Littner CP 80 Zephyr

Designed for racing: tapered wing with flaps added to reduce landing speed.

specifications
 
powerplant
propeller
length
height
wing span
wing area
seats
empty weight
useful load
gross weight
fuel capacity
range
Cont. HP Range90/65-90
x
17.3 ft
5.6 ft
9.7 ft
66.7 sq. ft
1
515 lb
x

840 lb
10 gal
280 n.m

performance

takeoff distance, ground roll
rate of climb
max speed
cruise speed
landing distance, ground roll
service ceiling
600 ft
2300 fpm
200 mph
155 mph
650 ft
10000 ft

limiting and recommended speeds

design manoeuvring speed (Va)
never exceed speed (Vne)
stall, power off (Vsl)
landing approach speed
x
x
50 mph
x

All specifications are based on manufacturer's calculations