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iKarus C42 Series User Manual

iKarus C42 Series
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Pilot Operating Handbook for the C42 Series
POH C42 SERIES ISSUE1 (B) REV7 25/04/2020 Page 10 of 73
Table of Contents
Table of Revisions ................................................................................................ 2
Manufacturer and Distributor Contact Details ................................................... 3
Introduction ........................................................................................................... 4
Three Side Views .................................................................................................. 6
Table of Contents ............................................................................................... 10
1. Operating Limits ..................................................................................... 13
1.1 Air Speeds ........................................................................................... 13
1.2 Weights ................................................................................................ 13
1.3 Structural Limitations ........................................................................ 14
1.4 Center of Gravity Limits ..................................................................... 14
1.5 Air Speed Markings ............................................................................ 14
1.6 Engine RPM Limitations .................................................................... 15
1.7 RPM Gauge Markings ......................................................................... 15
1.8 Flap Settings ....................................................................................... 15
1.9 Maximal Speed for Flap Settings ...................................................... 15
1.10 Propellers for BRP ROTAX 912 UL ............................................... 16
1.11 Hélices pour BRP ROTAX 912 ULS ............................................... 17
1.12 Noise Table for BRP ROTAX 912 UL and 912 ULS ...................... 18
1.12.1 ROTAX 912 UL ............................................................................ 18
1.12.2 ROTAX 912 ULS .......................................................................... 18
1.13 Engine Limitations ......................................................................... 19
2. Restrictions ............................................................................................. 20
3. Note to Engine Operation ...................................................................... 20
4. Flight Operations .................................................................................... 22
4.1 Taxiing ................................................................................................. 22
4.2 Take-off and Climb ............................................................................. 22
4.3 Cruise .................................................................................................. 24
4.4 Turn in Flight ....................................................................................... 25
4.5 Stall ...................................................................................................... 25
4.6 Approach and Landing ...................................................................... 26
4.7 Shutting Down the Engine ................................................................. 26
4.8 Sudden Loss of Engine Power .......................................................... 27
4.8.1 Loss of Engine Power During Take-off .................................... 27
4.8.2 Loss of Engine Power in Cruise Flight ..................................... 27
4.8.3 Start the Engine in Flight ........................................................... 28

Table of Contents

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iKarus C42 Series Specifications

General IconGeneral
ManufacturerComco Ikarus
TypeLight sport aircraft
Maximum takeoff weight472.5 kg (1, 042 lb)
EngineRotax 912
Horsepower80 hp (60 kW)
Cruise speed160 km/h
Range800 km
Service ceiling4, 000 m
Stall speed65 km/h
Rate of climb5 m/s

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