Pilot's Operating Handbook
Section 4
Normal procedures
EASA Approved
Edition 0 - March 05, 2019
Rev. 0
Page 4.4.10
Preflight inspection
10/16
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Continuing
74 -
OAT probe
Condition
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
75 -
Fuel tank cap
Closed / Locked
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
●
NOTE
●
Fuel tank caps must be tight (which is characterized by a consequent exertion
to lock and unlock them) to avoid water infiltration in case of rain on ground,
and to avoid fuel loss in flight.
●
76 -
Fuel tank air vent
Unobstructed
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
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NOTE
●
Air vent is not likely to be obstructed by ice or water, as it is located in a wing
lower surface recess.
●
77 -
Left pitot
Condition
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
78 -
Wing lower surface
No leak
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
79 -
Check fuel tank access doors for leaks.
80 -
Check for surface damage.
81 -
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.
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Continue
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PIM - DO NOT USE FOR FLIGHT OPERATIONS