gptkbp:instance_of
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gptkb:aircraft
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gptkbp:bfsLayer
|
5
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gptkbp:bfsParent
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gptkb:Ilyushin_Il-10
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gptkbp:aircraft_operated
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gptkb:aircraft
gptkb:Ilyushin_Il-114
gptkb:Ilyushin_Il-76
gptkb:Ilyushin_Il-96
general aviation
utility aircraft
single-engine
low-wing
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gptkbp:climb_rate
|
5 m/s
|
gptkbp:cockpit
|
tandem seating
|
gptkbp:crew
|
gptkb:musical
|
gptkbp:design
|
gptkb:aircraft
gptkb:Ilyushin_Design_Bureau
Vladimir Ilyushin
|
gptkbp:developer
|
Ilyushin Il-103 project
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gptkbp:engine
|
gptkb:Ilyushin_AI-14_R
180 hp
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gptkbp:engine_type
|
piston engine
|
gptkbp:features
|
all-metal construction
easy maintenance
high visibility cockpit
low-wing configuration
large cabin space
dual control system
low drag design
|
gptkbp:first_flight
|
gptkb:1992
gptkb:1995
1992-08-01
|
gptkbp:fuel_capacity
|
200 L
|
gptkbp:height
|
2.5 m
|
https://www.w3.org/2000/01/rdf-schema#label
|
Ilyushin Il-103
|
gptkbp:introduced
|
gptkb:1995
|
gptkbp:investment
|
training and leisure flying
|
gptkbp:landing_gear
|
tricycle gear
|
gptkbp:length
|
8.2 m
|
gptkbp:manufacturer
|
gptkb:Ilyushin
|
gptkbp:market
|
domestic and international
|
gptkbp:material
|
gptkb:NACA_4412
|
gptkbp:max_speed
|
250 km/h
300 km/h
|
gptkbp:max_takeoff_weight
|
300 m
400 m
1,200 kg
|
gptkbp:notable_users
|
gptkb:Russian_Air_Force
civil flight schools
|
gptkbp:number_built
|
50
|
gptkbp:origin
|
gptkb:Russia
|
gptkbp:production_location
|
gptkb:Russia
|
gptkbp:production_years
|
1995-2000
|
gptkbp:propulsion
|
constant speed propeller
two-bladed
propeller-driven
|
gptkbp:range
|
1,200 km
|
gptkbp:role
|
gptkb:aircraft
|
gptkbp:seating_capacity
|
gptkb:3
2
400 kg
|
gptkbp:service_ceiling
|
4,500 m
|
gptkbp:speed
|
70 km/h
|
gptkbp:status
|
in production
|
gptkbp:successor
|
gptkb:Ilyushin_Il-114
|
gptkbp:surface
|
gptkb:public_transportation_system
ailerons
rudder
aileron
|
gptkbp:type
|
gptkb:aircraft
|
gptkbp:variant
|
gptkb:Il-103_M
|
gptkbp:weight
|
1,200 kg
800 kg
|
gptkbp:wing_area
|
15.5 m²
15 m²
|
gptkbp:wingspan
|
10.5 m
|