657
INSPECTION FREQUENCY: MS in accordance with manufacturer OAMP ME-0098 MSG 3
“A” Check - at 450 flight hours
“C” Check - at 3500 flight hours or 18 months, whichever comes first
Last Accomplishment
Next Accomplishment
Maintenance
Program
A Check
A1
Date
Hours
Cycles
Date
Hours
Cycles
08 Aug 2008
78775
44405
79225
N/A
C Check
06 Mar 2007
76576
42916
N/A
06 Nov
2008
Remaining
(HOURS)
107
80076
N/A
1058
C2
Chapter 22. AUTOMATIC FLIGHT CONTROLS
Item
Logic Computer
Longitudinal Computer
Lateral Computer
Pitch Trim Computer
Pitch Compen. Computer
AFCS Test Computer
Yaw Stability Computer
Thrust Control Computer
Manufacturer
Honeywell
Honeywell
Honeywell
Honeywell
Honeywell
N/A
Honeywell
Honeywell
Remarks
DFGC
DFGC
DFGC
DFGC
MachTrim
N/A
Yaw Damper
Thrust Rate Comp
Part No
4034241-974
4034241-974
4034241-974
4034241-974
2587284-962
N/A
2589445-933
LG80E1
Qty
2
2
2
2
1
N/A
1
CHAPTER 23. COMMUNICATIONS
Item
Transceiver – VHF
Pax. Address Ampf.
VHF Aerial
Cockpit Voice Recorder
VHF Control Panel
HF SYSTEM
Manufacturer
COLLINS
COLLINS
SENSOR SYSTEM
SUNDSTRAND
GABLES
COLLINS
Remarks
Part No
622-1181-001
622-4487-001
S65-8262DC10A
980-6020-001
G6584
622-3371-001
Qty
2
1
2
1
2
1
AIRCRAFT TECHNICAL SPECIFICATION SHEET
YR-MDL (MSN: 48079)
CHAPTER 24. ELECTRIC POWER
Item
Generator Control Unit
Constant Speed Drive
Battery
Manufacturer
SUNDSTRAND
SUNDSTRAND
MARATHON
Remarks
Part No
976J254-4
696233B
30475-002
Qty
3
2
2
Chapter 25. EQUIPMENT AND FURNISHING
Item
First Class Seats
Tourist Class Seats
Tourist Class Seats
Oven
Galley G1
Galley G2
Galley G4
Galley G4B
AFT LAV LH
AFT LAV RH
FWD LAV RH
BALLISTIC DOOR
Manufacturer
Remarks
DOUBLE
TRIPLE
DOUBLE
Part No
Qty
6
28
23
1
1
1
1
1
1
1
1
1
Chapter 27. FLIGHT CONTROLS
Item
Manufacturer
Slat Control Unit
SUNDSTRAND
Slat/Flap Instrumentation Unit
ELDEC
Flap Instrumentation Unit
Ground Spoiler Control Box
HYDRO AIRE
Remarks
Stall warning
computer
Electronic Proximity
box
Pos. Ind. transmitter
Part No
Qty
965-0449-002
2
8336-5
1
ST12BH
42-091-3
1
Chapter 28. FUEL
Item
Fuel Qty Ind. Amplif.
Fuel Level Indicator
APU Fuel Booster P.
Manufacturer
GULL INSTRUMENTS
GULL INSTRUMENTS
LUCAS
Remarks
Part No
367-000-001
372-001-001
RR559A
Qty
1
1
1
AIRCRAFT TECHNICAL SPECIFICATION SHEET
YR-MDL (MSN: 48079)
Chapter 29. HYDRAULICS
Item
Aux Pump
Power Transfer Unit
Manufacturer
LUCAS WESTERN
AERO HYDRAULIC
Remarks
Part No
861555
4100310-6
Qty
1
1
Remarks
Part No
2222601-6
980-4120-DXUN
Qty
1
1
Remarks
Part No
5007887-2
5007898-3
9550267-X
Qty
4
4
2
Chapter 31. INDICATION AND RECORDING SYSTEMS
Item
FDAU
S/State Flt. Data Rec.
