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- AAC_Angel abstract "The Angel Aircraft Corporation Model 44 Angel is a twin-engine STOL utility aircraft produced in the United States since the mid-1990s. Designed by Carl Mortenson and The King's Engineering Fellowship to be well-suited for missionary work from remote locations around the world, it is a low-wing cantilever monoplane with retractable tricycle undercarriage and eight seats. The design is largely conventional, but for the fact that the engine nacelles are mounted on top of the wings in pusher configuration. Construction is of aluminium throughout.Design work began at the home of designer Carl Mortenson in 1972, with work on the prototype beginning in 1977, also from the designer's home. In 1980 the project was moved to the municipal airport in Orange City, Iowa. First flight took place on 13 January 1984, and FAA type certitication was achieved on 20 October 1992. Angel Aircraft Corporation manufactures the aircraft under a license agreement with The King's Engineering Fellowship.".
- AAC_Angel designer Carl_Mortenson.
- AAC_Angel manufacturer Angel_Aircraft_Corporation.
- AAC_Angel numberBuilt "4".
- AAC_Angel wikiPageExternalLink 6D9712752214C5388625713100569346?OpenDocument.
- AAC_Angel wikiPageExternalLink www.angelaircraft.com.
- AAC_Angel wikiPageExternalLink AACBrochure2.pdf.
- AAC_Angel wikiPageExternalLink 1993%20-%202331.html?search=kings%20angel.
- AAC_Angel wikiPageID "19320241".
- AAC_Angel wikiPageRevisionID "600583169".
- AAC_Angel capacity "7".
- AAC_Angel ceilingFt "19015".
- AAC_Angel ceilingM "5796".
- AAC_Angel climbRateFtmin "1345".
- AAC_Angel climbRateMs "6.83".
- AAC_Angel crew "One, pilot".
- AAC_Angel cruiseSpeedKmh "323".
- AAC_Angel cruiseSpeedMph "201".
- AAC_Angel designer Carl_Mortenson.
- AAC_Angel emptyWeightKg "1760".
- AAC_Angel emptyWeightLb "3880".
- AAC_Angel enduranceH "13".
- AAC_Angel enduranceMin "6".
- AAC_Angel eng1Hp "300".
- AAC_Angel eng1Kw "224".
- AAC_Angel eng1Number "2".
- AAC_Angel eng1Type "Lycoming IO-540-M1C5 air-cooled flat-six".
- AAC_Angel firstFlight "1984-01-13".
- AAC_Angel grossWeightKg "2631".
- AAC_Angel grossWeightLb "5800".
- AAC_Angel hasPhotoCollection AAC_Angel.
- AAC_Angel heightFt "11".
- AAC_Angel heightIn "6".
- AAC_Angel heightM "3.51".
- AAC_Angel lengthFt "33".
- AAC_Angel lengthIn "6".
- AAC_Angel lengthM "10.21".
- AAC_Angel manufacturer Angel_Aircraft_Corporation.
- AAC_Angel maxSpeedKmh "333".
- AAC_Angel maxSpeedMph "207".
- AAC_Angel metOrEng%3F_ "eng".
- AAC_Angel nationalOrigin "United States".
- AAC_Angel numberBuilt "4".
- AAC_Angel rangeKm "3187".
- AAC_Angel rangeMiles "1980".
- AAC_Angel ref "Jane's All The World's Aircraft 1993–94".
- AAC_Angel seeAlso "* Evangel 4500 – another Mortenson twin-engine STOL design".
- AAC_Angel spanFt "39".
- AAC_Angel spanIn "11.5".
- AAC_Angel spanM "12.18".
- AAC_Angel stallSpeedKmh "106".
- AAC_Angel stallSpeedMph "66".
- AAC_Angel type "STOL utility aircraft".
- AAC_Angel wingAreaSqft "225.4".
- AAC_Angel wingAreaSqm "20.94".
- AAC_Angel subject Category:Pusher_aircraft.
- AAC_Angel subject Category:United_States_civil_utility_aircraft_1980–1989.
- AAC_Angel type Aircraft.
- AAC_Angel type MeanOfTransportation.
- AAC_Angel type Product.
- AAC_Angel type Model_airplane.
- AAC_Angel type DesignedArtifact.
- AAC_Angel comment "The Angel Aircraft Corporation Model 44 Angel is a twin-engine STOL utility aircraft produced in the United States since the mid-1990s. Designed by Carl Mortenson and The King's Engineering Fellowship to be well-suited for missionary work from remote locations around the world, it is a low-wing cantilever monoplane with retractable tricycle undercarriage and eight seats.".
- AAC_Angel label "AAC Angel".
- AAC_Angel sameAs m.04lgbln.
- AAC_Angel sameAs Q4649841.
- AAC_Angel sameAs Q4649841.
- AAC_Angel wasDerivedFrom AAC_Angel?oldid=600583169.
- AAC_Angel homepage www.angelaircraft.com.
- AAC_Angel isPrimaryTopicOf AAC_Angel.