Statements (56)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
aircraft
|
| gptkbp:aircraft |
light aircraft
single-engine trainer aircraft short takeoff and landing easy maintenance low operating costs good climb rate cantilever wing used in pilot training programs good fuel efficiency good maneuverability easy to fly stable flight characteristics low stall speed reliable engine performance good visibility from cockpit popular among flight schools suitable for aerobatics often featured in aviation events |
| gptkbp:cockpit |
open cockpit
|
| gptkbp:controls |
elevator
rudder aileron |
| gptkbp:crew |
1
|
| gptkbp:design |
high-wing monoplane
Piper_Aircraft_design_team |
| gptkbp:engineType |
piston engine
|
| gptkbp:firstFlight |
1936
|
| gptkbp:fuelCapacity |
30 US gallons
|
| gptkbp:headlights |
conventional tail
|
| gptkbp:height |
8 ft 0 in
|
| gptkbp:historicalSignificance |
popular in the 1930s
|
| https://www.w3.org/2000/01/rdf-schema#label |
P-26D
|
| gptkbp:landingGear |
tailwheel
|
| gptkbp:length |
24 ft 0 in
|
| gptkbp:manufacturer |
gptkb:Piper_Aircraft
|
| gptkbp:maxSpeed |
200 mph
|
| gptkbp:maxTakeoffWeight |
2,200 lb
|
| gptkbp:notableUsers |
civilian pilots
|
| gptkbp:numberBuilt |
approximately 1,000
|
| gptkbp:operationalHistory |
used in various airshows
|
| gptkbp:passengerCapacity |
1
|
| gptkbp:productionYears |
1936-1940
|
| gptkbp:propulsion |
fixed-pitch propeller
|
| gptkbp:range |
500 miles
|
| gptkbp:relatedAircraft |
P-26
P-28 P-30 |
| gptkbp:renovated |
popular among vintage aircraft enthusiasts
|
| gptkbp:retirementYear |
1960s
|
| gptkbp:role |
civil aviation
|
| gptkbp:services |
15,000 ft
|
| gptkbp:weight |
1,500 lb
|
| gptkbp:wingArea |
200 sq ft
|
| gptkbp:wingspan |
36 ft 0 in
|