|
gptkbp:instance_of
|
gptkb:aircraft
|
|
gptkbp:aircraft_operated
|
gptkb:training
|
|
gptkbp:armament
|
gptkb:none
|
|
gptkbp:avionics
|
modern avionics suite
|
|
gptkbp:climb_rate
|
1,500 ft/min
|
|
gptkbp:cockpit
|
glass cockpit
|
|
gptkbp:crew
|
2
initial pilot training
|
|
gptkbp:design
|
low-wing monoplane
|
|
gptkbp:design_feature
|
high wing
|
|
gptkbp:engine
|
2 × Pratt & Whitney Canada PT6 A-25
|
|
gptkbp:engine_type
|
turboprop
|
|
gptkbp:first_delivery
|
gptkb:1993
|
|
gptkbp:first_flight
|
gptkb:1991
|
|
gptkbp:fuel_capacity
|
1,200 lb
|
|
gptkbp:height
|
4.57 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
T-1 Jayhawk
|
|
gptkbp:introduced
|
gptkb:1993
|
|
gptkbp:landing_distance
|
2,500 ft
|
|
gptkbp:landing_gear
|
tricycle landing gear
|
|
gptkbp:length
|
12.68 m
|
|
gptkbp:manufacturer
|
gptkb:Beechcraft
|
|
gptkbp:max_speed
|
400 knots
|
|
gptkbp:max_takeoff_weight
|
5,400 kg
|
|
gptkbp:military_lessons
|
yes
|
|
gptkbp:number_built
|
over 200
|
|
gptkbp:number_of_engines
|
2
|
|
gptkbp:operational_range
|
1,200 nm
|
|
gptkbp:passenger_capacity
|
2
|
|
gptkbp:payload_capacity
|
1,800 lb
|
|
gptkbp:primary_function
|
pilot training
|
|
gptkbp:propeller
|
constant speed propellers
|
|
gptkbp:range
|
1,200 nautical miles
|
|
gptkbp:retirement
|
still in service
|
|
gptkbp:role
|
gptkb:trainer_aircraft
multi-engine trainer
|
|
gptkbp:service_ceiling
|
25,000 ft
|
|
gptkbp:service_entry
|
gptkb:1993
|
|
gptkbp:stall_speed
|
70 knots
|
|
gptkbp:successor
|
gptkb:none
|
|
gptkbp:takeoff_distance
|
3,000 ft
|
|
gptkbp:training
|
multi-engine flight training
|
|
gptkbp:used_by
|
gptkb:United_States_Air_Force
|
|
gptkbp:variant
|
gptkb:T-1_A_Jayhawk
|
|
gptkbp:weight
|
3,600 kg
|
|
gptkbp:wing_area
|
30.5 m²
|
|
gptkbp:wingspan
|
14.63 m
|
|
gptkbp:bfsParent
|
gptkb:United_States_Air_Force
|
|
gptkbp:bfsLayer
|
3
|