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 |