Daher TBM 900 - Page 310

Pilot's Operating Handbook
Section 4
Normal procedures
EASA Approved
Edition 0 - October 31, 2013
Rev. 5
Page 4.5.3
Flight into known icing conditions 3/5
► Continuing
3 - INERT SEP ON Check ON. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
4 - AIRFRAME DE ICE switch ON. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
5 - PROP DE ICE switch ON. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
6 - WINDSHIELD switch ON. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
● NOTE ●
Standby compass indications are altered when windshield deicing system(s)
operate(s).
●
When operating under IMC :
▲ CAUTION ▲
Inertial separator position affects engine parameters, particularly TRQ
and ITT. Care must be exercised when operating the inertial separator
or when increasing power with the inertial separator ON, to avoid
exceeding engine limitations.
▲
7 - INERT SEP switch ON. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
8 - IGNITION switch ON. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
● NOTE ●
IGNITION switch may be left ON for a long period.
●
9 - INERT SEP ON Check ON. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
10 - AIRFRAME DE ICE switch ON. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
11 - PROP DE ICE switch ON. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Continue ►
PIM - DO NOT USE FOR FLIGHT OPERATIONS