1974 Aero Commander 500S
Description
The Aero Commander 500S was a twin-engine light aircraft produced by Aero Commander from 1974 to 1980. It was designed as a light business aircraft and is a stretched version of the earlier Aero Commander 500. It was powered by two Continental IO-520-C flat-six engines rated at 285hp each and could carry up to six passengers. The 500S had a maximum cruising speed of 200mph and a range of 1,400 miles. The 500S was replaced in 1980 by the improved Aero Commander 520.
Features
- Total Time: 6020
- Engines:
- Lycoming IO-720
- 1800 TBO
- LE TT: 3632.7 TSOH: 900.9
- RE TT: 3632.7 TSOH: 900.9
- Props:
- Hartzell props
- 567.3 Time Since New
- Avionics:
- Collins Proline
- Collins AP-106 autopilot with yaw damper and electric trim
- Collins FD-112V flight director
- (1) Garmin GNS-400 WAAS GPS with roll steer
- (2) Collins VHF-20 com
- (2) Collins VIR-30 nav
- (1) Collins DME-40
- (1) Collins Radio Altimeter
- (1) Collins PN-101 HSI
- (1) Collins RMI-332C-10
- Garmin 345 ADSB transponder
- Dual Collins audio panels with marker beacons
- PM6000 six place intercom
- Shadin fuel flow
- Alcor 8-probe engine analyzer
- Features:
- Long-range fuel – 223 gallons total
- Winglets
- Cool Air™ Air Conditioning
- Woodward prop sync
- Factory pilot front door
- Extended baggage
- Shoulder harnesses for Pilot, Copilot & rear bench
- Cleveland wheels & brakes
- Flap gap seals
- Useful load is appx 2,482
- Tinted cabin windows
- Plumbed for de-ice boots
- Plumbed for oxygen
- Alcohol windshield
- Wired for hot propellers
- Windshield wiper
- Cowling mounted recognition lights
- Hot weather and cold weather cowlings
- Frameless pilot & Copilot vent windows
- Vertically adjustable pilot seat
- Turbo Commander front seat rails for more leg room
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