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- Canadair_CL-84 abstract "The Canadair CL-84 "Dynavert", designated by the Canadian Forces as the CX-131, was a V/STOL turbine tiltwing monoplane designed and manufactured by Canadair between 1964 and 1972. Only four of these experimental aircraft were built with three entering flight testing. Two of the CL-84s crashed due to mechanical failures, but no loss of life occurred as a result of these accidents. Despite the fact that the CL-84 was very successful in the experimental and operational trials carried out between 1972 and 1974, no production contracts resulted.".
- Canadair_CL-84 manufacturer Canadair.
- Canadair_CL-84 numberBuilt "4".
- Canadair_CL-84 origin Canada.
- Canadair_CL-84 productionEndYear "1972".
- Canadair_CL-84 productionStartYear "1964".
- Canadair_CL-84 thumbnail Canadair_CL-84-1_Dynavert_tail_rotor_02.JPG?width=300.
- Canadair_CL-84 wikiPageExternalLink 19700013309_1970013309.pdf.
- Canadair_CL-84 wikiPageExternalLink aircraftDetail.php?DYNAVERT-241.
- Canadair_CL-84 wikiPageExternalLink dynavert.htm.
- Canadair_CL-84 wikiPageExternalLink open.file?id=0108113.
- Canadair_CL-84 wikiPageExternalLink CanadairCL-84Dynavert.shtml.
- Canadair_CL-84 wikiPageExternalLink www.flight-manuals-on-cd.com.
- Canadair_CL-84 wikiPageID "2669133".
- Canadair_CL-84 wikiPageRevisionID "589197034".
- Canadair_CL-84 airfoil "NACA 633-418".
- Canadair_CL-84 capacity "12".
- Canadair_CL-84 climbRateFtmin "4200".
- Canadair_CL-84 crew "2".
- Canadair_CL-84 cruiseSpeedMph "301".
- Canadair_CL-84 emptyWeightLb "8417".
- Canadair_CL-84 eng1Name Lycoming_T53.
- Canadair_CL-84 eng1Number "2".
- Canadair_CL-84 eng1Shp "1500".
- Canadair_CL-84 eng1Type "shaft-turbines".
- Canadair_CL-84 firstFlight "1965-05-07".
- Canadair_CL-84 hasPhotoCollection Canadair_CL-84.
- Canadair_CL-84 heightM "4.34".
- Canadair_CL-84 introduced "in test evaluation".
- Canadair_CL-84 lengthFt "47".
- Canadair_CL-84 lengthIn "3.5".
- Canadair_CL-84 lists "* List of VTOL aircraft * List of experimental aircraft".
- Canadair_CL-84 manufacturer Canadair.
- Canadair_CL-84 maxSpeedMph "321".
- Canadair_CL-84 maxTakeoffWeightLb "14500".
- Canadair_CL-84 maxTakeoffWeightNote "12600".
- Canadair_CL-84 moreGeneral "*Maximum width over propeller tips:34 ft 8 in *Maximum height over propellers during wing tilt: 17 ft 1½ in".
- Canadair_CL-84 morePerformance "*Disk loading: 195 kg/m² *Power loading: 1.35 kg/kW".
- Canadair_CL-84 nationalOrigin Canada.
- Canadair_CL-84 neverExceedSpeedMph "415".
- Canadair_CL-84 numberBuilt "4".
- Canadair_CL-84 primeUnits%3F_ "imp".
- Canadair_CL-84 produced "1964".
- Canadair_CL-84 propBladeNumber "4".
- Canadair_CL-84 propDiaFt "14".
- Canadair_CL-84 propDiaIn "0".
- Canadair_CL-84 rangeMiles "421".
- Canadair_CL-84 rangeNote "with max wing fuel, VTOL, & 10% reserves".
- Canadair_CL-84 ref "Jane's All The World's Aircraft 1971–72".
- Canadair_CL-84 retired "1974".
- Canadair_CL-84 rotDiaFt "14".
- Canadair_CL-84 rotDiaIn "0".
- Canadair_CL-84 rotNumber "1".
- Canadair_CL-84 sequence "* CL-41 - CL-44 - CL-66 - CL-84 - CL-89 - CL-90 - CL-215".
- Canadair_CL-84 similarAircraft "* Bell XV-3 * Bell XV-15 * Curtiss-Wright X-19 * Hiller X-18 * LTV XC-142".
- Canadair_CL-84 spanFt "34".
- Canadair_CL-84 spanIn "4".
- Canadair_CL-84 status "retired".
- Canadair_CL-84 type "experimental VSTOL".
- Canadair_CL-84 wingAreaSqft "233.3".
- Canadair_CL-84 subject Category:Canadair_aircraft.
- Canadair_CL-84 subject Category:Canadian_experimental_aircraft_1960–1969.
- Canadair_CL-84 subject Category:Cancelled_military_aircraft_projects.
- Canadair_CL-84 subject Category:High-wing_aircraft.
- Canadair_CL-84 subject Category:Tiltwing_aircraft.
- Canadair_CL-84 subject Category:Turboshaft-powered_aircraft.
- Canadair_CL-84 subject Category:Twin-engined_tractor_aircraft.
- Canadair_CL-84 type Aircraft.
- Canadair_CL-84 type MeanOfTransportation.
- Canadair_CL-84 type Product.
- Canadair_CL-84 type Model_airplane.
- Canadair_CL-84 type TransportationDevice_Vehicle.
- Canadair_CL-84 type DesignedArtifact.
- Canadair_CL-84 comment "The Canadair CL-84 "Dynavert", designated by the Canadian Forces as the CX-131, was a V/STOL turbine tiltwing monoplane designed and manufactured by Canadair between 1964 and 1972. Only four of these experimental aircraft were built with three entering flight testing. Two of the CL-84s crashed due to mechanical failures, but no loss of life occurred as a result of these accidents.".
- Canadair_CL-84 label "Canadair CL-84".
- Canadair_CL-84 label "Canadair CL-84".
- Canadair_CL-84 label "Canadair CL-84".
- Canadair_CL-84 label "Canadair CL-84".
- Canadair_CL-84 label "Canadair CL-84".
- Canadair_CL-84 label "カナディア CL-84".
- Canadair_CL-84 sameAs Canadair_CL-84.
- Canadair_CL-84 sameAs Canadair_CL-84.
- Canadair_CL-84 sameAs Canadair_CL-84.
- Canadair_CL-84 sameAs カナディア_CL-84.
- Canadair_CL-84 sameAs m.07wqf1.
- Canadair_CL-84 sameAs Q914041.
- Canadair_CL-84 sameAs Q914041.
- Canadair_CL-84 wasDerivedFrom Canadair_CL-84?oldid=589197034.
- Canadair_CL-84 depiction Canadair_CL-84-1_Dynavert_tail_rotor_02.JPG.
- Canadair_CL-84 isPrimaryTopicOf Canadair_CL-84.