Daher TBM 960 - Page 119

Air Start Procedure 2 / 2
► Continuing
NOTE
The FADEC system introduces fuel following ignitor excitation.
CAUTION
The FADEC engine protection system is disabled during engine air start, thus
there is no protection against ITT exceedances.
Acceptance of a transient ITT exceedance should be considered in such
emergency situation.
16 - ITT and Ng .......................................................................................... Monitor
If air start is not successful:
17 - Perform procedure
..........
Maximum Range Descent in Subsection 3.6.
End of procedure ■
If air start is successful:
When Ng above 45%:
18 - Starter ........................................................... Check
OFF automatically
19 -
STARTER .......................................................................... Check OFF
20 - Engine parameters ...................................................................... Check
Oil pressure, oil temperature and ITT in green sector
21
- THROTTLE ......................................................................... As required
22 - TRQ available .............................................................................. Check
23 - BLEED switch ..................................................................... As required
24 - Electrical equipment ............................................................ As required
► Land as soon as possible ◄
End of procedure.
Pilot's Information Manual
Section 3
Emergency Procedures
PIM TBM 960 - Edition 0
Rev. 00
Page 3.4.3
PIM - DO NOT USE FOR FLIGHT OPERATIONS