FK-Lightplanes FK 14 B, Pilot Operating Handbook

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POH FK 14 B FK Lightplanes
Revision 23 Limitations page 2-3
document code: FK 14 des.002
Note: Oil system, Engine lubrication system
Engines which have had the prop spun for more than 1 turn in reverse
direction allow air to be ingested into the valve train.
Action:
1. It is forbidden to spun the prop in reverse direction for more than 1
turn.
2. Inspection for correct venting of the oil system has to be performed
in cases when the prop has been spun in reverse direction for more
than 1 turn.
2.5. Propeller
Pos. Engine Propeller Diameter
01 ROTAX 912 ULS Warp / DUC 3
– Blades
1720 mm
02 ROTAX 912 ULS Mühlbauer 3
– Blades
constant speed
1570 mm
03 ROTAX 912 ULS Warp / DUC 3
– Blades
1720 mm
04 ROTAX 912 ULS Neuform 3
– Blades
constant speed
1700 mm
05 ROTAX 912 iS Mühlbauer 2
– Blades
constant speed
1750 mm
2.6. Service Ceiling
The maximum Altitide in ISA conditions at a weight of 544 kg is:
Engine ceiling
Please observe Oxygen
requirements and respect any
local regulations and rules!
ROTAX 912 ULS 16000ft = 4877m