Maintenance Manual V001
FRECCIA
Maintenance Manual V001
FRECCIA
Seite 30
Seite 31
Gascolator inspection/cleaning
1
Remove upper cowling and bottom cowling.
2
Make sure the Fuel Selector Valve is in the off position.
3
Drain the Fuel gascolator by the draining vent on the fuel gascolator tank. Remove all fuel
from Fuel gascolator tank.
4
Remove Fuel filter tank from the Fuel gascolator
5
Clean Fuel gascolator fuel strainer and sediment bowl. Inspect the Fuel gascolator sealing
for condition, replace it if damaged.
6
Install back Fuel filter tank from the Fuel gascolator. The rest of the Fuel filter tank installati-
on process goes in reverse to the Fuel filter tank removing process.
7
Move the Fuel Selector Valve to the Right tank position ON. Inspect Fuel Gascolator for
leakage.
8
Install back the Upper cowling and Bottom cowling.
2.18. PITOT – STATIC PRESSURE SYSTEM
The pitot-static tube is located under the leading edge of the right wing and consists of a air
duct. Total system pressure is sensed through the hole in the pitot-tube face and static pressure is
sensed through the holes on both sides of the rear part of fuselage.
Pressure distribution to individual instruments is received by means of flexible plastic hoses. The
tube supplies dynamic ram air pressure to the airspeed indicator, and the static ports supply
outside atmospheric pressure to the airspeed indicator, altimeter, and vertical speed indicator. If
installed, the altitude hold portion of the autopilot or mode C transponder is also connected to
the pitot system.
Static Pressure System
Static Pressure System
Pitot Pressure System
