For Sale: 1961 CESSNA 182D

Useful Load: 796 lbs

• Continental O-470-L S/N 81546-0-L-4 (1500 TBO)
• Overhauled 1/10/2013 by B&G Flying Service, Inc.
• 524 SMOH

• Propeller: Hartzell 3-Bladed Constant Speed Propeller PHC-G3YF-1RF S/N NT221B (2400 TBO)
• Installed New 11/18/15. Overhauled and installed 12/2/24 with 322 total time
• SMOH: 17.1

• Interior refurbished 5/19/16. Burgundy Leather seats and sidewalls with Brown Carpeting and Cream Headliner.

• Painted January 2016 by New Beginnings Aircraft. Base Matterhorn White Jetglo, Light Burgundy Metallic, Charcoal Grey Metallic.

• Dual Bendix/King KX-155 Nav/Com
• PS Engineering PMA 8000B Audio Panel
• Garmin GTX 335 ADS-B Transponder
• Bendix/King KR-86 ADF
• Bendix/King KI-208 VOR/LOC Indicator
• Kenwood TK-7180H VHF FM Transceiver

• Wing Tanks 65 Gallon Total Capacity
• Aux Tank 18 Gallon Capacity

All logs since new. Available upon request. 

01/18/26 – 100 Hour/Annual accomplished
03/22/25 – Transponder check accomplished.
Aircraft was maintained under Part 135 operations until recently.

Damage History: 5/6/2001 - Mishap pilot was flying fire line between ridges on Chandler Mountain. The aircraft had been operated approximately 90 minutes before the incident. The pilot stated that the engine began to run rough and then quit. Several attempts were made to restart the engine. The pilot was unable to restart and landed the aircraft in a field. Minor damage to the left wing tip and tail drag strip occurred when the pilot hard landed the aircraft. Pilot stated that he attempted to restart the engine after emergency landing, the engine would not start. The fuel tanks were left 3/4 full, right 1/4 full and the auxiliary tank was 3/4 full. At the time of the incident fuel transfer was in-progress, from auxiliary to right main, and the fuel selector valve was selected to left tank. The fuel tanks, sumps, and filters were inspected for contamination, small traces of fuel bladder shavings in the filter screen. Trace amounts in carburetor filter. Engine was run and had excessive vibration 800-1200 RPM. The engine had been operated for approximately 20 hours since complete overhaul. Owner is shipping engine to repair station for warranty exchange. The FAA will follow-up with repair station to explore the possibility of external or internal damage.

• Horton Stol Kit 
• 3 Blade Prop
• Knisely Exhaust System STC SA01293LA
• Aero Fabricators Shoulder Harness System STC SA1474GL
• Javelin Aircraft Company, Inc. Auxiliary Fuel Tank
• Precise Flight Standby Vacuum System
• Cleveland Wheel and Brakes STC SA13GL    
• Rosen Sun Visors