iS
G3-8 MA FM 9408 - R01
8
Aircraft Ground Handling and Servicing
Aircraft Ground Handling and Servicing 8 - 3
crankcase. The speed of rotation is not important for the pressure
transfer into the crankcase. This process is finished when air is
returning back to the oil tank and can be noticed by a murmur from the
open oil tank.
The oil level should be between the minimum and maximum marking
on the oil dipstick. Avoid oil levels exceeding the maximum mark as
excess oil will be poured through the venting line.
Difference between “min” and “max” marking is app. 0.5
quarts.
Approved oil grade and specification can be obtained from section 8.6
of this manual.
8.4
Servicing with Fuel
fueling the aircraft
The fuel system is grounded to the aircraft engine and its subsystems.
Before fueling have the aircraft grounded on the exhaust pipe
underneath the front belly.
The filler cap is not locked. To open the filler cap (on fuselage shoulder
behind right wing root) open lid and rotate about 1/8 turn, then pull filler
neck out of fuel tank inlet. The filler cap is not connected with the
aircraft, stow it separately while fueling the aircraft. The filler neck is
sufficient in size to accommodate an AVGAS gas pump nozzle and
the venting of the fuel tank allows quick filling.
When fueling the airplane, fuel will spill out of the venting line on the
belly of the fuselage once the fuel tank is full. To avoid or minimize
environmental pollution, put a vat underneath the venting line.
Alternatively, fill up fuel until the sight gauge indicates full and do not
add more than two US gallons beyond this point.
Summary of Contents for GXiS
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Page 93: ...iS G3 8 MA FM 9405 R01 5 Performance Performance 5 11 5 6 Cruise Speed and Fuel Flow...
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Page 96: ...iS G3 8 MA FM 9405 R01 5 Performance Performance 5 14 5 8 Rate of Climb...
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Page 199: ...REMOS GXiS POH Supplement Flight Training...
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Page 214: ...REMOS GXiS POH Supplement Continued Airworthiness...
Page 230: ...REMOS GXiS POH Supplement Abbreviated Checklists...
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