iKarus C 42 Series User Manual

C42 SERIES Pilot Operating Handbook
POH Issue 4 Rev. 5 Page 14 of 91
1.3 Structural limitations
Positive limit load factor ........................................................................ +4 g
Negative limit load factor ....................................................................... -2 g
1.4 Center of gravity limits
Reference datum ................................... Wing leading edge at a rib station
Forward center of gravity ...................... 11.8 inches (300 mm) aft of datum
Rearward center of gravity .................... 22.0 inches (560 mm) aft of datum
1.5 Airspeed markings
until 2009
white arc .............................................................. 38 - 57 kn / 71 - 105 km/h
since 2009
white arc .............................................................. 38 - 63 kn / 71 - 117 km/h
Green arc
C42 / C42B / C42E / C42C ................................. 43 - 97 kn / 79 - 180 km/h
C42CS .............................................................. 43 - 101 kn / 79 - 187 km/h
Yellow arc:
C42B / C42E / C42C ....................................... 97 - 116 kn / 180 - 216 km/h
C42CS .......................................................... 101 - 121 kn / 187 - 225 km/h
Yellow triangle:.......................................................... V
X
= 54 kn / 100 km/h
Yellow line: ................................................................ V
A
= 75 kn / 148 km/h
Red line:
C42 ......................................................................... V
NE
= 97 kn / 180 km/h
C42B / C42E / C42C ............................................. V
NE
= 116 kn / 216 km/h
C42CS .................................................................. V
NE
= 121 kn / 225 km/h
ATTENTION: C42 - No yellow area! → V
B
= V
NE

iKarus C 42 Series Specifications

General

Brand	iKarus
Model	C 42 Series
Category	Aircrafts
Language	English