|
gptkbp:instance_of
|
gptkb:aircraft
|
|
gptkbp:bfsLayer
|
5
|
|
gptkbp:bfsParent
|
gptkb:T-6_B
|
|
gptkbp:aircraft_operated
|
gptkb:horse_race
fixed-wing aircraft
twin-engine
conventional tail
straight wing
military trainer
|
|
gptkbp:armament
|
gptkb:none
|
|
gptkbp:climb_rate
|
5 m/s
|
|
gptkbp:cockpit
|
pressurized
dual control
|
|
gptkbp:crew
|
2
|
|
gptkbp:design
|
gptkb:Beech_Aircraft_Corporation
low-wing monoplane
|
|
gptkbp:engine
|
gptkb:musical
550 hp
P T6 A-25
|
|
gptkbp:engine_type
|
turboprop
|
|
gptkbp:first_flight
|
gptkb:1956
|
|
gptkbp:fuel_capacity
|
1,200 L
300 L
|
|
gptkbp:height
|
2.74 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
T-34 C Turbo Mentor
|
|
gptkbp:introduced
|
gptkb:1957
|
|
gptkbp:is_used_by
|
gptkb:battle
|
|
gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:length
|
8.23 m
8.38 m
|
|
gptkbp:manufacturer
|
gptkb:Beechcraft
|
|
gptkbp:max_speed
|
370 km/h
|
|
gptkbp:max_takeoff_weight
|
300 m
500 m
600 m
400 m
1,600 kg
|
|
gptkbp:nickname
|
Turbo Mentor
|
|
gptkbp:notable_features
|
gptkb:engine
|
|
gptkbp:notable_users
|
gptkb:battle
|
|
gptkbp:number_built
|
approximately 600
over 600
|
|
gptkbp:operational_history
|
used in various conflicts
|
|
gptkbp:primary_user
|
U. S. Navy, U. S. Marine Corps
|
|
gptkbp:produced_by
|
gptkb:battle
|
|
gptkbp:production_years
|
1956-1980
|
|
gptkbp:propulsion
|
2
3-bladed
|
|
gptkbp:range
|
1,200 km
1,500 km
|
|
gptkbp:retired
|
2000s
|
|
gptkbp:role
|
gptkb:aircraft
|
|
gptkbp:roll_rate
|
30°/s
4.5°/s
|
|
gptkbp:seating_capacity
|
500 kg
|
|
gptkbp:service_ceiling
|
10,000 m
|
|
gptkbp:service_history
|
U. S. Navy, U. S. Coast Guard
|
|
gptkbp:services
|
gptkb:1957
|
|
gptkbp:speed
|
100 km/h
90 km/h
|
|
gptkbp:successor
|
gptkb:T-6_Texan_II
|
|
gptkbp:surface
|
elevators, ailerons, rudder
|
|
gptkbp:tail_type
|
T-tail
|
|
gptkbp:training
|
basic flight training
primary flight training
|
|
gptkbp:variant
|
gptkb:T-34_Mentor
|
|
gptkbp:weight
|
1,200 kg
1,600 kg
|
|
gptkbp:wing_area
|
20 m²
|
|
gptkbp:wingspan
|
10.67 m
|