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- Aérostructure_Lutin_80 abstract "The Aérostructure Lutin 80, earlier known as the PLM 80 (planeur léger motorisé), is a small, single seat motor glider with a low power pusher configuration engine, designed and built in France in the 1980s. Only two were completed.".
- Aérostructure_Lutin_80 wikiPageID "37469437".
- Aérostructure_Lutin_80 wikiPageRevisionID "593012731".
- Aérostructure_Lutin_80 airfoil "Wortmann WX-66S-196-V1".
- Aérostructure_Lutin_80 aspectRatio "18.91".
- Aérostructure_Lutin_80 ceilingM "5000".
- Aérostructure_Lutin_80 ceilingNote "approximately".
- Aérostructure_Lutin_80 climbRateMs "6".
- Aérostructure_Lutin_80 climbRateNote "powered, maximum at sea level".
- Aérostructure_Lutin_80 crew "One".
- Aérostructure_Lutin_80 cruiseSpeedKmh "170".
- Aérostructure_Lutin_80 cruiseSpeedNote "economical, powered".
- Aérostructure_Lutin_80 emptyWeightKg "155".
- Aérostructure_Lutin_80 eng1Kw "28.5".
- Aérostructure_Lutin_80 eng1Name "JPX PAL 640".
- Aérostructure_Lutin_80 eng1Number "1".
- Aérostructure_Lutin_80 eng1Type "three cylinder two stroke, 636 c.c. swept volume.".
- Aérostructure_Lutin_80 firstFlight "1983-05-03".
- Aérostructure_Lutin_80 fuelCapacity "30.0".
- Aérostructure_Lutin_80 glideRatio "32".
- Aérostructure_Lutin_80 heightM "1.1".
- Aérostructure_Lutin_80 lengthM "5.1".
- Aérostructure_Lutin_80 manufacturer "Aérostructure SARL".
- Aérostructure_Lutin_80 maxSpeedKmh "220".
- Aérostructure_Lutin_80 maxSpeedNote "powered or gliding in smooth air".
- Aérostructure_Lutin_80 maxTakeoffWeightKg "275".
- Aérostructure_Lutin_80 nationalOrigin France.
- Aérostructure_Lutin_80 neverExceedSpeedKmh "260".
- Aérostructure_Lutin_80 neverExceedSpeedNote "powered".
- Aérostructure_Lutin_80 numberBuilt "2".
- Aérostructure_Lutin_80 mass "103".
- Aérostructure_Lutin_80 primeUnits%3F_ "met".
- Aérostructure_Lutin_80 propBladeNumber "3".
- Aérostructure_Lutin_80 propDiaM "0.94".
- Aérostructure_Lutin_80 propDiaNote ", pusher. Folding glass-fibre blades. Some photographs show a 2-bladed propeller.".
- Aérostructure_Lutin_80 rangeKm "600".
- Aérostructure_Lutin_80 rangeNote "witn maximum fuel".
- Aérostructure_Lutin_80 ref "Jane's All the World's Aircraft 1984-85. ''All performance figures estimated.".
- Aérostructure_Lutin_80 sinkRateMs "0.7".
- Aérostructure_Lutin_80 spanM "11".
- Aérostructure_Lutin_80 stallSpeedKmh "75".
- Aérostructure_Lutin_80 type "Single seat motor glider".
- Aérostructure_Lutin_80 m "49.29".
- Aérostructure_Lutin_80 subject Category:French_ultralight_aircraft_1980–1989.
- Aérostructure_Lutin_80 type Aircraft.
- Aérostructure_Lutin_80 type MeanOfTransportation.
- Aérostructure_Lutin_80 type Product.
- Aérostructure_Lutin_80 type DesignedArtifact.
- Aérostructure_Lutin_80 comment "The Aérostructure Lutin 80, earlier known as the PLM 80 (planeur léger motorisé), is a small, single seat motor glider with a low power pusher configuration engine, designed and built in France in the 1980s. Only two were completed.".
- Aérostructure_Lutin_80 label "Aérostructure Lutin 80".
- Aérostructure_Lutin_80 sameAs A%C3%A9rostructure_Lutin_80.
- Aérostructure_Lutin_80 sameAs Q4833241.
- Aérostructure_Lutin_80 sameAs Q4833241.
- Aérostructure_Lutin_80 wasDerivedFrom Aérostructure_Lutin_80?oldid=593012731.