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- Helio_Stallion abstract "The Helio HST-550 Stallion was an STOL utility aircraft developed in the United States in 1963. The prototype flew in July 1964. Initially conceived as a turboprop-powered variant of the Helio Courier, it eventually emerged as a completely new design of the same general configuration and much of its design was initiated from components used in the Helio H-500 Twin. It was a much larger aircraft than the Courier, and Helio soon discovered that it was too expensive for the market.The USAF however, emerged as a buyer for the design, purchasing the aircraft for the Credible Chase programme as the AU-24A. This was the gunship version of the Stallion, with a PT6A-27 680 shp (510 kW) turboprop, equipped with a General Electric XM-197 three-barrel 20 mm Gatling gun mounted in the left cargo door. It also had five underwing and fuselage hardpoints. Of the 18 aircraft purchased, fourteen or fifteen were eventually sold to the Cambodian (Khmer) Air Force.".
- Helio_Stallion manufacturer Helio_Aircraft_Company.
- Helio_Stallion numberBuilt "20".
- Helio_Stallion origin United_States.
- Helio_Stallion wikiPageID "17103161".
- Helio_Stallion wikiPageRevisionID "556008316".
- Helio_Stallion capacity "9".
- Helio_Stallion ceilingFt "25000".
- Helio_Stallion ceilingM "7620".
- Helio_Stallion climbRateFtmin "2200".
- Helio_Stallion climbRateMs "11".
- Helio_Stallion crew "One pilot".
- Helio_Stallion cruiseSpeedKmh "257".
- Helio_Stallion cruiseSpeedMph "160".
- Helio_Stallion emptyWeightKg "1287".
- Helio_Stallion emptyWeightLb "2860".
- Helio_Stallion eng1Hp "680".
- Helio_Stallion eng1Kw "507".
- Helio_Stallion eng1Number "1".
- Helio_Stallion eng1Type "Pratt & Whitney Canada PT6A-27".
- Helio_Stallion firstFlight "1964-06-05".
- Helio_Stallion grossWeightKg "2313".
- Helio_Stallion grossWeightLb "5100".
- Helio_Stallion hasPhotoCollection Helio_Stallion.
- Helio_Stallion heightFt "9".
- Helio_Stallion heightIn "3".
- Helio_Stallion heightM "2.81".
- Helio_Stallion lengthFt "39".
- Helio_Stallion lengthIn "7".
- Helio_Stallion lengthM "12.07".
- Helio_Stallion manufacturer Helio_Aircraft_Company.
- Helio_Stallion maxSpeedKmh "348".
- Helio_Stallion maxSpeedMph "216".
- Helio_Stallion metOrEng%3F_ "eng".
- Helio_Stallion nationalOrigin United_States.
- Helio_Stallion numberBuilt "20".
- Helio_Stallion primaryUser Central_Intelligence_Agency.
- Helio_Stallion primaryUser United_States_Air_Force.
- Helio_Stallion rangeKm "1031".
- Helio_Stallion rangeMiles "641".
- Helio_Stallion ref "Jane's All The World's Aircraft 1976-77".
- Helio_Stallion spanFt "41".
- Helio_Stallion spanIn "0".
- Helio_Stallion spanM "12.5".
- Helio_Stallion type "Civil utility aircraft".
- Helio_Stallion wingAreaSqft "242".
- Helio_Stallion wingAreaSqm "22.48".
- Helio_Stallion subject Category:Helio_aircraft.
- Helio_Stallion subject Category:Single-engine_aircraft.
- Helio_Stallion subject Category:United_States_attack_aircraft_1960–1969.
- Helio_Stallion subject Category:United_States_civil_utility_aircraft_1960–1969.
- Helio_Stallion type Aircraft.
- Helio_Stallion type MeanOfTransportation.
- Helio_Stallion type Product.
- Helio_Stallion type Model_airplane.
- Helio_Stallion type DesignedArtifact.
- Helio_Stallion comment "The Helio HST-550 Stallion was an STOL utility aircraft developed in the United States in 1963. The prototype flew in July 1964. Initially conceived as a turboprop-powered variant of the Helio Courier, it eventually emerged as a completely new design of the same general configuration and much of its design was initiated from components used in the Helio H-500 Twin.".
- Helio_Stallion label "Helio HST-550".
- Helio_Stallion label "Helio Stallion".
- Helio_Stallion sameAs Helio_HST-550.
- Helio_Stallion sameAs m.0420ytw.
- Helio_Stallion sameAs Q1457708.
- Helio_Stallion sameAs Q1457708.
- Helio_Stallion wasDerivedFrom Helio_Stallion?oldid=556008316.
- Helio_Stallion isPrimaryTopicOf Helio_Stallion.