Daher TBM 940 - Page 283

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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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. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
● 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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PIM - DO NOT USE FOR FLIGHT OPERATIONS