iKarus C42 Series User Manual

Pilot Operating Handbook for the C42 Series
POH C42 SERIES ISSUE1 (B) REV7 25/04/2020 Page 39 of 73
Loading plan
weight x lever arm = torque
Empty weight
kg
mm
kg mm
1. Passenger
400
2. Fuel
950
3. Lugage (max 10kg)
950
total weight:
total torque:
lever%arm =
!"!#$%!"&'()%
[
+,%--
]
/0/12%34567/%
[
86
]
=% mm
Maximum lever arm authorized: at max weight: 300 – 560 mm
(from the reference point BP) at empty weight: 280 – 460 mm
Place and Date: ______________________________________
Signature : __________________________________________
Loading plan
weight x lever arm = torque
Empty weight
kg
mm
kg mm
1. Passenger
400
2. Fuel
950
3. Lugage (max 10kg)
950
total weight:
total torque:
lever%arm =
!"!#$%!"&'()%
[
+,%--
]
/0/12%34567/%
[
86
]
=% mm
Maximum lever arm authorized: at max weight: 300 – 560 mm
(from the reference point BP) at empty weight: 280 – 460 mm
Place and Date: ______________________________________
Signature : __________________________________________

iKarus C42 Series Specifications

General

Manufacturer	Comco Ikarus
Type	Light sport aircraft
Maximum takeoff weight	472.5 kg (1, 042 lb)
Engine	Rotax 912
Horsepower	80 hp (60 kW)
Cruise speed	160 km/h
Range	800 km
Service ceiling	4, 000 m
Stall speed	65 km/h
Rate of climb	5 m/s