Pilot's Operating Handbook
Section 4
Normal procedures
EASA Approved
Edition 1 - January 15, 2018
Rev. 2
Page 4.4.14
Preflight inspection 14/16
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103 - Propeller and spinner No nicks, cracks or oil leaks / Attachment. . . . .
● NOTE ●
In case of operation from contaminated runways, it is necessary to carefully
examine propeller blades, where traces of abrasion may be found. Propeller
damage may reduce blade life time and degrade performance. Any propeller
damage should be referred to maintenance personnel.
●
Nose gear
104 - Shock absorber Check
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
105 - Doors Check. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
106 - Tire Check. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
107 - Wheel well Check. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
● NOTE ●
Without passengers and baggages on board, the unpainted surface of the nose
gear shock absorber tube must be visible about :
57 mm (2.22 in) of minimum height with full tanks,
63 mm (2.46 in) of minimum height with half tank.
●
● NOTE ●
Crush or relieve the shock absorber one time or twice before the inspection to
remove possible sticking.
●
In case of doubt, request a check of the shock absorber pressure.
108 - R.H. exhaust stub Condition / No cracks. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
R.H. wing
V
Additional remarks are identical to those of L.H. wing.
109 - Fuel tank drain (two on each wing) Drain
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Fuel free of water and contamination
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