Tecnam P2006T, Aircraft Flight Manual

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Garmin G950 IFDS - Supplement
Section 4 – Normal procedures
PREFLIGHT CHECKS
4
th
Edition, Rev. 0
Page S4 - 14
10
Left wing top and bottom panels
Visual inspection
11
Left winglet, nav and strobe
lights, static discharge wick
Check for integrity and fixing
12
Left aileron and balance mass
Visual inspection, remove tie-down devices
and control locks if employed.
13
Left Flap and hinges
Visual inspection
14
Left static port
Remove protective cap – Visual inspection
15
Antennas
Check for integrity
16
Gear pump, external power and
battery compartment
Check emergency landing gear extension
system pressure (low pressure limit: 20
bar), external power and battery compart-
ments closure.
17
Horizontal and vertical empennage
and tabs. Static discharge wicks.
Check the actuating mechanism of control
surfaces and the connection with related
tabs. Check wicks for integrity. Remove tie-
down device if employed.
18
Stabilator leading edge
Check for integrity
19
Fuselage top and bottom skin
Visual inspection
20
Right static port
Remove protective cap – Visual inspection
21
Right Flap and hinges
Visual inspection
22
Right aileron and balance weight
Visual inspection, remove tie-down devices
and control locks if employed.
23
Right winglet, nav and strobe
lights, static discharge wick
Check for integrity and fixing and lighting
24
Right wing top and bottom panels
Visual inspection
25
Right wing leading edge
Visual inspection. Check cabin ventilation
inlet and carburettor heating inlet for con-
dition and free of obstruction. Check stall
strip.
26
Right fuel tank
Check that the refuelling port cap is
properly secured, then perform the fuel
tank sump drainage operating the related
valve which, after operation, must be
checked closed. Fuel must checked for wa-
ter and sediment. Verify the tank vent outlet
is clear.
27
Propeller and spinner:
The propeller blades and spinner should be
free of cracks, nicks, dents and other