SOCATA TBM 700 - Page 261

SECTION 4
NORMAL PROCEDURES
D.G.A.C. Approved
T B M
700 PILOT’S INFORMATION MANUAL
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Page 4.4.45 (b)
Rev. 6
AMPLIFIED PROCEDURES
TAKEOFF (Cont’d)
6 – Radar switch (if installed) As required. . . . . . . . . . . . . . . . . . . . . . .
7 – PROP O’ SPEED GOVERNOR TEST
– Increase power until propeller RPM reaches 1900 RPM
– PROP O’ SPEED TEST : Maintain engaged. . . . . . . . . . . . . .
– Observe that propeller RPM decreases of 50 to 150 RPM
– PROP O’ SPEED TEST : Release. . . . . . . . . . . . . . . . . . . . . . . .
– Check that propeller RPM increases again up to 1900 RPM
8 – Brakes RELEASED. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
It is not necessary to reduce power at the end of ”OVERSPEED”
test ; torque will be about 40 % before brake release. For a normal
takeoff, maximum torque (100 %) will be applied after brake
release. On short runway, maximum torque will be applied before
brake release.
9 – Power lever TRQ = 100 %. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
10 – Takeoff ROTATION : See ”Takeoff. . . . . . . . . . . . . . . . . . . . . . . . . .
distances” Chapter 5.8
ATTITUDE : 85
Rotation speed at takeoff, according to airplane weight, is also
given in Chapter 5.8.
11 – Vertical speed indicator POSITIVE. . . . . . . . . . . . . . . . . . . . . . . . . .
12 – Brakes APPLY. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
(Briefly)