gptkbp:instanceOf
|
aircraft
|
gptkbp:aircraft
|
single-engine aircraft
low-wing configuration
16 lb/sq ft
|
gptkbp:avionics
|
modern avionics systems
|
gptkbp:category
|
general aviation
|
gptkbp:climbRate
|
1,000 ft/min
|
gptkbp:cockpit
|
pressurized cockpit
|
gptkbp:constructionMaterial
|
aluminum alloy
all-metal fuselage
|
gptkbp:controls
|
yoke
|
gptkbp:crew
|
1
|
gptkbp:design
|
Piper_Aircraft_design_team
|
gptkbp:engine
|
IO-540-U4A5
|
gptkbp:engineConfiguration
|
Lycoming
|
gptkbp:engineType
|
reciprocating engine
|
gptkbp:firstFlight
|
1956
|
gptkbp:fuelCapacity
|
12 gallons/hour
60 US gallons
|
gptkbp:golfingEvents
|
10,000 ft
|
gptkbp:headlights
|
T-tail configuration
|
gptkbp:height
|
8 ft 6 in
|
https://www.w3.org/2000/01/rdf-schema#label
|
Piper PA-24-250 Comanche 250
|
gptkbp:introduced
|
1956
|
gptkbp:landingGear
|
tricycle gear
|
gptkbp:legacy
|
part_of_the_Piper_Comanche_series
|
gptkbp:length
|
25 ft 2 in
|
gptkbp:manufacturer
|
gptkb:Piper_Aircraft
|
gptkbp:market
|
general aviation market
|
gptkbp:maximum_speed
|
140 knots
|
gptkbp:maximumDepth
|
1,400 lb
|
gptkbp:maxRange
|
1,000 nautical miles
|
gptkbp:maxTakeoffWeight
|
3,200 lb
|
gptkbp:nickname
|
Comanche_250
|
gptkbp:notableFeature
|
low-wing design
|
gptkbp:numberBuilt
|
1,500
|
gptkbp:operationalHistory
|
used for personal and business travel
|
gptkbp:passengerCapacity
|
3
|
gptkbp:performance
|
good performance in cross-country flights
|
gptkbp:powerOutput
|
12 lb/hp
|
gptkbp:powers
|
250 hp
|
gptkbp:productionYears
|
1956-1972
|
gptkbp:products
|
A-754
|
gptkbp:propulsion
|
variable-pitch propeller
Hartzell
HC-C3YR-1
|
gptkbp:range
|
800 nautical miles
|
gptkbp:rateOfFire
|
1,000 ft/min
|
gptkbp:relatedAircraft
|
gptkb:Piper_PA-24_Comanche
|
gptkbp:retired
|
1972
|
gptkbp:serviceHistory
|
used in various flight schools.
|
gptkbp:services
|
15,000 ft
|
gptkbp:speed
|
125 knots
55 knots
|
gptkbp:takeoffDistance
|
1,500 ft
65 knots
|
gptkbp:weight
|
1,800 lb
|
gptkbp:wingArea
|
200 sq ft
|
gptkbp:wingspan
|
36 ft 0 in
|