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SOCATA TBM 700 - Page 92

SOCATA TBM 700
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T B M
PILOTS INFORMATION MANUAL 700
SECTION 3
EMERGENCY PROCEDURES
D.G.A.C. Approved
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Contents
Page 3.3.8
Rev. 4
3.3 ENGINE FAILURES
EXCESSIVE PROPELLER ROTATION SPEED
Indicates :
a propeller governor failure
In that case, the propeller overspeed limiter will limit initially the
rotation speed to 2100 RPM approximately.
or a propeller governor and overspeed limiter failure
In that case, only the torque limiter operates to limit the power.
However, the pilot intervention is necessary to maintain
Np 2000 RPM. The propeller reducer is designed for a max. Np of
2200 RPM.
1 Reduce the power and the aircraft speed to avoid propeller rotation
speeds higher than 2000 RPM.
2 Land as soon as possible.
3 Do not perform a goaround.
A goaround would damage the propeller reducer.

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