iKarus C42 Owner's Manual

C42 Owner’s Manual (Microlight) Page 9
SECTION 2 - OPERATIONAL LIMITATIONS
This aircraft
- must not be flown in aerobatic manoeuvres.
- must not be flown at bank angles beyond 60 degrees.
- must be flown under daylight, VFR conditions only.
- must not be flown in known airframe icing conditions.
- must not be flown in conditions of moderate turbulence or above, or in winds exceeding 22 kts,
at surface level, less if gusty.
Always follow the appropriate regulations for this category of aircraft.
Permitted Manoeuvres
Non-aerobatic operation only.
Any manoeuvre necessary for normal flight.
Stalls.
Steep turns with bank angles not exceeding 60°
Placarded limitation must be observed at all times. Additionally pilots should only fly in conditions which
are compatible with their own ability.
Maximum permitted dry empty weight: 100 hp 912S 265.5 kg
80 hp 912 268 kg
With 472.5kg MTOW Performance Aviation MOD C42PAUK/001 and Ballistic Recovery System
Performance Aviation MOD C42PAUK/003 or C42PAUK/006:
Maximum permitted dry empty weight: 100 hp 912S 288 kg
80hp
912 290.5 kg

iKarus C42 Specifications

General

Brand	iKarus
Model	C42
Category	Aircrafts
Language	English