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Gulfstream American GA-7 Cougar

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As a development of the company's single-engined designs, Grumman American developed a twin-engined version, designated the GA-7 which it named the Cougar, in keeping with the existing Lynx, Cheetah and Tiger names for aircraft in the company's line. The prototype Cougar with two 160 hp
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engines of 180 hp (134 kW) each and a re-designed cockpit, it was designated the TB 360. The first Tangara was a modified Cougar, had 160 hp (119 kW) engines and first flew in mid-1996. The complete Tangara prototype was also a converted Cougar and had the 180 hp
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Before production started the company was taken over on 1 September 1978 by American Jet Industries, who changed the company name to Gulfstream American. Production of the Cougar ran for only two model years, 1978 and 1979, before production was halted. Just 115 Cougars were delivered.
145:(119 kW) Lycoming O-320 engines first flew on the 29 December 1974. The prototype had a sliding canopy but this was soon changed to a starboard side door on the production aircraft. With other rework required the production prototype did not fly until 14 January 1977. 176:
The Cougar is a twin-engined low-wing cantilever monoplane using a honeycomb and bonded metal construction that is the hallmark of the line since the BD-1. The prototype's single spar wing was upgraded to a double-spar configuration and this allowed a
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engines of 160 hp (119 kW). It carries four people at maximum cruise speed of 160 kn (296 km/h) and a typical cruise speed of 140 kn (259 km/h). It was certified under US
165:(134 kW) engines. It first flew in February 1997. After delays in getting the type certified SOCATA announced at the end of 1999 that it had delayed indefinitely plans to certify the type. 481: 210:
Restarted production of the 160 hp (119 kW) version by SOCATA, two modified Cougars were converted to Tangara prototypes 1996-97, production was never started.
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Re-designed variant from SOCATA with 180 hp (134 kW) O-360 engines, one prototype, a modified Cougar, was first flown in 1997, never entered production.
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who intended to produce the aircraft as the TB 320 Tangara for the training market. It was also to develop a variant with two
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On 23 May 2019 the type certificate was transferred by SOCATA to the Cougar Aircraft Corporation in the United States.
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160 hp (119 kW) version designed by Grumman American and produced by Gulfstream American 1978-79. 115 built.
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FAA Type Certificate, The Incomplete Guide to Airfoil Usage, Pilot's Operating Handbook and Pilot Friend
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1,170 nmi (1,350 mi, 2,170 km) maximum economy with no reserves
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63 kn (72 mph, 117 km/h) calibrated airspeed, flaps down
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188 kn (216 mph, 348 km/h) indicated airspeed
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61 kn (70 mph, 113 km/h) indicated airspeed
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A GA-7 Cougar on the ramp at Les Cedres Quebec, May 2005
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160 kn (180 mph, 300 km/h) true airspeed
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In 1995 the type certificate for the GA-7 was sold to
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Aircraft of comparable role, configuration, and era
124:. The Cougar was a twin-engine development of the 307:aircraft engines, 160 hp (120 kW) each 2776: 221:Specifications (Gulfstream American GA-7 Cougar) 184:The Cougar is powered by a pair of wing-mounted 2554: 2672: 2658: 2540: 715: 455:, page 233. Jane's Publishing Company, 1982. 634: 628: 438: 436: 434: 2795:1970s United States civil utility aircraft 2665: 2651: 2547: 2533: 722: 708: 453:Jane's World Aircraft Recognition Handbook 376:20.65 lb/sq ft (100.8 kg/m) 322:168 kn (193 mph, 311 km/h) 579: 431: 103: 668: 582:"The Incomplete Guide to Airfoil Usage" 573: 482:"Type Certificate Data Sheet No. A17SO" 472: 470: 468: 2777: 540: 508:Aircraft Owners and Pilots Association 2646: 2528: 703: 501: 2810:Twin piston-engined tractor aircraft 541:Legros, Francois (January 3, 2000). 465: 260:36 ft 10 in (11.23 m) 445: 13: 600: 569:EASA.IM.A.381 dated 15 August 2019 266:10 ft 4 in (3.15 m) 254:28 ft 8 in (8.74 m) 14: 2821: 688: 502:Marsh, Alton K (August 1, 1996). 272:184 sq ft (17.1 m) 580:Lednicer, David (October 2007). 543:"Tangara delayed 'indefinitely'" 370:1,150 ft/min (5.8 m/s) 29: 24:GA-7 Cougar & TB 320 Tangara 673:. England: Airlife Publishing. 567:Cougar Aircraft Corporation GA7 562:European Aviation Safety Agency 522:"Socata to manufacture Cougars" 478:Federal Aviation Administration 126:Gulfstream American AA-5B Tiger 114:Gulfstream American GA-7 Cougar 555: 534: 514: 495: 139: 128:and traces its lineage to the 1: 425: 364:17,400 ft (5,300 m) 293:3,800 lb (1,724 kg) 287:2,569 lb (1,165 kg) 2805:Aircraft first flown in 1974 2785:Gulfstream American aircraft 612:"Pilot's Operating Handbook" 60:Gulfstream American Aviation 7: 2743:TBM 700/850/900/910/930/940 389: 195: 10: 2826: 695:Pilot's Operating Handbook 671:Airlife's General Aviation 2751: 2685: 2599: 2563: 2501: 2275: 2182: 2141: 2070: 2029: 1988: 1967: 1851: 1844: 742: 171: 94: 86: 78: 73: 65: 53: 42: 37: 28: 23: 385:11.9 lb/hp (7.19 kg/kW) 233:General characteristics 120:, 4-seat, twin-engined 16:American light aircraft 669:Simpson, R.W. (1991). 192:on 22 September 1977. 109: 635:Pilot Friend (n.d.). 401:Grumman American AA-5 348:Minimum control speed 107: 656:: CS1 maint: year ( 608:Gulfstream Aerospace 548:Flight International 530:: 24. June 27, 1995. 527:Flight International 305:horizontally-opposed 2617:Gulfstream American 2190:Apollo Lunar Module 442:Simpson 1991, p. 25 395:Related development 162:Lycoming O-360-A1G6 130:AA-1 Yankee Clipper 38:General information 2071:Utility/Transports 413:Beechcraft Duchess 339:Never exceed speed 301:Lycoming O-320-D1D 186:Lycoming O-320-D1D 110: 2800:Low-wing aircraft 2772: 2771: 2640: 2639: 2607:American Aviation 2556:American Aviation 2522: 2521: 2271: 2270: 565:Type Certificate 102: 101: 98:December 20, 1974 87:Introduction date 2817: 2667: 2660: 2653: 2644: 2643: 2622:American General 2612:Grumman American 2549: 2542: 2535: 2526: 2525: 1849: 1848: 735:Northrop Grumman 724: 717: 710: 701: 700: 684: 662: 661: 655: 647: 645: 643: 632: 626: 625: 623: 621: 616: 610:(October 1978). 604: 598: 597: 595: 593: 584:. 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Index


trainer aircraft
Manufacturer
Gulfstream American Aviation

all-metal
light aircraft
Gulfstream American AA-5B Tiger
AA-1 Yankee Clipper
Bede BD-1
SOCATA
France
Lycoming O-360-A1G6
wet wing
Lycoming O-320-D1D
FAR Part 23
Airfoil
Lycoming O-320-D1D
horizontally-opposed
Never exceed speed
Minimum control speed
Power/mass
Grumman American AA-5
Beechcraft Duchess
Piper Seminole



ISBN
0-7106-0202-2

Text is available under the Creative Commons Attribution-ShareAlike License. Additional terms may apply.

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