iKarus C 42 Series User Manual

C42 SERIES Pilot Operating Handbook
POH Issue 4 Rev. 5 Page 63 of 91
b) During towing
- Lateral displacement of less than 30°, vertical displacement of the glider
- less than 30° (up) and 20° (down) - can be corrected using the rudder
and elevator. In the case of greater displacement angles, particularly
high vertical displacement angles, the tow rope should be released by
the towing pilot.
- Avoid tight circling with a long tow rope. When circling, make sure that
the turn radius is sufficiently large so that the glider can follow the towing
aircraft.
- If there is a danger of exceeding the maximum engine temperatures (oil
and cylinder head temperature), reduce engine power and increase the
towing speed.
c) Failure of the release mechanism
- If the release mechanism of the towing aircraft fails, execute final
approach over an obstacle-free area and land with tow hook released.
- If both release mechanisms fail, execute descent but do not exceed the
maximum rate of descent of 295.3 ft/min (1.5 m/s) and land with the
tow hook released (by employing the brake flaps of the glider, make
sure that tow rope is tense).
Avoid further releasing attempts
during the landing procedures!

iKarus C 42 Series Specifications

General

Brand	iKarus
Model	C 42 Series
Category	Aircrafts
Language	English