iKarus C42 Maintenance Manual

COMCO IKARUS
Maintenance Manual C42 Series
MaintenanceManual C42-
Series_Issue_VII_18.02.2014.doc
Revison No.:1 15 from 107
- After functionality test secure the Bowden cable with cable and sleeve and
shrink tubing and cut off the supernatant Bowden cable.
III. Electrical Installation:
- Dismantel free temperature sensor at the front left cylinder.
- Mount the temperature switch, move up the sensor cable with abrasion
protection between both left cylinders and push it through the central firewall
aperture.
Figure 13: temperature switch
- In the appropriate place at the pilot’s side drill a hole for the warning light and
mount it.
Figure 14: warning light / actuating lever
- Connect the sensor cable with a cable shoe to the warning light.
- Connect the second port of the warning light with instruments " + ".
- Make functionality test with turned on main switch by removing the sensor
cable from the temperature switch and hold it against mass.
Important The light must be on.

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