Daher TBM 940 - Page 285

Pilot's Operating Handbook
Section 4
Normal procedures
EASA Approved
Edition 0 - March 05, 2019
Rev. 0
Page 4.4.12
Preflight inspection 12/16
► Continuing
Fuselage forward section
IV
Forward compartment
87 - Inside Check. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
88 - Door Close / Lock. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
89 - GPU door Closed. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
If not used
90 - Fuel circuit drain Drain. . . .
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Fuel free of water and contamination
▲ WARNING ▲
If the clogging indicator is extended, red collar visible, the flight is
not authorized.
▲
91 - Filter contamination indicator (clogging indicator) Check. . . . . . . . . . . . . . . . .
92 - L.H. exhaust stub Condition / No cracks. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
● NOTE ●
Inspect if possible pressure port located inside exhaust stub. A missing port or
a cracked port may hinder correct operation of continuous heating of air inlet lip.
●
93 - Upper engine cowls Open. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
For the first flight of the day :
94 - Oil cap Closed / Locked. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
95 - Engine oil level Check. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
96 - Fuel pipes No leak, deterioration, wear. . . . . . . . . . . . . . . . . . . . . . . . . . .
97 - Engine cowls Condition. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Closed / Locked
Continue ►
PIM - DO NOT USE FOR FLIGHT OPERATIONS