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