|

Fokker
Dr-1
Ron Sands


specifications
powerplant
propeller
length
height
wing span
wing area
seats
empty weight
useful load
gross weight
fuel capacity
range |
LeRhone
P Range110/145-180
Engine options: Warner,Lycoming;
x
x
9.4ft
3.6ft
201.8sq. ft
1
1150lb
x
1600lb
22.5gal
250n.m
|
performance
takeoff distance,
ground roll
rate of climb
max speed
cruise speed
landing distance, ground roll
service ceiling |
300ft
1800fpm
120mph
110mph
200ft
15,000ft |
limiting and recommended speeds
design manoeuvring speed (Va)
never exceed speed (Vne)
stall, power off (Vsl)
landing approach speed |
x
x
42mph
x |
All specifications are based on manufacturer's
calculations |
|
|