Manufacturer
AER TRANSPORT SYSTEM
SUNDSTRAND
Chapter 32. LANDING GEAR
Item
Brakes
Wheels (Main)
Wheels (Nose)
Manufacturer
ABS
ABS
ABS
Landing Gear Data
P/N
S/N
Left Main Gear
5935354-503
S0075
Right Main Gear
5935355-507
R8990
Nose Gear
5910448-537
R8600
NOTE: MRB OH LIMITS-20000cy/10Y whichever occurs first
TSO/
CSO
7650:00
5167
9908:00
9017
8964:00
5798
OH DATE
30 Oct 2003
11 Sep 1999
29 Sep 2003
AIRCRAFT TECHNICAL SPECIFICATION SHEET
YR-MDL (MSN: 48079)
Chapter 34. NAVIGATION
Item
Receiver – ADF
Tx – Weather Radar
Standby Compass
Altimeter
Standby Altimeter
Radio Altimeter Indic.
Tx/Rx – Radio Altimeter
MHRS Coupler
INS Inertial Navigation Unit
INS Mode Selector
Vertical Speed Indicator
Horizontal Situation Indicator
ATT/Director Indic.
Standby Horizontal Indic.
Transponder – ATC
Mach Airspeed Indicator
Standby Airspeed Indicator
Interrog. (Tx/Rx)– DME
Rx – Marker Beacon
Rx – VOR/ILS
GPS
GPWS/TAWS
ADC – Air Data Comp.
Accelerometer
TCAS Computer
WINDSHEAR SYSTEM
Manufacturer
COLLINS
HONEYWELL
SFENA
SPERRY
SPERRY
COLLINS
COLLINS
N/A
N/A
N/A
HONEYWELL
Honeywell
Honeywell
SFENA
COLLINS
HONEYWELL
SPERRY
COLLINS
COLLINS
COLLINS
TRIMBLE
ACSS
HONEYWELL
HONEYWELL
ACSS
HONEYWELL
Remarks
Part No
777-1492-004
20412170413
C4E
4005123-907
WL101AMS1
522-4825-004
622-3890-015
N/A
N/A
N/A
4067241-860
4038930-901
4019700-903
706-7V92
622-7878-201
4057800-906
WL101AMS5
622-2921-001
522-2996-001
822-0760-001
TNL2101
9000000-2002
HG280D80
40342238-901
9000000-2002
4059845-911
Qty
2
1
1
2
1
2
2
2
2
2
1
2
2
1
2
1
2
1
1
2
2
1
1
AIRCRAFT TECHNICAL SPECIFICATION SHEET
YR-MDL (MSN: 48079)
Chapter 49. AIRBORNE AUXILIARY POWER (APU)
Item
Model
Manufacturer
Part Number
Serial Number
APU
GTCP85-98
ALLIED SIGNAL
3800368-1
P-1076C
Chapter 72. ENGINES
Item
Serial Number
Manufacturer
Model
Thrust Rating*
Install Date
Time Since New
Cycle Since New
T.S.L.S.V.
C.S.L.S.V.
First Limiter Disc
First Limiter Cycle
Last Shop Visit Center
Engine 1
708419
PWA
JT8D-217A
20000lbs*
16 Sep 2004
64505
36521
5123
3502
HPT Shaft
1922
ITR MEXICO
Engine 2
708420
PWA
JT8D-217A
20000lbs*
21 Jul 2008
60087
33725
467
353
LPT Shaft
5273
BONUS AEROSPACE
(*)NOTE
A thrust setting limited to 19,250 lbs. (JT8D-209), 20,850 lbs. (JT8D-217, -217A, -217C) and 21,700
lbs. (JT8D-219) static thrust at sea level, flat rated to 84°F ambient temperature has been
established as maximum takeoff thrust rating. A thrust setting limited to 18,500 lbs. (JT8D-209),
20,000 lbs. (JT8D-217) static thrust at seal level, flat rated to 77°F ambient temperature and 20,000
lbs. (JT8D-217A-217C) and 21,000 lbs. (JT8D-219) static thrust at sea level, flat rated to 84°F
ambient temperature has been established as normal takeoff thrust rating for normal takeoff
operation.
Appendix
PERFORMED C CHECK SUMMARY
Maintenance Type
C1
Last O/H Center
ROMAERO S.A.
Date
06 Mar 2007
Hours
76576
Cycles
42916