About: Valmet L-80 Turbo-Vinha

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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.

Attributes	Values
rdf:type	Thing schema:Product mean of transportation Aircraft yago:Abstraction100002137 yago:Category105838765 yago:Cognition100023271 yago:Concept105835747 yago:Content105809192 yago:Idea105833840 yago:Kind105839024 yago:PsychologicalFeature100023100 aircraft yago:Type105840188
rdfs:label	Valmet L-80 Turbo-Vinha (en)
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)
dcterms:subject	1980s Finnish military trainer aircraft Low-wing aircraft Single-engined turboprop aircraft Single-engined tractor aircraft Valmet aircraft
Wikipage page ID	9719257 (xsd:integer)
Wikipage revision ID	1121787505 (xsd:integer)
Link from a Wikipage to another Wikipage	NACA airfoil Valmet Valmet L-70 Vinka Valmet L-90 Redigo Turboprop 1980s Finnish military trainer aircraft Low-wing aircraft Single-engined turboprop aircraft Hartzell Propeller Single-engined tractor aircraft Finland Valmet aircraft Valmet L-70 Valmet L-90 Allison 250-B17D
sameAs	Valmet L-80 Turbo-Vinha Valmet L-80 Turbo-Vinha Valmet L-80 Turbo-Vinha
span m	10.250000 (xsd:double)
stall speed kmh	110 (xsd:integer)
stall speed note	idle, flaps up :::: idle, flaps down (en)
wing area sqft	150.700000 (xsd:double)
wing loading note	120 (xsd:integer)
dbp:wikiPageUsesTemplate	dbt:Commons_category dbt:Cvt dbt:ISSN dbt:Refimprove dbt:Reflist dbt:Valtion_lentokonetehdas_aircraft dbt:Aircontent dbt:Aircraft_specs dbt:Infobox_Aircraft_Type
dbp:primeUnits%3F_	met (en)
first flight	1985-02-12 (xsd:date)
capacity	up to 3 (en)
crew	1 (xsd:integer)
fuel capacity	/ (en)
introduced	1983 (xsd:integer)
manufacturer	Valmet
ref	Valmet's Turbotrainer, Jane's All the World's Aircraft 1984–85 (en)
related	* Valmet L-70 * Valmet L-90 (en)
retired	1990 (xsd:integer)
status	cancelled (en)
type	Trainer (en)
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)
airfoil	root: NACA NACA 63-218(mod B3); tip: NACA 63-412(mod B3) (en)
aspect ratio	7 (xsd:integer)
ceiling m	7500 (xsd:integer)
ceiling note	+ (en)
climb rate ftmin	2065 (xsd:integer)
empty weight kg	840 (xsd:integer)
empty weight note	equipped (en)
eng1 kw	268 (xsd:integer)
eng1 name	Allison 250-B17D
eng1 number	1 (xsd:integer)
eng1 type	turboprop engine (en)
hardpoint bombs	bombs (en)
hardpoint capacity	Maximum ; inboard pylons ; outboard pylons (en)
hardpoint missiles	anti-helicopter missiles (en)
hardpoint other	various machine-gun pods, flares searchlight pods (en)
hardpoint rockets	37 (xsd:integer)
hardpoints	4 (xsd:integer)
height m	3.300000 (xsd:double)
length m	7.880000 (xsd:double)
max speed kmh	350 (xsd:integer)
max speed note	at (en)
max takeoff weight kg	1800 (xsd:integer)
max takeoff weight note	(en)
more performance	Take-off distance to : Landing distance from : (en)
never exceed speed kmh	460 (xsd:integer)
number built	one L-80, two L-90 prototypes (en)
prop blade number	3 (xsd:integer)
prop dia m	2.190000 (xsd:double)
prop dia note	constant-speed propeller (en)
prop name	Hartzell Propeller
range km	1550 (xsd:integer)
range note	max fuel, no reserve (en)

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