Structural Limitations; Center Of Gravity Limits; Air Speed Markings - iKarus C42 Series Pilot Operating Handbook

Pilot Operating Handbook for the C42 Series

1.3 Structural Limitations

Maximal admissible positive load factor:
Maximal admissible negative load factor:

1.4 Center of Gravity Limits

Reference datum (PB) :
Forward center of gravity:
Rearward center of gravity:

1.5 Air Speed Markings

White arc:
Green arc:
Yellow arc:
Yellow triangle:
Yellow line:
Red line:
ATTENTION : C42 - No yellow arc ! -> VB = V
The deviation curve for the airspeed indicator can be interpolated from
the following table.
IAS
60 70
km/h
EAS
65 74
km/h
POH C42 SERIES ISSUE1 (B) REV7
until 2009:
since 2010:
C42 (C42A), B & C
C42CS
C42 (C42A), B & C
C42CS
C42 (C42A)
C42B & C42C
C42CS
80 90 100 110 120 130 140 150 160 170 180 190 200
83 91 100 109 117 125 134 142 151 160 168 177 185
Wing leading edge at a rib
station
300 mm after PB (11.8 in)
560 mm after PB (22.0 in)
71 - 105 km/h
71 - 117 km/h
79 - 180 km/h
79 - 187 km/h
180 - 216 km/h (97 – 116 kts)
180 - 225 km/h (97 – 121 kts)
V = 100 km/h (54 kts)
X
V =148 km/h
A
V =180 km/h (97 kts)
NE
V = 216 km/h (116 kts)
NE
V = 225 km/h (121 kts)
NE
25/04/2020
+ 4 g
- 2 g
(38 - 57 kts)
(38 - 63 kts)
(43 - 97 kts)
(43 - 100 kts)
(75 kts)
NE
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