Ilyushin Il-103

GPTKB entity

Statements (75)
Predicate Object
gptkbp:instance_of gptkb:aircraft
gptkbp:bfsLayer 5
gptkbp:bfsParent gptkb:Ilyushin_Il-10
gptkbp:aircraft_operated gptkb:aircraft
gptkb:Ilyushin_Il-114
gptkb:Ilyushin_Il-76
gptkb:Ilyushin_Il-96
general aviation
utility aircraft
single-engine
low-wing
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
gptkbp:engine gptkb:Ilyushin_AI-14_R
180 hp
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