Pilot's Operating Handbook
Section 4
Normal procedures
EASA Approved
Edition 0 - March 05, 2019
Rev. 0
Page 4.4.13
Preflight inspection 13/16
► Continuing
Air inlets
98 - Main No cracks - Unobstructed. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
● NOTE ●
Check for no cracks, which are sometimes put in evidence by traces of soot
resulting from exhaust gases.
●
99 - Lateral / upper Unobstructed. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
● NOTE ●
Lateral air inlets, which supply air conditioning system and oil cooler, are
provided with blanking covers. It is not the case for upper air inlets of RAM AIR
system (circular grille located in front of R.H. windshield) and of vapor cycle
cooling system (two rectangular grilles located forward of the circular grille).
●
100 - 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
101 - Shock absorber Check. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
102 - Doors Check. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
103 - Tire Check. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
104 - 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.
●
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