Avia M-137 A

URI: https://gptkb.org/entity/Avia_M-137_A
GPTKB entity
Statements (47)
Predicate Object
gptkbp:instance_of gptkb:aircraft
gptkbp:bfsLayer 6
gptkbp:bfsParent gptkb:Avia_M-137
gptkbp:aircraft_operated gptkb:aircraft
low-wing
gptkbp:armament gptkb:none
gptkbp:aspect_ratio 7.0
gptkbp:cockpit tandem seating
gptkbp:crew 2
gptkbp:design gptkb:Milan_B._Šebestík
gptkbp:engine Avia M-137 A engine
gptkbp:engine_type piston engine
gptkbp:features low drag design
gptkbp:first_flight gptkb:1955
gptkbp:first_introduced gptkb:1956
gptkbp:flaps split flaps
gptkbp:floors conventional
gptkbp:fuel_capacity 200 liters
gptkbp:historical_significance used for training pilots during Cold War.
https://www.w3.org/2000/01/rdf-schema#label Avia M-137 A
gptkbp:is_used_by gptkb:Czechoslovak_Air_Force
gptkbp:landing_gear tricycle gear
gptkbp:length 8.5 m
gptkbp:manufacturer Avia
gptkbp:max_speed 250 km/h
gptkbp:max_takeoff_weight 300 m
80 km/h
400 m
1,500 kg
gptkbp:notable_ships conventional
gptkbp:number_built 50
gptkbp:origin gptkb:Monarch
gptkbp:production_years 1955-1960
gptkbp:propulsion two-bladed propeller
gptkbp:range 1,000 km
gptkbp:retired 1970s
gptkbp:role gptkb:aircraft
pilot training
gptkbp:roll_rate 4°/s
gptkbp:service_ceiling 4,500 m
gptkbp:speed 70 km/h
gptkbp:successor gptkb:Avia_M-137_B
gptkbp:type gptkb:aircraft
gptkbp:variant gptkb:Avia_M-137_B
gptkbp:weight 1,200 kg
gptkbp:wing_area 15 m²
gptkbp:wingspan 10.5 m