SOCATA TBM 700 - Page 90

T B M
PILOT’S INFORMATION MANUAL 700
SECTION 3
EMERGENCY PROCEDURES
D.G.A.C. Approved
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Contents
Page 3.3.6
Rev. 9
3.3 – ENGINE FAILURES
ENGINE REGULATION DISCREPANCY,
POWER LOSS,
POWER LEVER CONTROL LOSS (Cont’d)
6 – Perform a normal landing WITHOUT REVERSE
7 – Braking AS REQUIRED. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
If minimum power obtained is excessive :
1 – Reduce airspeed by setting airplane in nose–up attitude at
IAS < 178 KIAS
2 –”INERT SEP” switch ON. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
3 – If ITT > 800°C :
”INERT SEP” switch OFF. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
4 – Landing gear control DN. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
5 – Flaps TO. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
6 – Establish a long final or an ILS approach respecting
IAS < 178 KIAS
7 – When runway is assured :
Condition lever CUT OFF. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
8 – Propeller governor lever FEATHER. . . . . . . . . . . . . . . . . . . . . . . . . .
if necessary to extend trajectory
9 – Flaps LDG as required. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
(at IAS < 122 KIAS)
10 – Land normally WITHOUT REVERSE
11 – Braking AS REQUIRED. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .