iKarus C 42 Series 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 C 42 Series Specifications

General

Brand	iKarus
Model	C 42 Series
Category	Aircrafts
Language	English