SOCATA TBM 700 - Page 255

SECTION 4
NORMAL PROCEDURES
D.G.A.C. Approved
T B M
700 PILOT’S INFORMATION MANUAL
Back to
Contents
Page 4.4.41
Rev. 6
AMPLIFIED PROCEDURES
BEFORE TAKEOFF
1 – Parking brake SET. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
WARNING LIGHT
PARK BRAKE
ON
2 – Condition lever HI / IDLE. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
[Ng : 68 % (+ 2 %)]
3 – Propeller governor lever FEATHER twice,. . . . . . . . . . . . . . . . . . . .
then MAX. RPM
During this test, the power lever must be at flight idle. Keep the time
spent with the propeller RPM in the caution (yellow) range at a
minimum.
4 – Fuel
– Gages CHECK. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
(Quantity / Symmetry)
–”FUEL SEL” switch CHECKED AUTO. . . . . . . . . . . . . . . . . . . . .
–”AUX BP” switch CHECKED AUTO. . . . . . . . . . . . . . . . . . . . . . .
5 – Flaps TO. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
6 – DE ICE SYSTEM panel
–”AIRFRAME DE ICE” switch As required. . . . . . . . . . . . . . . . . .
–”PROP DE ICE” switch As required. . . . . . . . . . . . . . . . . . . . . .
If runway is in good condition, without icing conditions :
–”INERT SEP” switch OFF. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
WARNING LIGHT
ÎÎÎÎÎ
ÎÎÎÎÎ
ÎÎÎÎÎ
ÎÎÎÎÎ
INERT SEP
OFF
Warning light goes out immediately, but it takes 30 seconds to
retract the separator.