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Civil Aircraft Model Number AERO COMMANDER 500

General Information of AERO COMMANDER 500
First Flight : 23 April 1948 (Model L3085)

Introduction : 19268

Manufacturer : Aero Design and Engineering Company/Aero Commander

Produced : 1951-1986

Role : Utility and transport aircraft

General characteristics of AERO COMMANDER 500
Aspect Ratio : 9.45:1

Airfoil : NACA 23012 modified

Capacity : four passengers

Crew : Two

Empty Weight : 4,635 lb (2,102 kg)

Height : 14 ft 6 in (4.42 m)

Length : 36 ft 9¾ in (11.22 m)

Max Takeoff Weight : 6,750 lb (3,062 kg)

Powerplant : 2 × Lycoming IO-540-E1B5 air-cooled flat-six piston engines, 290 hp (216 kW) each

Wing Area : 255 ft² (23.69 m²)

Wingspan : 49 ft 0½ in (14.95 m)

Performance of AERO COMMANDER 500
Cruise Speed : 203 mph (176 knots, 326 km/h) at 9,000 ft (2,750 m), 75% power, TAS

Maximum Speed : 215 mph (187 knots, 346 km/h) at sea level (TAS)

Range : 1,078 miles (936nmi, 1,735 km)

Rate Of Climb : 1,340 ft/min (6.8 m/s)

Service Ceiling : 19,400 ft (5,913 m)

Stall Speed : 68 mph (59 knots, 109km/h) flaps and landing gear down,CAS

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