|
gptkbp:instance_of
|
gptkb:aircraft
|
|
gptkbp:bfsLayer
|
7
|
|
gptkbp:bfsParent
|
gptkb:Mikulin
|
|
gptkbp:aircraft_operated
|
gptkb:Yakovlev_Yak-18
manual controls
cantilever wing
|
|
gptkbp:armament
|
gptkb:none
|
|
gptkbp:aspect_ratio
|
6.0
|
|
gptkbp:cockpit
|
tandem seating
|
|
gptkbp:crew
|
2
|
|
gptkbp:design
|
gptkb:Yakovlev_Design_Bureau
|
|
gptkbp:emergency_services
|
gptkb:musician
|
|
gptkbp:engine
|
2
|
|
gptkbp:engine_type
|
turboprop
AI-14 R
|
|
gptkbp:features
|
low-wing monoplane
|
|
gptkbp:first_flight
|
gptkb:1976
|
|
gptkbp:flaps
|
split flaps
|
|
gptkbp:floors
|
trimmable
|
|
gptkbp:fuel_capacity
|
800 liters
|
|
gptkbp:height
|
4.0 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Yakovlev Yak-66
|
|
gptkbp:instrumentation
|
analog instruments
|
|
gptkbp:is_designed_to
|
pilot training
|
|
gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:length
|
12.5 m
|
|
gptkbp:manufacturer
|
gptkb:Yakovlev
|
|
gptkbp:material
|
monocoque
symmetrical airfoil
|
|
gptkbp:max_speed
|
400 km/h
|
|
gptkbp:max_takeoff_weight
|
600 m
700 m
3,000 kg
|
|
gptkbp:notable_event
|
none reported
|
|
gptkbp:notable_ships
|
trimmable
|
|
gptkbp:number_built
|
50
|
|
gptkbp:operational_history
|
limited use
|
|
gptkbp:origin
|
gptkb:Monarch
|
|
gptkbp:primary_user
|
gptkb:Soviet_Air_Force
|
|
gptkbp:production_years
|
1976-1980
|
|
gptkbp:propulsion
|
variable-pitch propellers
|
|
gptkbp:range
|
1,200 km
|
|
gptkbp:retirement_year
|
gptkb:1990
|
|
gptkbp:role
|
gptkb:aircraft
|
|
gptkbp:roll_rate
|
5°/s
|
|
gptkbp:seating_capacity
|
1,000 kg
|
|
gptkbp:service_ceiling
|
6,000 m
|
|
gptkbp:speed
|
100 km/h
|
|
gptkbp:status
|
retired
|
|
gptkbp:surface
|
elevators, ailerons, rudder
|
|
gptkbp:tail_type
|
T-tail
|
|
gptkbp:training
|
basic flight training
|
|
gptkbp:type
|
gptkb:aircraft
|
|
gptkbp:wing_area
|
30 m²
|
|
gptkbp:wingspan
|
12.0 m
|