Daher TBM 940 - Itt

Pilot's Operating Handbook
Section 3
Emergency procedures
EASA Approved
Edition 0 - March 05, 2019
Rev. 2
Page 3.3.12
ITT
Indicates that ITT is more than 840°C.
▲ CAUTION ▲
Autothrottle engine protection system does not relieve the pilot's
responsibility to monitor and control the engine parameters within the
limitations.
▲
During engine start :
1 - Starting procedure Abort. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Refer to procedure Engine start, chapter 4.4
2 - Cancel the flight.
Inform maintenance department.
End of procedure ■
After engine start :
On ground :
3 - Cancel the flight.
Inform maintenance department.
End of procedure ■
In flight :
► Fly the airplane ◄
4 - AT disengaged Check. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
5 - THROTTLE Reduce. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
To get ITT < 840°C
► Land as soon as possible ◄
Inform maintenance department.
End of procedure.
PIM - DO NOT USE FOR FLIGHT OPERATIONS