SOCATA TBM 700 - Page 252

T B M
PILOT’S INFORMATION MANUAL 700
SECTION 4
NORMAL PROCEDURES
D.G.A.C. Approved
Back to
Contents
Page 4.4.38
Rev. 6
AMPLIFIED PROCEDURES
AFTER STARTING ENGINE (Cont’d)
10 –”EFIS MASTER” switch (if installed) ON. . . . . . . . . . . . . . . . . . . . .
–”TEST / CMPST” button PRESS. . . . . . . . . . . . . . . . . . . . . . . . .
–”TST / REF” button PRESS at least 3 seconds. . . . . . . . . . . . .
Detailed control procedures of EFIS system are described in
Section 9 ”Supplements”.
11 –”AP / TRIMS MASTER” switch ON. . . . . . . . . . . . . . . . . . . . . . . . . .
– Preflight test button PRESS. . . . . . . . . . . . . . . . . . . . . . . . . . . . .
–”AP / TRIMS MASTER” operation CHECK. . . . . . . . . . . . . . . . .
Detailed control procedures of autopilot and electrical pitch trim are
described in Section 9 ”Supplements”.
– Pitch trim UP / DN, then ADJUSTED. . . . . . . . . . . . . . . . . . . . .
Adjust the indicator in green range (graduated from 12 to 37 % of
center of gravity) facing corresponding center of gravity.
– Yaw trim L / R, then ADJUSTED. . . . . . . . . . . . . . . . . . . . . . . . .
Adjust the indicator in green range TO (TAKEOFF).
– Roll trim L / R, then ADJUSTED. . . . . . . . . . . . . . . . . . . . . . . . .
Adjust the indicator first at neutral position (horizontal marker).