2001 BOEING 737 700
Aircraft Summary
General
Year
2001
Manufacturer
BOEING
Model
737-700
Condition
Used
Description
CONTACT: Aviation Management Group (AMG)
www.amgaviation.com
Jack Hareland
(520) 977-5694
[email protected]
Jim Weiland
(615) 476-8877
[email protected]
Gary Laguardia
(786) 423-6424
[email protected]
- ETOPS: 180 minutes
- Airstair: Foward
- WEIGHTS: Operational -
Max Taxi Weight: 146,500 lbs - 66,451 Kg
Max Take Off Weight: 146,000 lbs - 66,224 Kg
Max Landing Weight: 128,000 lbs - 58,059 Kg
Max Zero Fuel Weight: 120,500 lbs - 54,657 Kg
Operating Empty Weight: 82,966 lbs - 37,633 Kg
- Fuel Capacity -
Usable Fuel: 45,972 lbs - 20,896 Kg
Tank Positions: LH, RH Wing and Center Body
- Landing Gears -
All three gears have 4 years/8200 cycles remaining to overhaul. 9800 total cycles since new, 16,800/16,800 hrs SNEW-Engines, Honeywell Avionics. 136 Seats (tourist class)
Airframe
Total Time
16700.0
Airframe Notes
- 16,700 Total Hours since new
- 9,800 Total Cycles since new
Engine Program
Engine Program Notes
Type: CFM56-7B24
Engine #1:
- 16,800 Hours Since New
- 9,700 Cycles Since New
- 8,100 Cycles to First Limiter
Engine #2:
- 16,800 Hours Since New
- 9,700 Cycles Since New
- 7,700 Cycles to First Limiter
Avionics
Avionics/Radios
- (2) Honeywell Computer Flight Control
- Smiths Aerospace Computer Auto Throttle
- Honeywell Transceiver, HF COMM
- (2) Honeywell RTA-44D Transceiver, VHF COMM
- Coltech SELCAL Decoder
- Rockwell Collins Amplifier, Passenger Address
- Matsushita Reproducer, Tape Pram
- Artex AF Emergency Locator Transmitter
- Honeywell Cockpit Voice Recorder
- Honeywell Digital Flight Data Recorder
- Honeywell DFDAU Acquisition Unit
- Honeywell CDS-Display Unit (PFD/ND/Engine)
- Smiths Aerospace Standby Altimeter Indicator
- (2) Honeywell Air Data Inertial Reference Unit (ADIRU)
- Rockwell Collins RMI Indicator
- Ametek Standby Compass Indicator
- BF Goodrich Standby Altitude Indicator
- (2) Honeywell RMA-55B Multi-Mode Receiver
- (2) Honeywell RVA-36B Marker Beacon/VOR Receiver
- (2) Honeywell ALA-52B Long Range Radio Altimeter
- Honeywell WXR Tranceiver
- Honeywell TPA-81A TCAS (Change 7.0)
- Honeywell MKV EGPWS
- (2) Honeywell ATC Mode S Transponder
- (2) Honeywell DMA-37B DME
- Honeywell DFA-75B ADF
- (2) Honeywell Display Electronic Unit (DEU)
- (2) Smiths Aerospace 2584A Control Display Unit (CDU)
- Smiths Aerospace 2904A4 Flight Management Computer
Interior
Interior Notes
- 136 Seats (all tourist class)
Inspection Status
Inspection Status
Current Program: Phase 36
500 Hrs
- Last Performed: May 27th, 2007
- Hours Since Check: 12
- Cycles Since Check: 14
- Next Check Due: Phase 37
6000 hrs
- Last Performed: Nov 21st, 2006
- Hours Since Check: 185
- Cycles Since Check: 120
- Next Check Due: Phase 48/Nov 2009
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