SOCATA TBM 700 - Page 153

SECTION 3
EMERGENCY PROCEDURES
D.G.A.C. Approved
T B M
700 PILOT’S INFORMATION MANUAL
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Page 3.13.1
Rev. 6
3.13 – MISCELLANEOUS
RUNAWAY OF ONE OF THE THREE
ELECTRICAL TRIM TABS
1 –”AP / DISC TRM INT” push button PRESSED AND HOLD. . . . .
The three trim tabs are disconnected and runaway stops
2 –”AP / TRIMS MASTER” switch OFF. . . . . . . . . . . . . . . . . . . . . . . . .
3 –”AP / DISC TRM INT” push button RELEASED. . . . . . . . . . . . . . .
4 – Pitch trim may be used manually
5 – Reduce airspeed if necessary to reduce control forces
If pitch trim runaway
6 –”AP / TRIMS MASTER” switch AP OFF. . . . . . . . . . . . . . . . . . . . . .
The pitch trim may be used manually, the two other trim tabs may be
used again electrically
If rudder or aileron trim runaway
7 – PULL circuit–breaker corresponding to the defective trim tab
8 –”AP / TRIMS MASTER” switch ON. . . . . . . . . . . . . . . . . . . . . . . . . .
Two other trim tabs may be used again electrically
CRACK IN COCKPIT WINDOW OR
WINDOW PANEL
1 – Descend slowly
2 – Reduce cabin
∆P by selecting a higher cabin altitude and the
maximum cabin rate