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Daher TBM 930 - Page 122

Daher TBM 930
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Pilot's Operating Handbook
Section 3
Emergency procedures
EASA Approved
Edition 1 - January 15, 2018
Rev. 2
Page 3.3.6
Engine regulation discrepancy, power loss,
throttle control loss 2/3
Continuing
CAUTION
When MAN OVRD control is used, the available power may not be
sufficient to ensure a go-around in landing configuration, particularly if
the weight is near the maximum weight.
Do not perform a go around
Do not use the reverse
9 - Land normally.
10 - Brakes As required. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
End of procedure
If minimum power obtained is excessive :
11 - Airspeed Reduce below 178 KIAS. . . . . . . . . . . . . . . . . . . . . . . . . . . . .
By setting nose-up attitude
12 - INERT SEP switch ON. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
If ITT > 840°C :
13 - INERT SEP switch OFF. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
14 - LANDING GEAR lever DN. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
15 - FLAPS lever TO. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
16 - Long final or ILS approach Establish. . . . . . . . . . . . . . . . . . . . . . . . . . . . .
At IAS < 178 KIAS
Continue
PIM - DO NOT USE FOR FLIGHT OPERATIONS

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