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gptkbp:instanceOf
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gptkb:aircraft
|
|
gptkbp:capacity
|
3 passengers
|
|
gptkbp:configuration
|
low-wing
single-engine
|
|
gptkbp:crew
|
1
|
|
gptkbp:designer
|
gptkb:Morane-Saulnier
|
|
gptkbp:developedBy
|
gptkb:Morane-Saulnier_MS.880
|
|
gptkbp:engineType
|
piston engine
|
|
gptkbp:firstFlight
|
1959
|
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gptkbp:height
|
2.25 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Socata Rallye
|
|
gptkbp:introduced
|
1961
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|
gptkbp:landingGear
|
fixed landing gear
|
|
gptkbp:length
|
7.25 m
|
|
gptkbp:manufacturer
|
gptkb:SOCATA
|
|
gptkbp:maximumSpeed
|
210 km/h
|
|
gptkbp:maxTakeoffWeight
|
1,000 kg
|
|
gptkbp:notableFeature
|
STOL capability
full-span automatic leading edge slats
large flaps
|
|
gptkbp:numberBuilt
|
over 3,300
|
|
gptkbp:origin
|
gptkb:France
|
|
gptkbp:powerplant
|
gptkb:Lycoming_O-320
gptkb:Lycoming_O-360
|
|
gptkbp:range
|
1,000 km
|
|
gptkbp:role
|
gptkb:aircraft
gptkb:trainer_aircraft
touring aircraft
|
|
gptkbp:serviceCeiling
|
4,000 m
|
|
gptkbp:successor
|
SOCATA TB series
|
|
gptkbp:usedBy
|
gptkb:French_Army
gptkb:French_Air_Force
civilian operators
|
|
gptkbp:variant
|
gptkb:Rallye_100
gptkb:Rallye_150
gptkb:Rallye_235
gptkb:Rallye_Commodore
gptkb:Rallye_Minerva
Rallye Club
|
|
gptkbp:wingspan
|
10.00 m
|
|
gptkbp:bfsParent
|
gptkb:Royal_Cameroonian_Air_Force
|
|
gptkbp:bfsLayer
|
5
|