iKarus C42 Owner's Manual

C42 Owner’s Manual (Microlight) Page 3
CONTENTS
Page
CONTENTS ............................................................................................................................................................................... 3
ISSUE AMENDMENTS ............................................................................................................................................................. 4
Preamble ................................................................................................................................................................................ 5
SECTION 1 - AIRFRAME AND ENGINE LIMITATIONS........................................................................................................ 6
SECTION 2 - OPERATIONAL LIMITATIONS ......................................................................................................................... 9
SECTION 3 - OPERATION OF THE POWERPLANT ........................................................................................................... 10
SECTION 4 - FLIGHT ............................................................................................................................................................. 11
SECTION 5 - MINIMUM REQUIRED EQUIPMENT: ........................................................................................................... 16
SECTION 6 - WEIGHT AND BALANCE .............................................................................................................................. 17
SECTION 7 - DATA PLACARDS .......................................................................................................................................... 19
SECTION 8 - CHECKLISTS.................................................................................................................................................... 24
SECTION 9 - FLIGHT PERFORMANCE............................................................................................................................... 26
SECTION 10 - DESCRIPTION OF SYSTEMS........................................................................................................................ 27
SECTION 11 - INSPECTION AND MAINTENANCE .......................................................................................................... 33
SECTION 12 - WING RIGGING AND DE-RIGGING, FLYING WITH DOORS REMOVED.......................................... 36
SECTION 13 - SETTING (RIGGING) AND MISCELLANEOUS DATA.............................................................................. 40

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