iKarus C42B User Manual

C42 SERIES Pilot Operating Handbook
POH Issue 4 Rev. 5 Page 37 of 91
8.1 Loading plan
Loading plan
position weight x lever arm = torque
kp cm cm kp
empty weight
1. seats 40
2. fuel 95
3. baggage 130
total weight kp total torque kp
total torque [cm kp]
center of gravity CG = ------------------------------------------ = cm
total weight [kp]
allowed range for CG: 300 - 560 mm behind zero datum (leading edge)
empty weight CG: 280 - 460 mm behind zero datum (leading edge)
Date:________________ Signature:________________
Loading plan
position weight x lever arm = torque
kp cm cm kp
empty weight
1. seats 40
2. fuel 95
3. baggage 130
total weight kp total torque kp
total torque [cm kp]
center of gravity CG = ------------------------------------------ = cm
total weight [kp]
allowed range for CG: 300 - 560 mm behind zero datum (leading edge)
empty weight CG: 280 - 460 mm behind zero datum (leading edge)
Date:________________ Signature:________________
It is the pilot’s responsibility to ensure that the MTOW of 1041 lbs
(472.5 kg) is not exceeded.

iKarus C42B Specifications

General

Brand	iKarus
Model	C42B
Category	Aircrafts
Language	English