Statements (29)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:aircraft
|
| gptkbp:armament |
gptkb:none
|
| gptkbp:cockpit |
tandem seating
|
| gptkbp:crew |
2
|
| gptkbp:design |
IAR team
|
| gptkbp:engine_type |
piston engine
|
| gptkbp:first_flight |
gptkb:1966
|
| gptkbp:fuel_capacity |
200 L
|
| https://www.w3.org/2000/01/rdf-schema#label |
IAR 111
|
| gptkbp:landing_gear |
tricycle gear
|
| gptkbp:length |
8.5 m
|
| gptkbp:manufacturer |
IAR
|
| gptkbp:max_speed |
250 km/h
|
| gptkbp:max_takeoff_weight |
1,200 kg
|
| gptkbp:number_built |
50
|
| gptkbp:number_of_engines |
gptkb:1
|
| gptkbp:operational_history |
used in flight schools
|
| gptkbp:primary_user |
gptkb:Romanian_Air_Force
|
| gptkbp:production_years |
1966-1970
|
| gptkbp:propeller |
constant speed propeller
|
| gptkbp:role |
gptkb:trainer_aircraft
|
| gptkbp:service_ceiling |
4,500 m
|
| gptkbp:successor |
gptkb:IAR_99
|
| gptkbp:training |
basic flight training
|
| gptkbp:variant |
gptkb:IAR_111_B
IAR 111 A |
| gptkbp:wingspan |
10.5 m
|
| gptkbp:bfsParent |
gptkb:IAR_111-2_B
|
| gptkbp:bfsLayer |
8
|