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Davis DA-2A
specifications
powerplant
propeller
length
height
wing span
wing area
seats
empty weight
useful load
gross weight
fuel capacity
range |
Continental O-200A producing 100
hp at 2,750 rpm.
64-inch diameter, two-bladed,
all-wood, fixed-pitch
17 ft 10 in
5 ft 5 in
19 ft 3 in
82.5 sq ft
2
794 lb
x
1,200 lb mtow
19.5 imp gal
315 nm |
performance
takeoff distance,
ground roll
rate of climb
max speed
cruise speed
landing distance, ground roll
service ceiling |
x
800 fpm
100kt
x
x
x |
limiting and recommended speeds
design manoeuvring speed (Va)
never exceed speed (Vne)
stall, power off (Vsl)
landing approach speed |
x
146kt
54 kt
x |
All specifications are based on manufacturer's
calculations
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