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gptkbp:instance_of
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gptkb:aircraft
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gptkbp:avionics
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basic instrumentation
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gptkbp:climb_rate
|
700 ft/min
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|
gptkbp:cockpit
|
tandem seating
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gptkbp:control_surfaces
|
elevator, ailerons, rudder
|
|
gptkbp:crew
|
gptkb:1
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|
gptkbp:cruise_speed
|
110 knots
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gptkbp:discontinued
|
gptkb:1977
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gptkbp:engine_power
|
100 hp
|
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gptkbp:engine_type
|
gptkb:Continental_O-200
piston engine
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|
gptkbp:first_flight
|
gptkb:1955
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|
gptkbp:flaps
|
split flaps
|
|
gptkbp:flight_style
|
stable and forgiving
|
|
gptkbp:fuel_capacity
|
26 gallons
|
|
gptkbp:fuel_type
|
avgas
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|
gptkbp:fuselage_material
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gptkb:metal
|
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gptkbp:height
|
2.54 m
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|
https://www.w3.org/2000/01/rdf-schema#label
|
Cessna 150 L
|
|
gptkbp:introduced
|
gptkb:1966
|
|
gptkbp:landing_distance
|
60 knots
|
|
gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:length
|
8.23 m
|
|
gptkbp:maintenance
|
relatively easy
|
|
gptkbp:manufacturer
|
gptkb:Cessna_Aircraft_Company
|
|
gptkbp:market_position
|
long-standing
|
|
gptkbp:market_segment
|
general aviation
|
|
gptkbp:max_speed
|
120 knots
|
|
gptkbp:max_takeoff_weight
|
1,157 kg
|
|
gptkbp:military_lessons
|
popular choice
|
|
gptkbp:modifications
|
STOL kits
|
|
gptkbp:notable_accidents
|
few incidents reported
|
|
gptkbp:notable_users
|
flying schools
|
|
gptkbp:number_built
|
over 23,000
|
|
gptkbp:offers_certificate
|
A1 CE
|
|
gptkbp:operational_cost
|
low
|
|
gptkbp:passenger_capacity
|
gptkb:3
|
|
gptkbp:production_years
|
1955-1977
|
|
gptkbp:propeller
|
two-bladed
|
|
gptkbp:range
|
400 nautical miles
|
|
gptkbp:rate_of_fire
|
8-10 gallons/hour
|
|
gptkbp:service_ceiling
|
14,000 ft
|
|
gptkbp:stall_speed
|
45 knots
|
|
gptkbp:tail_type
|
conventional tail
|
|
gptkbp:type
|
gptkb:light_aircraft
|
|
gptkbp:variant
|
gptkb:Cessna_150
|
|
gptkbp:weight
|
680 kg
477 kg
|
|
gptkbp:wing_area
|
16.2 m²
|
|
gptkbp:wing_configuration
|
straight wing
high wing
|
|
gptkbp:wingspan
|
11.95 m
|
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gptkbp:bfsParent
|
gptkb:Martinique_Air_Force
|
|
gptkbp:bfsLayer
|
5
|