N900PJ - 1969 COMMANDER 1121B
Aircraft Summary
General
Year
1969
Manufacturer
COMMANDER
Model
1121B
Serial Number
135
Registration #
N900PJ
Condition
Used
FlightRules
IFR
Description
Thrust Reversers, Ground Air Conditioning, GPS, Collins AP-105 A/P & FDS-109 F/D, Dual Navs, Coms, DMEs, ADFs, Xpers, Gross Weight Increase, More.
Airframe
Total Time
7330.0
Airframe Notes
• Registration: N900PJ
• Serial Number: 135
• Airframe: 7,330 Hours Total Time Since New
• • 6,209 Landings
• Price: $95,000 USD, Will Trade for Cessna Citation 500, 501, Citation I SP
• Location: Byron Airport, Byron, California (C83)
Engine Program
Engine Program Notes
• Engines: Manufacturer: General Electric
• Model Number: CJ610-5 with Thrust Reversers
• Left
• Serial Number: 249-043A
• Time Since Overhaul: 1,274 Hours
• Cycles Since Overhaul: 1,230
• TBO Interval: 3,000 Hours
• Total Time Since New: 7,312 Hours
• Cycles Since New: 6,299
• Overhaul Date: 11/14/1978
• Overhauled By: General Electric Co.
• HSI Interval: 1,000 Hours
• Time Since HSI: 379 Hours
• HSI Date: 05/02/1996
• Cycles Since HSI: 310
• Right
• Serial Number: 249-077A
• Time Since Overhaul: 1,274 Hours
• Cycles Since Overhaul: 1,230
• TBO Interval: 3,000 Hours
• Total Time Since New: 7,312 Hours
• Cycles Since New: 6,299
• Overhaul Date: 11/14/1978
• Overhauled By: General Electric Co.
• HSI Interval: 1,000 Hours
• Time Since HSI: 379 Hours
• HSI Date: 05/02/1996
• Cycles Since HSI: 310
Engine 1
Engine 1 Time
1274
Engine 1 Time Since
SOH
Engine 1 Time Since HSI/MPI/Mid-Life
379
Engine 2
Engine 2 Time
1274
Engine 2 Time Since
SOH
Engine 2 Time Since HSI/MPI/Mid-Life
379
Avionics
Avionics/Radios
• COM: Dual Collins KTR-908 Com Units
• NAV: Dual Collins 51RV-1A Nav Units
• GPS: Trimble Navigation TNL 2000A GPS Navigation System
• Autopilot: Collins AP-105 Autopilot
• FDS: Collins FDS-109 Flight Director System with Dual Indicators
• Gyros: Dual Collins 332-E-2 Directional Gyros
• Vertical Gyros: Dual Collins 392-D-11 Vertical Gyros
• ADF: Dual Collins 514-4-A ADFs
• DME: Dual Bendix/King KN63DMEs
• Radar: Bendix RT-131-A Weather Radar System
• Transponder #1: Collins TDR-90 Transponder
• Transponder #2: Collins TDR-92 Transponder
• Altimeter: IDC Encoding Altimeter
• IVSI: Dual Instantaneous Vertical Speed Indicators
• ELT: Narco 910 ELT
• Clocks: Dual Electric Clocks
• Copilot Instruments
Additional Equipment
Additional Equipment
• Brake Assemblies Overhauled 12/03/2005
• Aircraft Fuel Leak Checked and Sealed 11/23/2004
• Right Engine Hydraulic Pump Overhauled 05/06/2004
Exterior
Year Painted
2010
Exterior Notes
• Exterior Refinished and Touched Up March 2010
• Overall White with Jet-Glo Polyurethane Jet Black and Red Accents and Trim
• Condition 7 (National Aircraft Appraisers Association Exterior Rating Guide)
Interior
Year Interior
2010
Number of Seats
9
Interior Notes
• Interior Refurbished March 2010
• Nine Place Executive Fireblocked Interior (Two Crew and Seven Passenger)
• Forward Three Place Divan
• Aft Four Place Club Seating
• Medium Neutral Leather Sidewalls
• Light Neutral Leather Panels
• Tigermoth Bulkhead Panels
• Medium Parchment Leather Seats, Two Individual Seats Fully Configurable
• Midnight and Sand Floor Carpeting
• High Gloss Dark Wood Cabinetry
• Dual Dark Wood Executive Writing Tables
• Belted Lavatory Seat
• Spacious Forward Closet/Baggage Compartment Area with Hanger Rod
• Condition 8 (National Aircraft Appraisers Association Interior Rating Guide)
Modifications/Conversions
Modifications/Conversions
• Ground Air Conditioning STC SA1513SW
• Thrust Reverser System STC SA1879SW (Includes Drag Chute Removal)
• Thrust Reverser Pressure Gauge STC SA2716SW
• Taxi Lights STC SA2695SW
• Manual Ignition Switches STC SA4045SW
• Microcom Battery Temperature Monitor and Overtemp Warning System Installed 04/03/1974 per STC SA1551SW
• General Electric RB27 Batteries STC SA1274SW
• Gross Weight Increase to 18,500 Lbs. with Main Landing Gear Anti-Skid System STC SA1345SW
Inspection Status
Inspection Status
• Inspections: Airframe A Check Performed at 7,248 Hours TTAF
• • Airframe B Check Performed at 6,797 Hours TTAF
• • Airframe C Check Performed at 7,099 Hours TTAF
• • IFR Recertification Due June 2015
• Damage: No Known Damage History
• Records: Complete and Continuous Logbooks, Complete Records
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