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词条 Gulfstream American GA-7 Cougar
释义

  1. Development

  2. Design

  3. Variants

  4. Specifications (Gulfstream American GA-7 Cougar)

  5. See also

  6. References

  7. External links

name=GA-7 Cougar & TB 320 Tangaraimage=GulfstreamAmericanGA-7Cougar03.jpgcaption=

}}{{Infobox Aircraft Type

type= Personal and trainer aircraftmanufacturer=Gulfstream American Aviationdesigner=first flight= 20 December 1974[1]introduced=February 1978retired=status=primary user=more users=produced=1978-1979number built=115unit cost=developed from=variants with their own articles=
}}

The Gulfstream American GA-7 Cougar is an American all-metal, 4-seat, twin-engined light aircraft. The Cougar was a twin-engine development of the Gulfstream American AA-5B Tiger and traces its lineage to the AA-1 Yankee Clipper and the Bede BD-1.

Development

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 {{convert|160|hp|kW|0|abbr=on}} 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.[2]

Before production started the company was taken over on 1 September 1978 by American Jet Industries, who changed the company name to Gulfstream American.[1] Production of the Cougar ran for only two model years, 1978 and 1979, before production was halted. Just 115 Cougars were delivered.[4][3]

In 1995 the type certificate for the GA-7 was sold to SOCATA of France who intended to produce the aircraft as the TB 320 Tangara for the training market.[4] It was also to develop a variant with two Lycoming O-360-A1G6 engines of {{convert|180|hp|kW|0|abbr=on}} each and a re-designed cockpit, it was designated the TB 360. The first Tangara was a modified Cougar, had {{convert|160|hp|kW|0|abbr=on}} engines and first flew in mid-1996. The complete Tangara prototype was also a converted Cougar and had the {{convert|180|hp|kW|0|abbr=on}} 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.[5]

Design

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 wet wing.

The Cougar is powered by a pair of wing-mounted Lycoming O-320-D1D engines of {{convert|160|hp|kW|0|abbr=on}}. It carries four people at maximum cruise speed of {{convert|160|kn|km/h|0|abbr=on}} and a typical cruise speed of {{convert|140|kn|km/h|0|abbr=on}}. It was certified under US FAR Part 23 on 22 September 1977.[6]

Variants

GA7 Cougar

{{convert|160|hp|kW|0|abbr=on}} version designed by Grumman American and produced by Gulfstream American 1978-79. 115 built.[1]

TB 320 Tangara

Re-started production of the {{convert|160|hp|kW|0|abbr=on}} version by SOCATA, two modified Cougars were converted to Tangara prototypes 1996-97, production was never started.

TB 360 Tangara

Re-designed variant from SOCATA with {{convert|180|hp|kW|0|abbr=on}} O-360 engines, one prototype, a modified Cougar, was first flown in 1997, never entered production.

Specifications (Gulfstream American GA-7 Cougar)

{{Aircraft specs
|ref=FAA Type Certificate,[6] The Incomplete Guide to Airfoil Usage,[7] Pilot's Operating Handbook[8] and Pilot Friend[9]
|prime units?=kts


|genhide=
|crew=one
|capacity=three passengers
|length m=
|length ft=28
|length in=8
|length note=
|span m=
|span ft=36
|span in=10
|span note=
|height m=
|height ft=10
|height in=4
|height note=
|wing area sqm=
|wing area sqft=184
|wing area note=
|aspect ratio=
|airfoil=NACA 63A415
|empty weight kg=
|empty weight lb=2569
|empty weight note=
|gross weight kg=
|gross weight lb=3800
|gross weight note=
|max takeoff weight kg=
|max takeoff weight lb=
|max takeoff weight note=
|fuel capacity=
|more general=


|eng1 number=2
|eng1 name=Lycoming O-320-D1D
|eng1 type=four cylinder, horizontally-opposed aircraft engines
|eng1 kw=
|eng1 hp=160
|eng1 shp=
|eng1 kn=
|eng1 lbf=
|eng1 note=
|power original=
|thrust original=
|prop blade number=
|prop name=
|prop dia m=
|prop dia ft=
|prop dia in=
|prop note=


