|
gptkbp:instance_of
|
gptkb:aircraft
|
|
gptkbp:aircraft_configuration
|
single-engine
|
|
gptkbp:aircraft_operated
|
gptkb:light_aircraft
advanced avionics
good maneuverability
developed for training purposes.
|
|
gptkbp:aircraft_role
|
trainer and light attack
|
|
gptkbp:aircraft_type
|
Aero 1400 A, Aero 1400 B
|
|
gptkbp:armament
|
gptkb:none
|
|
gptkbp:climb_rate
|
8 m/s
|
|
gptkbp:cockpit
|
glass cockpit
|
|
gptkbp:country_of_origin
|
gptkb:Czech_Republic
|
|
gptkbp:crew
|
1 pilot
|
|
gptkbp:design
|
low-wing monoplane
Aero Vodochody design team
|
|
gptkbp:engine_type
|
gptkb:turbofan_engine
gptkb:Pratt_&_Whitney_Canada_PT6_A
|
|
gptkbp:first_flight
|
gptkb:1995
|
|
gptkbp:fuel_capacity
|
400 liters
|
|
gptkbp:height
|
3.5 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Aero 1400
|
|
gptkbp:intended_use
|
pilot training
|
|
gptkbp:landing_distance
|
500 m
|
|
gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:length
|
12.5 m
|
|
gptkbp:manufacturer
|
gptkb:Aero_Vodochody
|
|
gptkbp:max_speed
|
400 km/h
|
|
gptkbp:max_takeoff_weight
|
1500 kg
|
|
gptkbp:notable_pilots
|
basic flight training
|
|
gptkbp:notable_users
|
gptkb:Czech_Air_Force
|
|
gptkbp:number_built
|
50
|
|
gptkbp:number_of_engines
|
gptkb:1
|
|
gptkbp:operational_history
|
used by military and civilian pilots
|
|
gptkbp:production_years
|
gptkb:1996
1996-2000
|
|
gptkbp:propulsion
|
jet propulsion
|
|
gptkbp:range
|
1,200 km
|
|
gptkbp:role
|
gptkb:trainer_aircraft
|
|
gptkbp:roll_rate
|
4.5°/s
|
|
gptkbp:service_ceiling
|
10,000 m
|
|
gptkbp:squadrons
|
military camouflage
|
|
gptkbp:stall_speed
|
90 km/h
|
|
gptkbp:successor
|
gptkb:Aero_L-39_Albatros
|
|
gptkbp:takeoff_distance
|
600 m
|
|
gptkbp:type
|
civil aircraft
|
|
gptkbp:weight
|
900 kg
600 kg
|
|
gptkbp:wingspan
|
10.5 m
|
|
gptkbp:bfsParent
|
gptkb:Czechoslovak_Air_Force
|
|
gptkbp:bfsLayer
|
5
|