Pilot's Operating Handbook
Section 4
Normal procedures
EASA Approved
Edition 1 - January 15, 2018
Rev. 2
Page 4.4.11
Preflight inspection 11/16
► Continuing
80 - Left pitot Condition. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
81 - Wing lower surface No leak. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
82 - Check fuel tank access doors for leaks.
83 - Check for surface damage.
84 - Wing deicer boots Condition / Attachment. . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
● NOTE ●
Care must be taken when refuelling the airplane to avoid damaging the wing
deicer boots. A protective apron should be used if possible.
●
85 - Fuel tank drain (two on each wing) Drain
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Fuel free of water and contamination
● NOTE ●
In case of water in fuel system, drain it carefully using the four drain valves of
tank sumps, and the fuel filter drain valve, till every trace of water or deposit has
disappeared.
A long term storage of the airplane causes water accumulation in fuel, which
absorbs additive. This phenomenon occurs when an excessive quantity of
water accumulates in fuel tank sumps. Refer to section 8 for servicing
operations relative to fuel additives.
●
L.H. main LANDING GEAR
86 - Shock absorber Check. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
87 - Doors Check. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
88 - Tire Check. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
89 - Wheel well Check. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
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