Daher-Socata TBM 900 Pilot's Information Manual page 113

PILOT'S OPERATING HANDBOOK
3.4 - ENGINE MISCELLANEOUS
1 - If circumstances allow :
Throttle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
2 - Confirm engine still running
3 - Tank selector . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
4 - Check that no parameter exceeds allowed values
5 - "MAN OVRD" control
If the available power is weak, extend the landing gear only on a glide path in final approach and extend full flaps
only in short final.
Do not perform a go-around.
IN "MANUAL OVERRIDE" ENGINE IS NEITHER PROTECTED AGAINST SLAM
ACCELERATIONS, NOR AGAINST MAXIMUM SPEED OVERSHOOTING. AVOID RAPID
CONTROL MOVEMENTS AND MANAGE ENGINE PARAMETERS
IN SOME CASES, WHEN "MANUAL OVERRIDE" CONTROL IS USED, THE AVAILABLE
POWER MAY NOT BE SUFFICIENT TO ENSURE A GO-AROUND IN LANDING
CONFIGURATION, IN PARTICULAR IF THE WEIGHT IS NEAR THE MAXIMUM WEIGHT
6 - Continue flight, LAND AS SOON AS POSSIBLE
7 - Perform a normal landing WITHOUT REVERSE
8 - Braking . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Edition 0 -- October 31, 2013
Rev. 1
ENGINE REGULATION DISCREPANCY,
POWER LOSS,
THROTTLE CONTROL LOSS (1/2)
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
CAUTION
CAUTION
EMERGENCY PROCEDURES
ACTUATED progressively forward
(Adjust power necessary to continue flight)
SECTION 3
EASA Approved
Flight IDLE
SWITCH TANKS
AS REQUIRED
Page 3.4.1