LIBIS KB-6

Infobox Aircraft
name= KB-6 Matajur


caption=
type= Two-seat light trainer and tourer
manufacturer=
designer= Letalski Institut Branko Ivanus Solvenija
first flight= 1952
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retired=
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The LIBIS KB-6 Matajur was a 1950s Yugoslavian two-seat light monoplane designed by Letalski Institut Branko Ivanus Solvenija.

Design and development

The aircraft design office of the Letalski Institut Branko Ivanus Solvenija brought together teachers and students of the Ljubljana technical high school. The design office designed the KB-6 Matajur which was a two-seat light trainer and tourer that first flew on the 4 June 1952. The KB-6 was a cantilever low-wing monoplane with fixed tailwheel landing gear and an enclosed cockpit with side-by-side seating and dual controls. The aircraft was produced for use in aero-clubs until the mid-1960s.

Variants

;KB-6 Matajur:Main production variant powered by a 136hp (101kw) Regnier 4L00 inline engine.;KB-6T Matajur:Three-seat development powered by a Walter Minor 6-III-J inline engine, eight built.;LIBIS 160:Further developed version of the KB-6T with swept vertical tail, 11 built.

pecifications (LIBIS 160)

aerospecs
met or eng?= met

crew=
capacity=Three
length m=10.56
length ft=34
length in=7¾
span m=10.60
span ft=34
span in=9¼
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height m=2.15
height ft=7
height in=0¾
wing area sqm=14
wing area sqft=150.70
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empty weight kg=728
empty weight lb=1,605
gross weight kg=1137
gross weight lb=2,507
lift kg=
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eng1 number=1
eng1 type=Walter Minor 6-III-J inverted inline piston
eng1 kw= 160
eng1 hp= 119
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References

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External links

ee also

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