Matches in DBpedia 2016-04 for { <http://dbpedia.org/resource/Lambert_Mission_106> ?p ?o }
- Lambert_Mission_106 abstract "The Lambert Mission 106 is a conventionally laid out, high-wing ultralight, seating two side-by-side. Designed in Belgium, there are ULM and LSA versions.".
- Lambert_Mission_106 numberBuilt "0".
- Lambert_Mission_106 origin Belgium.
- Lambert_Mission_106 type Ultralight_aviation.
- Lambert_Mission_106 unitCost "42500.0".
- Lambert_Mission_106 unitCost "43500.0".
- Lambert_Mission_106 wikiPageID "34244564".
- Lambert_Mission_106 wikiPageLength "7033".
- Lambert_Mission_106 wikiPageOutDegree "39".
- Lambert_Mission_106 wikiPageRevisionID "668325759".
- Lambert_Mission_106 wikiPageWikiLink Aileron.
- Lambert_Mission_106 wikiPageWikiLink Aircraft_fabric_covering.
- Lambert_Mission_106 wikiPageWikiLink Aircraft_fairing.
- Lambert_Mission_106 wikiPageWikiLink Belgium.
- Lambert_Mission_106 wikiPageWikiLink Bracing_(aeronautics).
- Lambert_Mission_106 wikiPageWikiLink Cantilever.
- Lambert_Mission_106 wikiPageWikiLink Category:Belgian_aircraft_2000–2009.
- Lambert_Mission_106 wikiPageWikiLink Conventional_landing_gear.
- Lambert_Mission_106 wikiPageWikiLink Dihedral_(aeronautics).
- Lambert_Mission_106 wikiPageWikiLink Elevator_(aeronautics).
- Lambert_Mission_106 wikiPageWikiLink Empennage.
- Lambert_Mission_106 wikiPageWikiLink Fin.
- Lambert_Mission_106 wikiPageWikiLink Flap_(aeronautics).
- Lambert_Mission_106 wikiPageWikiLink Flat-four_engine.
- Lambert_Mission_106 wikiPageWikiLink Fuselage.
- Lambert_Mission_106 wikiPageWikiLink Glass_fiber.
- Lambert_Mission_106 wikiPageWikiLink Homebuilt_aircraft.
- Lambert_Mission_106 wikiPageWikiLink Landing_gear.
- Lambert_Mission_106 wikiPageWikiLink Leading_edge.
- Lambert_Mission_106 wikiPageWikiLink Light-sport_aircraft.
- Lambert_Mission_106 wikiPageWikiLink Longeron.
- Lambert_Mission_106 wikiPageWikiLink Monoplane.
- Lambert_Mission_106 wikiPageWikiLink Rotax.
- Lambert_Mission_106 wikiPageWikiLink Rudder.
- Lambert_Mission_106 wikiPageWikiLink Slovakia.
- Lambert_Mission_106 wikiPageWikiLink Tailplane.
- Lambert_Mission_106 wikiPageWikiLink Tandem.
- Lambert_Mission_106 wikiPageWikiLink Tricycle_landing_gear.
- Lambert_Mission_106 wikiPageWikiLink Trim_tab.
- Lambert_Mission_106 wikiPageWikiLink ULPower_UL260i.
- Lambert_Mission_106 wikiPageWikiLink Ultralight_aviation.
- Lambert_Mission_106 wikiPageWikiLink United_Kingdom.
- Lambert_Mission_106 wikiPageWikiLink Volkswagen.
- Lambert_Mission_106 wikiPageWikiLinkText "Lambert Mission 106".
- Lambert_Mission_106 wikiPageWikiLinkText "Mission 106".
- Lambert_Mission_106 airfoil "NACA 230102".
- Lambert_Mission_106 avionics "*Dyson Avionics D100 EFIS and EMS D10 standard".
- Lambert_Mission_106 capacity "two".
- Lambert_Mission_106 climbRateMs "5.08".
- Lambert_Mission_106 climbRateNote "maximum at sea level".
- Lambert_Mission_106 cruiseSpeedKmh "157".
- Lambert_Mission_106 emptyWeightKg "260".
- Lambert_Mission_106 eng1Hp "82".
- Lambert_Mission_106 eng1Name ULPower_UL260i.
- Lambert_Mission_106 eng1Number "1".
- Lambert_Mission_106 eng1Type Flat-four_engine.
- Lambert_Mission_106 firstFlight "c.2003".
- Lambert_Mission_106 fuelCapacity "78.0".
- Lambert_Mission_106 heightM "2.15".
- Lambert_Mission_106 heightNote "tailwheel undercarriage".
- Lambert_Mission_106 lengthM "6.1".
- Lambert_Mission_106 manufacturer "Lambert Aircraft Engineering BVBA".
- Lambert_Mission_106 maxSpeedKmh "185".
- Lambert_Mission_106 maxTakeoffWeightKg "450".
- Lambert_Mission_106 maxTakeoffWeightNote "495".
- Lambert_Mission_106 morePerformance "6600.0".
- Lambert_Mission_106 nationalOrigin Belgium.
- Lambert_Mission_106 neverExceedSpeedKmh "210".
- Lambert_Mission_106 numberBuilt "c.10".
- Lambert_Mission_106 primeUnits%3F_ "met".
- Lambert_Mission_106 propBladeNumber "3".
- Lambert_Mission_106 propName "DUC Swirl ground adjustable pitch".
- Lambert_Mission_106 rangeKm "700".
- Lambert_Mission_106 rangeNote "at 75% power".
- Lambert_Mission_106 ref "Jane's All the World's Aircraft 2011/12".
- Lambert_Mission_106 spanM "9.32".
- Lambert_Mission_106 stallSpeedKmh "65".
- Lambert_Mission_106 stallSpeedNote "flaps down".
- Lambert_Mission_106 status "In production".
- Lambert_Mission_106 type "Two seat ultralight".
- Lambert_Mission_106 unitCost "including taxes in 2010".
- Lambert_Mission_106 unitCost "€42,500 tailwheel".
- Lambert_Mission_106 unitCost "€43,500 nosewheel".
- Lambert_Mission_106 wikiPageUsesTemplate Template:Aircontent.
- Lambert_Mission_106 wikiPageUsesTemplate Template:Aircraft_specs.
- Lambert_Mission_106 wikiPageUsesTemplate Template:Commons_category.
- Lambert_Mission_106 wikiPageUsesTemplate Template:Convert.
- Lambert_Mission_106 wikiPageUsesTemplate Template:Infobox_Aircraft_Type.
- Lambert_Mission_106 wikiPageUsesTemplate Template:Reflist.
- Lambert_Mission_106 wingAreaSqm "11.8".
- Lambert_Mission_106 subject Category:Belgian_aircraft_2000–2009.
- Lambert_Mission_106 type Aircraft.
- Lambert_Mission_106 type MeanOfTransportation.
- Lambert_Mission_106 type Product.
- Lambert_Mission_106 type DesignedArtifact.
- Lambert_Mission_106 type Thing.
- Lambert_Mission_106 type Q11436.
- Lambert_Mission_106 comment "The Lambert Mission 106 is a conventionally laid out, high-wing ultralight, seating two side-by-side. Designed in Belgium, there are ULM and LSA versions.".
- Lambert_Mission_106 label "Lambert Mission 106".
- Lambert_Mission_106 sameAs Q6481276.