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gptkbp:instance_of
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gptkb:aircraft
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gptkbp:bfsLayer
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7
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gptkbp:bfsParent
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gptkb:Curtiss_C-42
gptkb:Curtiss_C-42_Condor
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gptkbp:aircraft_operated
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Light aircraft
Single-engine aircraft
High-wing
Basic flight training
Cantilever wing
Private pilot license
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gptkbp:avionics
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gptkb:Garmin_G1000
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gptkbp:certification
|
TC A00001
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gptkbp:climb_rate
|
700 feet per minute
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gptkbp:cockpit
|
Side-by-side seating
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gptkbp:competitors
|
Piper Sport, Flight Design CT
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gptkbp:crew
|
2
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gptkbp:design
|
Cessna design team
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gptkbp:emergency_services
|
Ballistic parachute system
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gptkbp:engine
|
180 hp
Single-engine
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gptkbp:engine_type
|
Piston engine
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gptkbp:features
|
All-metal construction
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gptkbp:first_flight
|
gptkb:2000
|
|
gptkbp:fuel_capacity
|
50 gallons
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gptkbp:fuel_type
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gptkb:Avgas
|
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gptkbp:height
|
2.54 m
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|
https://www.w3.org/2000/01/rdf-schema#label
|
C-42 B
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gptkbp:is_designed_to
|
Training and recreational flying
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gptkbp:is_often_used_in
|
Flight training
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gptkbp:landing_gear
|
Tricycle gear
|
|
gptkbp:length
|
7.34 m
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gptkbp:maintenance
|
100 hours
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gptkbp:manufacturer
|
gptkb:Cessna
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|
gptkbp:market_segment
|
Light sport aircraft
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gptkbp:material
|
Aluminum alloy
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gptkbp:max_speed
|
120 knots
|
|
gptkbp:max_takeoff_weight
|
1,000 feet
1,200 feet
1,800 lbs
60 knots
|
|
gptkbp:notable_features
|
Low stall speed
|
|
gptkbp:number_built
|
Over 1,000
|
|
gptkbp:operational_area
|
Low operating costs
|
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gptkbp:origin
|
gptkb:United_States
|
|
gptkbp:production_years
|
2000-2010
|
|
gptkbp:propulsion
|
Variable-pitch propeller
|
|
gptkbp:range
|
600 miles
|
|
gptkbp:rating
|
Excellent performance
|
|
gptkbp:safety_features
|
4 stars
|
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gptkbp:seating_capacity
|
gptkb:4
|
|
gptkbp:service_ceiling
|
12,000 feet
|
|
gptkbp:service_history
|
Used in flight schools
|
|
gptkbp:speed
|
100 knots
45 knots
|
|
gptkbp:surface
|
Ailerons, elevators, rudder
|
|
gptkbp:weight
|
1,320 lbs
|
|
gptkbp:wing_area
|
150 sq ft
|
|
gptkbp:wingspan
|
10.67 m
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