SECTION 3
EMERGENCY PROCEDURES
D.G.A.C. Approved
T B M
700 PILOT’S INFORMATION MANUAL
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Page 3.3.5
Rev. 3
3.3 – ENGINE FAILURES
ENGINE REGULATION DISCREPANCY,
POWER LOSS,
POWER LEVER CONTROL LOSS
1 – If circumstances allow :
Power lever IDLE. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
2 – Confirm engine still running
3 – Check that no parameter exceeds allowed values
4 –”MAN OVRD” control ACTUATED. . . . . . . . . . . . . . . . . . . . . . . . . .
progressively forward
(Adjust power necessary to continue flight)
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.
CAUTION
IN ”MANUAL OVERRIDE” ENGINE IS NEITHER
PROTECTED AGAINST SLAM ACCELERATIONS, NOR
AGAINST MAXIMUM SPEED OVERSHOOTING.
AVOID RAPID CONTROL MOVEMENTS AND MANAGE
ENGINE PARAMETERS
CAUTION
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
5 – Continue flight, SHORTEN if possible
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