|
gptkbp:instance_of
|
gptkb:aircraft
|
|
gptkbp:aircraft_configuration
|
single-engine
|
|
gptkbp:aircraft_operated
|
gptkb:trainer_aircraft
gptkb:training
|
|
gptkbp:aircraft_role
|
gptkb:training
|
|
gptkbp:aircraft_type
|
basic trainer
|
|
gptkbp:armament
|
gptkb:none
|
|
gptkbp:aspect_ratio
|
6.5
|
|
gptkbp:climb_rate
|
1,200 ft/min
|
|
gptkbp:cockpit
|
tandem seating
|
|
gptkbp:control_surfaces
|
elevator, ailerons, rudder
|
|
gptkbp:controls
|
frise ailerons
|
|
gptkbp:crew
|
2
|
|
gptkbp:crew_capacity
|
2
|
|
gptkbp:design
|
gptkb:Beech_Aircraft_Corporation
low-wing monoplane
basic trainer
|
|
gptkbp:elevation
|
25,000 ft
|
|
gptkbp:engine
|
gptkb:Continental_IO-550
|
|
gptkbp:engine_type
|
piston engine
|
|
gptkbp:first_flight
|
1953
2000s
1953-12-01
|
|
gptkbp:flaps
|
split flaps
|
|
gptkbp:floors
|
conventional tail
|
|
gptkbp:fuel_capacity
|
200 liters
200 gallons
50 US gallons
|
|
gptkbp:fuselage_material
|
gptkb:NACA_2412
semi-monocoque
|
|
gptkbp:height
|
2.74 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
T-34 Mentor
|
|
gptkbp:introduced
|
gptkb:1954
|
|
gptkbp:landing_distance
|
1,200 ft
|
|
gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:length
|
8.23 m
|
|
gptkbp:manufacturer
|
gptkb:Beechcraft
|
|
gptkbp:max_speed
|
200 knots
|
|
gptkbp:max_takeoff_weight
|
2,800 lbs
1,600 kg
2,500 lb
|
|
gptkbp:military_technology
|
pilot training
aerobatic training
|
|
gptkbp:nickname
|
gptkb:mentorship
|
|
gptkbp:notable_features
|
low-wing monoplane
|
|
gptkbp:notable_ships
|
balanced rudder
|
|
gptkbp:number_built
|
over 1,000
over 600
|
|
gptkbp:offers_certificate
|
FAA Type Certificate A-754
|
|
gptkbp:operational_history
|
used in military training
|
|
gptkbp:power_source
|
gptkb:Continental_IO-550
|
|
gptkbp:primary_user
|
gptkb:United_States_Navy
civilian flight schools
|
|
gptkbp:produces
|
no
|
|
gptkbp:production_years
|
1953-1990
1953-1990s
|
|
gptkbp:propeller
|
two-bladed
variable-pitch propeller
|
|
gptkbp:range
|
1,000 miles
|
|
gptkbp:related_aircraft
|
gptkb:Boeing_707
gptkb:Diamond_DA40
Piper PA-28
|
|
gptkbp:retired
|
1990s
2000s
|
|
gptkbp:role
|
gptkb:trainer_aircraft
|
|
gptkbp:roll_rate
|
3.5°/s
|
|
gptkbp:service
|
1953
1990s
|
|
gptkbp:service_ceiling
|
15,000 ft
25,000 ft
|
|
gptkbp:stall_speed
|
60 knots
|
|
gptkbp:successor
|
gptkb:T-6_Texan
gptkb:T-6_Texan_II
gptkb:Beechcraft_T-6_Texan_II
turboprop trainer
|
|
gptkbp:tail_type
|
conventional tail
|
|
gptkbp:takeoff_distance
|
1,500 ft
|
|
gptkbp:training
|
primary flight training
|
|
gptkbp:type
|
civilian trainer
|
|
gptkbp:used_by
|
gptkb:United_States_Air_Force
gptkb:United_States_Navy
|
|
gptkbp:variant
|
gptkb:T-34_C_Mentor
T-34 A
T-34 B
T-34 C
T-34 D
T-34 A Mentor
T-34 B Mentor
|
|
gptkbp:weight
|
1,800 lbs
|
|
gptkbp:wing_area
|
200 sq ft
16.5 m²
|
|
gptkbp:wing_configuration
|
cantilever wing
|
|
gptkbp:wingspan
|
10.67 m
|
|
gptkbp:bfsParent
|
gptkb:E-2_C_Hawkeye
gptkb:Naval_Air_Station_New_Orleans
gptkb:T-6_Texan_II
|
|
gptkbp:bfsLayer
|
4
|