gptkbp:instance_of
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gptkb:aircraft
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gptkbp:armament
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gptkb:none
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gptkbp:aspect_ratio
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6.4
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gptkbp:climb_rate
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1,200 ft/min
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gptkbp:cockpit
|
dual control
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gptkbp:control_surfaces
|
elevator, ailerons, rudder
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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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gptkb:Continental_IO-550
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gptkbp:engine_type
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piston engine
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gptkbp:first_flight
|
1953
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gptkbp:flaps
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split flaps
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gptkbp:fuel_capacity
|
200 liters
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gptkbp:height
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2.74 m
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https://www.w3.org/2000/01/rdf-schema#label
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Beechcraft T-34 Mentor
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gptkbp:introduced
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gptkb:1954
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gptkbp:landing_gear
|
tricycle landing gear
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gptkbp:length
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8.23 m
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gptkbp:manufacturer
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gptkb:Beechcraft
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gptkbp:max_speed
|
200 knots
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gptkbp:notable_users
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gptkb:Philippine_Air_Force
gptkb:Venezuelan_Air_Force
gptkb:Colombian_Air_Force
gptkb:Royal_Canadian_Air_Force
gptkb:United_States_Army
gptkb:Brazilian_Air_Force
gptkb:Uruguayan_Air_Force
gptkb:Honduran_Air_Force
gptkb:U._S._Coast_Guard
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gptkbp:number_built
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over 6000
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gptkbp:power_output
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300 hp
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gptkbp:primary_function
|
pilot training
aerobatic training
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gptkbp:production_years
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1953-1990
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gptkbp:propeller
|
two-bladed propeller
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gptkbp:range
|
1,000 nautical miles
|
gptkbp:retired
|
2000s
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gptkbp:role
|
gptkb:trainer_aircraft
civilian aircraft
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gptkbp:roll_rate
|
4.5°/s
|
gptkbp:service_ceiling
|
25,000 ft
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gptkbp:stall_speed
|
60 knots
|
gptkbp:successor
|
gptkb:Beechcraft_T-6_Texan_II
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gptkbp:trademark
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gptkb:mentorship
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gptkbp:used_by
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gptkb:United_States_Air_Force
gptkb:United_States_Navy
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gptkbp:variant
|
T-34 A
T-34 B
T-34 C
T-34 D
|
gptkbp:weight
|
1,200 kg
|
gptkbp:weight_limit
|
1,600 kg
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gptkbp:wing_area
|
16.5 m²
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gptkbp:wingspan
|
10.67 m
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gptkbp:bfsParent
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gptkb:Philippines_Air_Force
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gptkbp:bfsLayer
|
6
|