|
1955
T-34
|
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Primary
function
|
Training
platform for Navy/Marine Corps
pilots
|
Contractor
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Raytheon
Aircraft Company (Formally Beech
Aircraft)
|
Unit
Cost
|
$1
million
|
Propulsion
|
Model
PT6A-25 turbo-prop engine
(Pratt & Whitney Aircraft of
Canada)
|
Wingspan
|
33
feet 5 inches (10
meters)
|
Length
|
28
feet 8 inches (9
meters)
|
Height
|
9
feet 11 inches (3
meters)
|
Weight
|
4,425
lb., Empty Wt. approx. 3,000
lb.
|
Speed
|
Max:
280 knots(322 mph or 515
km/hr
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Ceiling
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25,000
feet
|
Range
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Approx.
600 nautical miles
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Armament
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None
|
|
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