1972 Aero Commander 500A

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The Aero Commander 500A is a twin-engine executive aircraft developed by Aero Design and Engineering Company in 1960. It is a high-performance, light and reliable aircraft capable of carrying up to seven passengers. It is powered by two Lycoming IO-540 engines, which provide a maximum speed of 250 knots. The aircraft has a wingspan of 38 feet, a length of 34 feet and a height of 10 feet. It has a range of 1,500 nautical miles and can fly up to 13,500 feet. The 500A has a luxurious interior, with comfortable leather seats and a full galley. It is an ideal aircraft for corporate, business and charter flights.


  • Total Time: 8182
  • Engines:
  • Total Time Engines: 1327 Hrs. SMOH-2014 (Merlyn Turbocharger System)
  • Engine Model: IO-550-E MC(1900 TBO) - 320 BHP/Continuous
  • Props:
  • Total Time Props: 409 Hrs. TSOH (2/19)
  • Prop Model: Hartzell - PHC-C3YF-2UF
  • Avionics/Radios:
  • Audio Panel: NAT AMS 44T (Split Pilot/Copilot)
  • GPS/Nav/Comm 1: Garmin GNS 530
  • Nav/Comm 2: King KX-155 Selector Switch installed
  • Aux Com 2: King KY-196A
  • GPS: Portable Garmin 796
  • Auto Pilot: Century III
  • Transponder: GTX 335G - ADSB out
  • Engine Monitor: JPI EDM 760
  • Traffic: L-3 Skywatch 899 Traffic Avoidance System
  • AFF: Skyconnect Automatic Flight Following
  • FM1 NAT 136D
  • FM2: NAT 136D
  • AUX FM: Wired for handheld hookup FM/3rd NAT 136D

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