Statements (31)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:aircraft
|
| gptkbp:cockpit |
pressurized
|
| gptkbp:crew |
2
|
| gptkbp:design |
low-wing monoplane
|
| gptkbp:engine_type |
piston engine
|
| gptkbp:first_flight |
gptkb:1955
1955-06-01 |
| gptkbp:height |
5.5 m
|
| https://www.w3.org/2000/01/rdf-schema#label |
Breguet 22
|
| gptkbp:landing_gear |
tricycle gear
|
| gptkbp:length |
19.5 m
|
| gptkbp:manufacturer |
gptkb:Breguet
|
| gptkbp:max_speed |
300 km/h
|
| gptkbp:max_takeoff_weight |
6,500 kg
|
| gptkbp:number_built |
50
|
| gptkbp:passenger_capacity |
gptkb:20
|
| gptkbp:primary_user |
gptkb:French_Air_Force
|
| gptkbp:production_years |
1955-1960
|
| gptkbp:propulsion |
two engines
|
| gptkbp:range |
1,200 km
|
| gptkbp:role |
gptkb:military_logistics
gptkb:transport_aircraft |
| gptkbp:service_ceiling |
6,000 m
|
| gptkbp:successor |
gptkb:Breguet_941
|
| gptkbp:variant |
gptkb:Breguet_22_A
gptkb:Breguet_22_B gptkb:Breguet_22_C |
| gptkbp:wing_area |
60 m²
|
| gptkbp:wingspan |
20.0 m
|
| gptkbp:bfsParent |
gptkb:Breguet_XIV
|
| gptkbp:bfsLayer |
7
|