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- Grob_G_116 abstract "The Grob G 116 was a civil utility aircraft developed in Germany in the late 1980s. It was an enlarged and more powerful four-seat version of the two-seat Grob G 115. Like its predecessor, it was a conventional low-wing cantilever monoplane with fixed tricycle undercarriage. Also like the G 115, construction throughout was of composite materials.Grob commenced displaying a highly realistic mock-up of the design in 1987, and a prototype flew the following year. However, by 1989 the firm became uncertain about the commercial viability of the aircraft in the face of heavy competition in the four-seat sector, and the project was first postponed and finally cancelled.".
- Grob_G_116 manufacturer Grob_Aircraft.
- Grob_G_116 numberBuilt "1".
- Grob_G_116 wikiPageExternalLink 1987%20-%200989.html.
- Grob_G_116 wikiPageExternalLink 1989%20-%202432.html.
- Grob_G_116 wikiPageID "16917163".
- Grob_G_116 wikiPageLength "5035".
- Grob_G_116 wikiPageOutDegree "7".
- Grob_G_116 wikiPageRevisionID "668384171".
- Grob_G_116 wikiPageWikiLink Category:German_civil_utility_aircraft_1980–1989.
- Grob_G_116 wikiPageWikiLink Category:Grob_aircraft.
- Grob_G_116 wikiPageWikiLink Flight_International.
- Grob_G_116 wikiPageWikiLink Grob_Aircraft.
- Grob_G_116 wikiPageWikiLink Grob_G_115.
- Grob_G_116 wikiPageWikiLink Lycoming_O-360.
- Grob_G_116 wikiPageWikiLinkText "Grob G 116".
- Grob_G_116 capacity "3".
- Grob_G_116 climbRateFtmin "980".
- Grob_G_116 climbRateMs "5".
- Grob_G_116 crew "One pilot".
- Grob_G_116 emptyWeightKg "710".
- Grob_G_116 emptyWeightLb "1565".
- Grob_G_116 eng1Hp "180".
- Grob_G_116 eng1Kw "134".
- Grob_G_116 eng1Number "1".
- Grob_G_116 eng1Type Lycoming_O-360.
- Grob_G_116 firstFlight "April".
- Grob_G_116 grossWeightKg "1198".
- Grob_G_116 grossWeightLb "2641".
- Grob_G_116 heightFt "9".
- Grob_G_116 heightIn "10".
- Grob_G_116 heightM "3".
- Grob_G_116 lengthFt "27".
- Grob_G_116 lengthIn "11".
- Grob_G_116 lengthM "8.5".
- Grob_G_116 manufacturer Grob_Aircraft.
- Grob_G_116 maxSpeedKmh "285".
- Grob_G_116 maxSpeedMph "177".
- Grob_G_116 metOrEng%3F_ "met".
- Grob_G_116 nationalOrigin "Germany".
- Grob_G_116 numberBuilt "1".
- Grob_G_116 rangeKm "1200".
- Grob_G_116 rangeMiles "745".
- Grob_G_116 spanFt "36".
- Grob_G_116 spanIn "1".
- Grob_G_116 spanM "11".
- Grob_G_116 type "Civil utility aircraft".
- Grob_G_116 wikiPageUsesTemplate Template:Aerospecs.
- Grob_G_116 wikiPageUsesTemplate Template:Aircontent.
- Grob_G_116 wikiPageUsesTemplate Template:Avyear.
- Grob_G_116 wikiPageUsesTemplate Template:Cite_book.
- Grob_G_116 wikiPageUsesTemplate Template:Cite_journal.
- Grob_G_116 wikiPageUsesTemplate Template:Commons_category.
- Grob_G_116 wikiPageUsesTemplate Template:Grob_aircraft.
- Grob_G_116 wikiPageUsesTemplate Template:Infobox_Aircraft_Type.
- Grob_G_116 wingAreaSqft "167".
- Grob_G_116 wingAreaSqm "15.5".
- Grob_G_116 subject Category:German_civil_utility_aircraft_1980–1989.
- Grob_G_116 subject Category:Grob_aircraft.
- Grob_G_116 hypernym Aircraft.
- Grob_G_116 type Aircraft.
- Grob_G_116 type MeanOfTransportation.
- Grob_G_116 type Product.
- Grob_G_116 type DesignedArtifact.
- Grob_G_116 type Thing.
- Grob_G_116 type Q11436.
- Grob_G_116 comment "The Grob G 116 was a civil utility aircraft developed in Germany in the late 1980s. It was an enlarged and more powerful four-seat version of the two-seat Grob G 115. Like its predecessor, it was a conventional low-wing cantilever monoplane with fixed tricycle undercarriage. Also like the G 115, construction throughout was of composite materials.Grob commenced displaying a highly realistic mock-up of the design in 1987, and a prototype flew the following year.".
- Grob_G_116 label "Grob G 116".
- Grob_G_116 sameAs Q5609892.
- Grob_G_116 sameAs m.04122pn.
- Grob_G_116 sameAs Q5609892.
- Grob_G_116 wasDerivedFrom Grob_G_116?oldid=668384171.
- Grob_G_116 isPrimaryTopicOf Grob_G_116.