Structural Limitations; Center Of Gravity Limits; Airspeed Markings - iKarus C 42 Series Pilot Operating Handbook

C42 SERIES Pilot Operating Handbook

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
Yellow line: ................................................................ V
Red line:
C42 ......................................................................... V
C42B / C42E / C42C ............................................. V
C42CS .................................................................. V
ATTENTION: C42 - No yellow area! → V
POH Issue 4 Rev. 5
= 54 kn / 100 km/h
X
= 75 kn / 148 km/h
A
= 97 kn / 180 km/h
NE
= 116 kn / 216 km/h
NE
= 121 kn / 225 km/h
NE
= V
B NE
Page 14 of 91