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gptkbp:instance_of
|
gptkb:aircraft
|
|
gptkbp:bfsLayer
|
5
|
|
gptkbp:bfsParent
|
gptkb:Aero_1700
|
|
gptkbp:armament
|
gptkb:none
|
|
gptkbp:climb_rate
|
5 m/s
|
|
gptkbp:cockpit
|
tandem seating
|
|
gptkbp:crew
|
1 pilot
|
|
gptkbp:design
|
low-wing monoplane
Aero Vodochody design team
|
|
gptkbp:engine
|
200 hp
|
|
gptkbp:engine_type
|
piston engine
|
|
gptkbp:first_flight
|
gptkb:1960
1960-06-01
|
|
gptkbp:fuel_capacity
|
200 L
|
|
gptkbp:height
|
2.5 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Aero 660
|
|
gptkbp:influenced
|
gptkb:Aero_L-29_Delfin
|
|
gptkbp:influenced_by
|
Aero 45
|
|
gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:length
|
8.2 m
|
|
gptkbp:manufacturer
|
gptkb:Aero_Vodochody
|
|
gptkbp:max_speed
|
250 km/h
|
|
gptkbp:max_takeoff_weight
|
1,200 kg
|
|
gptkbp:notable_features
|
simple maintenance
low stall speed
good handling characteristics
good visibility from cockpit
|
|
gptkbp:number_built
|
50
|
|
gptkbp:operational_history
|
gptkb:Czechoslovak_Air_Force
flight schools
private owners
|
|
gptkbp:primary_user
|
gptkb:Czechoslovak_Air_Force
|
|
gptkbp:production_years
|
1960-1965
|
|
gptkbp:propulsion
|
two-bladed
|
|
gptkbp:range
|
1,000 km
|
|
gptkbp:retirement_year
|
1970s
|
|
gptkbp:role
|
gptkb:aircraft
|
|
gptkbp:service_ceiling
|
4,500 m
|
|
gptkbp:speed
|
70 km/h
|
|
gptkbp:successor
|
gptkb:Aero_L-29_Delfin
|
|
gptkbp:training
|
basic flight training
|
|
gptkbp:type
|
civilian aircraft
|
|
gptkbp:used_in
|
aerial photography
agricultural aviation
aerobatic training
glider towing
|
|
gptkbp:variant
|
Aero 660 A
Aero 660 B
|
|
gptkbp:wing_area
|
12.5 m²
|
|
gptkbp:wingspan
|
9.5 m
|