Statements (27)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:aircraft
|
| gptkbp:countryOfOrigin |
gptkb:France
|
| gptkbp:crew |
3
|
| gptkbp:engine |
Turbomeca Turmo IIIC
|
| gptkbp:enginesNumber |
4
|
| gptkbp:engineType |
turboprop
|
| gptkbp:firstFlight |
1 June 1961
|
| gptkbp:height |
7.19 m
|
| gptkbp:length |
20.04 m
|
| gptkbp:manufacturer |
gptkb:Breguet_Aviation
|
| gptkbp:maximumSpeed |
460 km/h
|
| gptkbp:maxTakeoffWeight |
24,000 kg
|
| gptkbp:notableFeature |
short takeoff and landing capability
|
| gptkbp:numberBuilt |
4
|
| gptkbp:operator |
gptkb:French_Army
gptkb:French_Air_Force |
| gptkbp:predecessor |
Breguet 940
|
| gptkbp:range |
1,800 km
|
| gptkbp:role |
STOL transport aircraft
|
| gptkbp:serviceCeiling |
7,500 m
|
| gptkbp:status |
retired
|
| gptkbp:successor |
none
|
| gptkbp:wingspan |
22.06 m
|
| gptkbp:bfsParent |
gptkb:Jean_Pinet
gptkb:Breguet_941 |
| gptkbp:bfsLayer |
8
|
| https://www.w3.org/2000/01/rdf-schema#label |
Breguet 941S
|