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Turner T 40 A
specifications
powerplant
propeller
length
height
wing span
wing area
seats
empty weight
useful load
gross weight
fuel capacity
range |
x
x
x
x
x
x
x
x
x
x
x
x |
performance
takeoff distance,
ground roll
rate of climb
max speed
cruise speed
landing distance, ground roll
service ceiling |
x
x
x
x
x
x |
limiting and recommended speeds
design manoeuvring speed (Va)
never exceed speed (Vne)
stall, power off (Vsl)
landing approach speed |
x
x
x
x |
All specifications are based on manufacturer's
calculations |
Top Speed, mph170
Cruise, mph 147
Stall, mph 56
Range, n.m 475
Rate of Climb, fpm 850
Takeoff Distance, ft 1250
Landing Distance, ft 1200
Service Ceiling, ft 12,000
Engine Used Lyc.
HP/HP Range 125
Fuel Capacity, gal 22
Empty Weight, lb 1050
Gross Weight, lb 1600
Height, ft 6
Length, ft 20
Wingspan, ft27.7
Wing Area, sq. ft 96
No. of Seats 2
Landing Gear tri or tail
Bldg. Materials W
Two-place version of T-40. Low-wing wood
monoplane; trigear or tailwheel design; wings fold. First flew in
1969noplane; trigear or tailwheel design; wings fold. Building lime listed
as 2-10 years rather than in man hours. First
flew in 1961.
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