iKarus C42 User Manual

Pilot Operating Handbook for the C42 Series
POH C42 SERIES ISSUE1 (B) REV7 25/04/2020 Page 30 of 73
4.10 Emergency Procedures
4.10.1 Stalling due to Low Speed
• Reduce back pressure on the stick and lower the nose.
• Recover
4.10.2 Sideslip
• Set rudder in the opposite direction to a sideslip
• Reduce back pressure on stick
4.10.3 Spin
• Throttle to idle.
• Apply rudder opposite to the direction of rotation until the rotation
will stop
• Reduce back pressure on stick
• Slowly pull aircraft up
4.10.4 Spiral Dive
• Set aileron and rudder opposite to the direction of rotation and
• pull back the stick slightly until a horizontal position will be taken.
4.10.5 Loss of Elevator Control
With the elevator trim flap, the aircraft can be trimmed to speeds between
80 and 170 km/h (43 and 92 kts).
In calm weather condition it can also be used to try to land the aircraft. If
in doubt, deploy the parachute rescue system.

iKarus C42 Specifications

General

Manufacturer	Comco Ikarus
Type	Ultralight Aircraft
Engine	Rotax 912
Cruise Speed	160 km/h
Stall Speed	65 km/h
Seats	2
Height	2.3 m
Maximum Takeoff Weight	472.5 kg
Range	800 km
Service Ceiling	4000 m
Power Output	80 hp
Rate of Climb	5 m/s