Armstrong Whitworth A.W. 96

GPTKB entity

Predicate	Object
gptkbp:instanceOf	aircraft
gptkbp:aircraft	civil transport aircraft
gptkbp:armament	none
gptkbp:cockpit	open cockpit
gptkbp:constructionMaterial	metal
gptkbp:countryOfOrigin	gptkb:United_Kingdom
gptkbp:crew	2
gptkbp:design	gptkb:John_Dudley_North 1930s
gptkbp:enginePower	450 hp
gptkbp:engineType	radial engine
gptkbp:firstFlight	1935 1935-07-01 1940-12-31
gptkbp:fuelCapacity	1,200 L
gptkbp:headlights	conventional tail
gptkbp:height	4.57 m
https://www.w3.org/2000/01/rdf-schema#label	Armstrong Whitworth A.W. 96
gptkbp:landingGear	tailwheel
gptkbp:length	15.24 m
gptkbp:manufacturer	gptkb:Armstrong_Whitworth
gptkbp:maxRange	1,500 km
gptkbp:maxSpeed	320 km/h
gptkbp:maxTakeoffWeight	3,600 kg
gptkbp:numberOfEpisodes	2
gptkbp:passengerCapacity	8
gptkbp:primaryUser	gptkb:Royal_Air_Force gptkb:British_Airways
gptkbp:productionCompany	50 units
gptkbp:productionYears	1935-1940
gptkbp:propulsion	two-bladed
gptkbp:relatedAircraft	gptkb:Armstrong_Whitworth_A.W._38 gptkb:Armstrong_Whitworth_A.W._44 gptkb:Armstrong_Whitworth_A.W._35 gptkb:Armstrong_Whitworth_A.W._15 gptkb:Armstrong_Whitworth_A.W._29
gptkbp:retirementYear	1940
gptkbp:role	passenger transport
gptkbp:service_ceiling	6,000 m
gptkbp:services	1936
gptkbp:successor	gptkb:Armstrong_Whitworth_A.W._194
gptkbp:usedBy	gptkb:Royal_Air_Force gptkb:British_Airways
gptkbp:variant	A.W. 96A A.W. 96B
gptkbp:wingspan	22.86 m