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Daher TBM 940 - Page 288

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Pilot's Operating Handbook
Section 4
Normal procedures
EASA Approved
Edition 0 - March 05, 2019
Rev. 0
Page 4.4.15
Preflight inspection 15/16
Continuing
Rear R.H. karman
121 - Oxygen cylinder Open. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
122 - Oxygen pressure Check. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
123 - Confirm OXYGEN quantity in regards with the expected flight.
124 - Oxygen pressure Check. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Fuselage rear section / empennages
VI
Check that outside handle of emergency exit is flush with door skin.
125 - ELT ARM / OFF. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
126 - ELT door Closed / Locked. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
NOTE
Access to ELT is possible through an inspection door located on R.H. side of
fuselage rear section.
127 - Static pressure ports Clean. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
128 - Ventral fins Condition / Attachments. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
NOTE
Ventral fins are made of two parts (one fixed part and one removable part with
rear lower inspection door). Check that these two parts are connected by the
locking roller.
129 - Inspection door under fuselage Attachments - Closed. . . . . . . . . . . . . . . . . . .
130 - Horizontal stabilizer deicer boots (R.H. side) Condition / Attachments. . . . . .
131 - Elevator and trim Condition / Deflection free movement /. . . . . . . . . . . . . . . .
Trim position
NOTE
To check the deflection, hold the two half-elevators near fuselage, inside both
elevator trims to avoid stresses.
Continue
PIM - DO NOT USE FOR FLIGHT OPERATIONS

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