FK-Lightplanes FK 9 ELA, Руководство пользователя

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Airplane Manual FK 9 ELA FK Lightplanes
Revision 6 Performance page 5-2
5.3. Cruise Performance
The following table (valid for ROTAX 912 UL; M160 (smart) is little better,
ROTAX 912 ULS little worse) presents data for fuel consumption and range.
For flight planning purpose, add a safety margin of at least 5%.
5.4. Service Ceiling
The maximum Altitide in ISA conditions is:
Engine ceiling
ROTAX 912 UL 14500ft = 4420m
ROTAX 912 ULS 16000ft = 4877m
M160 (60 KW) 15000ft = 4572m
M160 (74 KW) 16000ft = 4877m
Please observe Oxygen requirements and respect any local regulations
and rules!
When using the M160 engine do not overboost, observe the engine
manual!
12
13
14
15
16
17
18
19
130 140 150 160 170 180 190
spe e d IAS [k m /h ]
ra
n
ge
[
k
m
/l
]
6
7
8
9
10
11
12
13
14
15
co
n
su
m
pt
io
n
[
l/
h
]
range [km/l] consumpt ion [l/h]