SOCATA TBM 700 - Page 87

SECTION 3
EMERGENCY PROCEDURES
D.G.A.C. Approved
T B M
700 PILOT’S INFORMATION MANUAL
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Contents
Page 3.3.3
Rev. 6
3.3 – ENGINE FAILURES
ENGINE FAILURE DURING FLIGHT
1 – Power lever IDLE. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
2 – Propeller governor lever FEATHER. . . . . . . . . . . . . . . . . . . . . . . . . .
3 – Condition lever CUT OFF. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
4 – Remaining fuel CHECK. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
5 – Tank selector SWITCH TANKS. . . . . . . . . . . . . . . . . . . . . . . . . . . . .
6 –”AUX BP” switch
and fuel pressure CHECK / CORRECT. . . . . . . . . . . . . . . . . . . . . .
7 – Air start in flight (Refer to Chapter 3.4)
8 – In case of high altitude (above 12000 ft), undertake an
EMERGENCY DESCENT (Refer to Chapter 3.6)
9 – In case of failure, perform a FORCED LANDING (Refer to
Chapter 3.7)