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gptkbp:instanceOf
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aircraft
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gptkbp:aircraft
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general aviation
light aircraft
straight wing
training and utility
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gptkbp:avionics
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modern navigation systems
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gptkbp:built
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over 1,000
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gptkbp:climbRate
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5 m/s
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gptkbp:cockpit
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dual control
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gptkbp:constructionMaterial
|
aluminum construction
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gptkbp:crew
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2
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gptkbp:design
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low-wing monoplane
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gptkbp:engine
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Lycoming IO-360
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gptkbp:engineConfiguration
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single-engine
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gptkbp:engineType
|
piston engine
|
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gptkbp:firstFlight
|
1970
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gptkbp:fuel_capacity
|
200 L
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gptkbp:headlights
|
conventional tail
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gptkbp:height
|
2.74 m
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|
https://www.w3.org/2000/01/rdf-schema#label
|
T-4A
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gptkbp:introduced
|
1970
1970s
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gptkbp:is_used_in
|
military training schools
|
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gptkbp:landing_gear
|
tricycle gear
|
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gptkbp:length
|
8.23 m
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gptkbp:manufacturer
|
gptkb:Cessna
|
|
gptkbp:maximum_speed
|
200 km/h
|
|
gptkbp:maxTakeoffWeight
|
1,588 kg
|
|
gptkbp:model
|
McCauley
|
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gptkbp:operationalRange
|
1,200 km
|
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gptkbp:passengerCapacity
|
4
|
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gptkbp:powerOutput
|
180 hp
|
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gptkbp:primaryUser
|
gptkb:United_States_Air_Force
|
|
gptkbp:productionYears
|
1970-1980s
|
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gptkbp:propulsion
|
fixed-pitch propeller
|
|
gptkbp:range
|
1,200 km
|
|
gptkbp:role
|
trainer aircraft
|
|
gptkbp:service_ceiling
|
3,000 m
|
|
gptkbp:speed
|
160 km/h
65 km/h
|
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gptkbp:successor
|
gptkb:Cessna_172
|
|
gptkbp:surrounding_area
|
15.5 m²
|
|
gptkbp:takeoffDistance
|
300 m
70 km/h
400 m
|
|
gptkbp:training
|
pilot training
|
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gptkbp:variant
|
gptkb:T-4B
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|
gptkbp:weight
|
1,500 kg
1,000 kg
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|
gptkbp:wingspan
|
11.43 m
|