Valmet L-80 TP Turbo-Vinha was a prototype for a new Finnish turboprop basic trainer aircraft. The aircraft, which carried the designation OH-VBB, first flew on 12 February 1985. It was destroyed in a crash on 24 April 1985, during its 14th flight, killing the test pilot Paavo Janhunen. The aircraft was a further development of the Valmet L-70 Vinka and would eventually lead to the Valmet L-90 Redigo.
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rdfs:label
| - Valmet L-80 Turbo-Vinha (en)
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rdfs:comment
| - Valmet L-80 TP Turbo-Vinha was a prototype for a new Finnish turboprop basic trainer aircraft. The aircraft, which carried the designation OH-VBB, first flew on 12 February 1985. It was destroyed in a crash on 24 April 1985, during its 14th flight, killing the test pilot Paavo Janhunen. The aircraft was a further development of the Valmet L-70 Vinka and would eventually lead to the Valmet L-90 Redigo. (en)
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dcterms:subject
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sameAs
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span m
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stall speed kmh
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stall speed note
| - idle, flaps up
:::: idle, flaps down (en)
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wing area sqft
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wing loading note
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dbp:wikiPageUsesTemplate
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dbp:primeUnits%3F_
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first flight
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capacity
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crew
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fuel capacity
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introduced
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manufacturer
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ref
| - Valmet's Turbotrainer, Jane's All the World's Aircraft 1984–85 (en)
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related
| - * Valmet L-70
* Valmet L-90 (en)
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retired
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status
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type
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has abstract
| - Valmet L-80 TP Turbo-Vinha was a prototype for a new Finnish turboprop basic trainer aircraft. The aircraft, which carried the designation OH-VBB, first flew on 12 February 1985. It was destroyed in a crash on 24 April 1985, during its 14th flight, killing the test pilot Paavo Janhunen. The aircraft was a further development of the Valmet L-70 Vinka and would eventually lead to the Valmet L-90 Redigo. The Allison turboprop engine was used in the second aircraft, the L-80 TP Turbo-Vinha (OH-VTM) which was destroyed during an aerial display in Belgium. The third of the series (OH-VTP) got the new name Redigo or RediGo (used in sales brochures). (en)
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airfoil
| - root: NACA NACA 63-218(mod B3); tip: NACA 63-412(mod B3) (en)
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aspect ratio
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ceiling m
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ceiling note
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climb rate ftmin
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empty weight kg
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empty weight note
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eng1 kw
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eng1 name
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eng1 number
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eng1 type
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hardpoint bombs
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hardpoint capacity
| - Maximum ; inboard pylons ; outboard pylons (en)
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hardpoint missiles
| - anti-helicopter missiles (en)
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hardpoint other
| - various machine-gun pods, flares searchlight pods (en)
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hardpoint rockets
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hardpoints
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height m
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length m
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max speed kmh
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max speed note
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max takeoff weight kg
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max takeoff weight note
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more performance
| - *Take-off distance to :
*Landing distance from : (en)
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never exceed speed kmh
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number built
| - one L-80, two L-90 prototypes (en)
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prop blade number
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prop dia m
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prop dia note
| - constant-speed propeller (en)
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prop name
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range km
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range note
| - max fuel, no reserve (en)
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