|
gptkbp:instanceOf
|
gptkb:aircraft
|
|
gptkbp:aircraftType
|
gptkb:aircraft
single-engine
|
|
gptkbp:crew
|
1
|
|
gptkbp:cruiseSpeed
|
165 knots
|
|
gptkbp:engineType
|
piston
|
|
gptkbp:firstFlight
|
1975
|
|
gptkbp:height
|
8 ft 2 in
|
|
gptkbp:introduced
|
1976
|
|
gptkbp:landingGear
|
retractable tricycle
|
|
gptkbp:length
|
27 ft 7 in
|
|
gptkbp:manufacturer
|
gptkb:Piper_Aircraft
|
|
gptkbp:maximumSpeed
|
178 knots
|
|
gptkbp:maxTakeoffWeight
|
3600 lb
|
|
gptkbp:numberOfEngines
|
1
|
|
gptkbp:powerOutput
|
300 hp
|
|
gptkbp:powerplant
|
gptkb:Lycoming_IO-540-K1G5D
|
|
gptkbp:produced
|
1976
|
|
gptkbp:productionEndYear
|
1978
|
|
gptkbp:range
|
820 nmi
|
|
gptkbp:role
|
gptkb:helicopter
air taxi
personal transport
|
|
gptkbp:seatingCapacity
|
6
|
|
gptkbp:serviceCeiling
|
16,250 ft
|
|
gptkbp:successor
|
gptkb:Piper_Saratoga
|
|
gptkbp:tailDesign
|
conventional tail
T-tail (Lance II variant)
|
|
gptkbp:variant
|
gptkb:Piper_PA-32_Cherokee_Six
|
|
gptkbp:wingspan
|
32 ft 10 in
|
|
gptkbp:bfsParent
|
gptkb:Lycoming_IO-540-K1A5
gptkb:Air_Vietnam
|
|
gptkbp:bfsLayer
|
8
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Piper PA-32R Lance
|