|
gptkbp:instance_of
|
gptkb:aircraft
|
|
gptkbp:aircraft_operated
|
gptkb:aircraft
general aviation
fixed-wing aircraft
single-engine aircraft
conventional tail
straight wing
|
|
gptkbp:climb_rate
|
5 m/s
|
|
gptkbp:cockpit
|
tandem seating
|
|
gptkbp:controls
|
yoke
|
|
gptkbp:crew
|
1 pilot
|
|
gptkbp:design
|
low-wing monoplane
|
|
gptkbp:engine
|
gptkb:Continental_IO-520
|
|
gptkbp:engine_type
|
piston engine
|
|
gptkbp:first_flight
|
gptkb:1961
|
|
gptkbp:first_introduced
|
gptkb:1961
|
|
gptkbp:flaps
|
gptkb:military_officer
|
|
gptkbp:fuel_capacity
|
200 L
|
|
gptkbp:height
|
2.74 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
T-41 Mescalero
|
|
gptkbp:instrumentation
|
basic flight instruments
|
|
gptkbp:is_used_by
|
gptkb:aircraft
|
|
gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:length
|
8.23 m
|
|
gptkbp:manufacturer
|
gptkb:Cessna
|
|
gptkbp:max_speed
|
200 km/h
|
|
gptkbp:max_takeoff_weight
|
1,134 kg
|
|
gptkbp:number_built
|
gptkb:television_series
|
|
gptkbp:operational_history
|
used in military training
used in civilian training
|
|
gptkbp:primary_user
|
gptkb:military_unit
|
|
gptkbp:propulsion
|
two-bladed
propeller-driven
|
|
gptkbp:range
|
1,200 km
|
|
gptkbp:retired
|
1990s
|
|
gptkbp:role
|
gptkb:aircraft
pilot training
|
|
gptkbp:seating_capacity
|
gptkb:3
|
|
gptkbp:service_ceiling
|
4,600 m
|
|
gptkbp:speed
|
65 km/h
|
|
gptkbp:successor
|
gptkb:aircraft
|
|
gptkbp:surface
|
gptkb:public_transportation_system
rudder
aileron
|
|
gptkbp:training
|
basic flight training
advanced flight training
|
|
gptkbp:variant
|
gptkb:T-41_A
gptkb:T-41_B
gptkb:T-41_C
|
|
gptkbp:wing_area
|
16.5 m²
|
|
gptkbp:wingspan
|
11.43 m
|
|
gptkbp:bfsParent
|
gptkb:the_Army_Air_Forces
|
|
gptkbp:bfsLayer
|
5
|