SOCATA TBM 700 - Page 85

SECTION 3
EMERGENCY PROCEDURES
D.G.A.C. Approved
T B M
700 PILOT’S INFORMATION MANUAL
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Page 3.3.1
Rev. 2
3.3 – ENGINE FAILURES
ENGINE FAILURE AT TAKEOFF
BEFORE ROTATION
1 – Power lever IDLE. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
2 – Braking AS REQUIRED. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
If the airplane cannot be stopped on the remaining runway :
3 – Condition lever CUT OFF. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
4 – Tank selector OFF. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
5 – CRASH lever PULL DOWN. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .