The Gulfstream American GA-7 Cougar is a twin-engined four-seat light touring aircraft produced by the US-American manufacturer Gulfstream American.
| Crew | 1 | |
| Passengers | 3 | |
| Propulsion | 1 Piston Engine | |
| Engine Model | Lycoming O-320-D1D | |
| Engine Power | 119 kW | 160 hp |
| max. Cruise Speed | 300 km/h | 162 kts |
| max. Speed (vne) | 354 km/h | 191 kts |
| Service Ceiling | 5.304 m | 17.400 ft |
| Range | 1.556 km | 840 NM |
| Empty Weight | 1.165 kg | 2.569 lbs |
| max. Takeoff Weight | 1.724 kg | 3.800 lbs |
| Wing Span | 11,20 m | 36,7 ft |
| Wing Area | 17,1 m² | 184 ft² |
| Length | 9,02 m | 29,6 ft |
| Height | 3,15 m | 10,3 ft |
| 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 |
Remarks
The GA-7 Cougar is a twin-engined development of the Gulfstream American AA-5B Tiger.
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