|perfhide=
|max speed kmh=
|max speed mph=
|max speed kts=168
|max speed note=
|max speed mach=
|cruise speed kmh=
|cruise speed mph=
|cruise speed kts=160
|cruise speed note=true airspeed
|stall speed kmh=
|stall speed mph=
|stall speed kts=63
|stall speed note=calibrated airspeed, flaps down
|never exceed speed kmh=
|never exceed speed mph=
|never exceed speed kts=188
|never exceed speed note=indicated airspeed
|minimum control speed kmh=
|minimum control speed mph=
|minimum control speed kts=61
|minimum control speed note= indicated airspeed
|range km=
|range miles=
|range nmi=1170
|range note= maximum economy with no reserves
|combat range km=
|endurance=
|ceiling m=
|ceiling ft=17400
|ceiling note=
|g limits=
|roll rate=
|glide ratio=
|climb rate ms=
|climb rate ftmin=1150
|climb rate note=
|time to altitude=
|sink rate ms=
|sink rate ftmin=
|sink rate note=
|lift to drag=
|wing loading kg/m2=
|wing loading lb/sqft=20.65
|wing loading note=
|disk loading kg/m2=
|disk loading lb/sqft=
|disk loading note=
|fuel consumption kg/km=
|fuel consumption lb/mi=
|power/mass=11.9 lb/hp (0.14 kg/kW)
|thrust/weight=
|more performance=
|avionics=
}}

See also

{{aircontent
|related=
  • Grumman American AA-5

|similar aircraft=
  • Beechcraft Duchess
  • Piper Seminole

|sequence=
}}

References

1. ^Simpson 1991, p. 25
2. ^Wood, Derek: Jane's World Aircraft Recognition Handbook, page 233. Jane's Publishing Company, 1982. {{ISBN|0-7106-0202-2}}
3. ^{{cite web|url=http://www.aopa.org/News-and-Video/All-News/1996/August/1/Return-of-the-Night-Fighter|title=Return of the Night Fighter?: From predator to exotic bird,|last=Marsh|first=Alton K|date=Aug 1, 1996|publisher=Aircraft Owners and Pilots Association}}
4. ^{{cite journal|url=http://www.flightglobal.com/pdfarchive/view/1995/1995%20-%201853.htm|title=Socata to manufacture Cougars|journal=Flight International|date=27 June 1995|page=24}}
5. ^{{cite journal|url=http://www.flightglobal.com/pdfarchive/view/2000/2000%20-%200022.htm|title=Tangara delayed 'indefinitely'|journal=Flight International|date=3 January 2000|last=Legros|first=Francois}}
6. ^{{cite web|url = http://www.airweb.faa.gov/Regulatory_and_Guidance_Library/rgMakeModel.nsf/0/B2CEC2BAFD278D88862572A00056C584?OpenDocument&Highlight=ga-7|title = TYPE CERTIFICATE DATA SHEET NO. A17SO|accessdate = 2008-07-02|last = Federal Aviation Administration|authorlink = |date=March 2007}}
7. ^{{cite web|url = http://www.ae.uiuc.edu/m-selig/ads/aircraft.html|title = The Incomplete Guide to Airfoil Usage|accessdate = 2009-12-30|last = Lednicer |first = David|authorlink = |date=October 2007}}
8. ^{{cite web|url = http://www.88thservices.com/pdf/cougarflightmanual.pdf|title = Pilot's Operating Handbook|accessdate = 2009-12-31|last = Gulfstream Aerospace|authorlink = |date=October 1978}}
9. ^{{cite web|url = http://www.pilotfriend.com/aircraft%20performance/Grumman/8.htm|title = Grumman GA-7 Cougar performance and specifications |accessdate = 2009-12-30|last = Pilot Friend|authorlink = |year = n.d.}}
  • {{cite book |last=Simpson |first= R.W.|authorlink= |coauthors= |title= Airlife's General Aviation|year=1991 |publisher= Airlife Publishing|location= England |isbn=1 85310 194 X|pages=}}

External links

  • {{commons category-inline|Gulfstream American GA-7 Cougar}}
{{Grumman aircraft}}{{American Aviation}}{{SOCATA aircraft}}

6 : Gulfstream American aircraft|SOCATA aircraft|United States civil utility aircraft 1970–1979|Low-wing aircraft|Aircraft first flown in 1974|Twin piston-engined tractor aircraft

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