Avia M137

GPTKB entity

Statements (49)
Predicate Object
gptkbp:instance_of gptkb:aircraft
gptkbp:bfsLayer 7
gptkbp:bfsParent gptkb:Zlin_Z-42
gptkb:Zlin_Z-526
gptkbp:aircraft_operated gptkb:Avia_M135
general aviation
gptkbp:aspect_ratio 7.0
gptkbp:avionics basic avionics
gptkbp:cockpit enclosed
tandem seating
gptkbp:color military camouflage
gptkbp:controls conventional controls
gptkbp:crew gptkb:musical
gptkbp:design low-wing monoplane
gptkbp:engine_type piston engine
gptkbp:features high visibility cockpit
gptkbp:first_flight 1950
gptkbp:flaps split flaps
gptkbp:floors conventional
gptkbp:fuel_capacity 150 liters
gptkbp:historical_significance used in training pilots
https://www.w3.org/2000/01/rdf-schema#label Avia M137
gptkbp:landing_gear tricycle gear
gptkbp:length 8.0 m
gptkbp:manufacturer Avia
gptkbp:max_speed 200 km/h
gptkbp:max_takeoff_weight 300 m
400 m
gptkbp:navigation_system gptkb:radio_station
gptkbp:notable_ships balanced rudder
gptkbp:notable_users gptkb:Czechoslovak_Air_Force
gptkbp:number_built 50
gptkbp:origin gptkb:Monarch
gptkbp:production_location gptkb:Monarch
gptkbp:production_years 1950-1955
gptkbp:propulsion fixed-pitch propeller
gptkbp:range 800 km
gptkbp:retirement_year gptkb:1965
gptkbp:role gptkb:aircraft
gptkbp:seating_capacity 2
gptkbp:service_ceiling 3,000 m
gptkbp:speed 65 km/h
gptkbp:successor gptkb:Avia_M-137_A
gptkbp:type gptkb:aircraft
gptkbp:type_of frise ailerons
gptkbp:variant gptkb:Avia_M-137_B
gptkbp:weight 1,200 kg
gptkbp:wing_area 15 m²
gptkbp:wingspan 10.5 m