|
gptkbp:instanceOf
|
aircraft
|
|
gptkbp:aircraft
|
light aircraft
single-engine
|
|
gptkbp:climbRate
|
700 ft/min
|
|
gptkbp:cockpit
|
open cockpit
|
|
gptkbp:controls
|
elevator
rudder
aileron
|
|
gptkbp:crew
|
1 pilot
|
|
gptkbp:design
|
gptkb:Piper_Aircraft_Company
training and recreational flying
|
|
gptkbp:engine
|
gptkb:Lycoming_O-235
|
|
gptkbp:engineType
|
piston engine
|
|
gptkbp:firstFlight
|
1946
|
|
gptkbp:fuelCapacity
|
30 US gallons
|
|
gptkbp:fuelType
|
aviation gasoline
|
|
gptkbp:height
|
8 ft 0 in
|
|
gptkbp:historicalSignificance
|
popular post-war trainer
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
P-12A
|
|
gptkbp:landingGear
|
tricycle gear
|
|
gptkbp:length
|
24 ft 0 in
|
|
gptkbp:manufacturer
|
gptkb:Piper_Aircraft
|
|
gptkbp:maxSpeed
|
120 knots
|
|
gptkbp:maxTakeoffWeight
|
1,600 lb
|
|
gptkbp:notableFeature
|
low-wing design
|
|
gptkbp:numberBuilt
|
approximately 1,000
|
|
gptkbp:operationalHistory
|
used by flying schools
|
|
gptkbp:passengerCapacity
|
1 passenger
|
|
gptkbp:primaryUser
|
civil aviation
|
|
gptkbp:productionYears
|
1946-1950
|
|
gptkbp:products
|
gptkb:A-703
|
|
gptkbp:propulsion
|
two-bladed propeller
|
|
gptkbp:rateOfFire
|
700 ft/min
|
|
gptkbp:role
|
trainer aircraft
|
|
gptkbp:services
|
10,000 ft
|
|
gptkbp:speed
|
50 knots
|
|
gptkbp:succeededBy
|
3.5 seconds per 360 degrees
|
|
gptkbp:variant
|
gptkb:P-12C
P-12B
P-12D
|
|
gptkbp:weight
|
1,200 lb
|
|
gptkbp:wingArea
|
200 sq ft
|
|
gptkbp:wingspan
|
36 ft 0 in
|