iKarus C42 User Manual

Pilot Operating Handbook for the C42 Series
POH C42 SERIES ISSUE1 (B) REV7 25/04/2020 Page 38 of 73
8.1 Empty Weight and Center of Gravity
Serial Number: ________________
Type : __________ Identification Code: _____________________
Weightinh:
Reference weight: ___________ kg
Empty weight: ___________ kg
X1 = mm, X2 = mm
G
2
G
2R
: kg + G2
L
: kg =__________ kg
G1 =__________ kg
G total =__________ kg
x
s
mm: mm
x
s %
: % L
It is the pilot’s responsibility to respect and verify that the aircraft
does not surpasses the maximal take-off weight.
Empty weight: __________ kg
Maximal payload: __________ kg
Maximal payload with full tank: __________ kg
Maximal take-off mass: 450,0 kg 472,5 kg
(Strike the unnecessary weight indication)
Place and Date: ______________________________________
Signature : __________________________________________

iKarus C42 Specifications

General

Manufacturer	Comco Ikarus
Type	Ultralight Aircraft
Engine	Rotax 912
Cruise Speed	160 km/h
Stall Speed	65 km/h
Seats	2
Height	2.3 m
Maximum Takeoff Weight	472.5 kg
Range	800 km
Service Ceiling	4000 m
Power Output	80 hp
Rate of Climb	5 m/s