1974 Twin Commander 690A
Description
The Twin Commander 690A is a six- to nine-seat twin turboprop light business aircraft manufactured by Twin Commander Aircraft and introduced in 1981. It is an updated version of the Twin Commander 680, with increased range and payload. It features a pressurized cabin and two turbo-charged Lycoming TIO-540-A2C engines. The 690A can fly up to a maximum range of 1,400 nautical miles and has a maximum cruise speed of 260 knots. It also features an advanced avionics suite and can be equipped with a variety of optional extras, such as an autopilot and satellite communications system.
Features
- Total Time: 9036
- Engine 1 Time: 3267 SMOH
- Engine 2 Time: 3267 SMOH
- ENGINE SPECS
- Engines: 3267/3267 Hours Since Major Overhaul
- 398/398 Hours Since Hot Section Inspection
- 5Y Landing Gear Inspection c/w and not due again until June 2024
- 5Y Propeller Overhaul c/w and not due again until November 2025
- SB208 Lower Spar Cap Inspection c/w and due again March 2024
- AVIONICS AND OPTIONS
- Garmin GNS-530W Com/Nav/GPS/Moving Map Unit
- Collins VHF-20 Com Transceiver
- Collins VIR-30A Nav Receiver
- Garmin GTX-330ES Transponders (ADS-B Out)
- Collins TDR-90 Transponder
- Collins AP-106 Autopilot
- Collins ADF-60
- RCA Primus 300SL Radar
- Collins DME
- Collins Radar Altimeter
- Dual Digital Clock
- Gear Mounted Taxi Lights
- Clamshell Doors Removed
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