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SOCATA TBM 700 - Page 273

SOCATA TBM 700
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SECTION 4
NORMAL PROCEDURES
D.G.A.C. Approved
T B M
700 PILOTS INFORMATION MANUAL
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Contents
Page 4.4.53 (b)
Rev. 9 PostMOD7002132
AMPLIFIED PROCEDURES
BEFORE LANDING (Contd)
7
8 Autopilot OFF. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Autopilot must be disconnected at the latest at 200 ft above the
ground or at decision height or before goaround, whichever is the
highest.
9 Radar switch (if installed) SBY. . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Short final
10 Flaps (IAS 122 KIAS) LDG. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
However, when autopilot is engaged, in APR mode, with coupled
GS, flaps must be extended in landing position before crossing the
OUTER MARKER.
11 Approach speed (Flaps LDG) 80 KIAS. . . . . . . . . . . . . . . . . . . . . . .
To ensure positive and rapid engine response to throttle movement,
it is recommended that a minimum of 10 % torque be maintained on
final approach until landing is assured.
12 –”YAW DAMPER pushbutton OFF. . . . . . . . . . . . . . . . . . . . . . . . . .
The pilot effort required to use the rudder pedals is reduced if the
yaw damper is turned off. This is particularly significant when
landing in a crosswind.

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