Gulfstream American GA-7 Cougar
Touring Aircraft
The Gulfstream American GA-7 Cougar is a twin-engined four-seat light touring aircraft produced by the US-American manufacturer Gulfstream American.
The GA-7 Cougar is a twin-engined development of the Gulfstream American
AA-5B Tiger.
Propulsion | 1 Piston Engine |
Engine Model | Lycoming O-320-D1D |
Engine Power | 119 kW | 160 hp |
max. Cruise Speed | 300 km/h | 162 kts 186 mph |
max. Speed (vne) | 354 km/h | 191 kts 220 mph |
Service Ceiling | 5.304 m | 17.400 ft |
Range | 1.556 km | 840 NM 967 mi. |
Empty Weight | 1.165 kg | 2.569 lbs |
max. Takeoff Weight | 1.724 kg | 3.800 lbs |
Wing Span | 11,20 m | 36 ft 9 in |
Wing Area | 17,1 m² | 184 ft² |
Length | 9,02 m | 29 ft 7 in |
Height | 3,15 m | 10 ft 4 in |
First Flight | 20.12.1974 |
Production Status | out of production |
Total Production | 115 |
Developed from | American AA-5 |
ICAO Code | GA7 |
FAA TCDS | A17SO |
Data for (Version) | Gulfstream American GA-7 Cougar |
Variants | SOCATA TB 360 Tangara |