Pilot's Operating Handbook
Section 4
Normal procedures
EASA Approved
Edition 1 - January 15, 2018
Rev. 2
Page 4.4.12
Preflight inspection 12/16
► Continuing
● NOTE ●
If airplane has been used from muddy airfields or in snow, check wheel wells to
make sure they are clean and not obstructed.
Check frequently all landing gear retraction mechanism components,
shock-absorbers, tires and brakes. This is particularly important for airplanes
used from hilly fields.
Improperly serviced or worn shock-absorbers may result in excessive loads
being transmitted to the airplane structure during ground operations. Without
passengers and baggages on board, the unpainted surface of the main gear
shock absorber tube must be visible about :
55 mm (2.17 in) of minimum height with half tank,
40 mm (1.57 in) of minimum height with full tanks.
●
Fuselage forward section
IV
Forward compartment
90 - Inside Check. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
91 - Door Close / Lock. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
92 - GPU door Closed. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
If not used
93 - Fuel circuit drain Drain. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Fuel free of water and contamination
▲ WARNING ▲
If the clogging indicator is extended, red collar visible, the flight is
not authorized.
▲
94 - Filter contamination indicator (clogging indicator) Check. . . . . . . . . . . . . . . . .
95 - L.H. exhaust stub Condition / No cracks
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
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