G3-8 MA FM 3202 - R02
2
Operating Limitations
Operating Limitations 2 - 6
2.13 Approved Flight Maneuvers
The following maneuvers are permitted
‚
all non-aerobatic maneuvers,
including stalls and departure stalls
‚
flight with the doors off
2.14 Engine
manufacturer
Bombardier-Rotax
engine type
912 UL-S2 or 912-S2
max. power
take-off
73.5 kW / 100 HP
max. cont.
69.0 kW / 95 HP
max. engine speed
take-off
5,800 rpm
continuous
5,500 rpm
gear ratio
2.43 : 1
slipper clutch
optional
coolant
BASF Glysantin Protect Plus/G48
coolant or CHT temp min
not defined
max
135°C = 275°F
120°C = 248°F with SB-011 complied
mixing ratio
1:1 (Glysantin : water)
NOTE
Please refer to REMOS notification NOT-001 and
ROTAX SI-912-016/SI-914-019 for further information
on suitable engine fluids (fuel, oil, cooling liquid,
additives, etc).
Have a frequent look on
www.flyrotax.com
and on
www.remos.com
for the latest information.
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Страница 121: ...G3 8 MA FM 3207 R02 7 Airplane and Systems Description Systeme 7 31 fuel shut off valve engine sided fuel system...
Страница 135: ...POH Supplement Flight Training...
Страница 149: ...POH Supplement Glider Towing...
Страница 169: ...POH Supplement Banner Towing...
Страница 185: ...POH Supplement Continued Airworthiness...