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Daher TBM 930 - Page 284

Daher TBM 930
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Pilot's Operating Handbook
Section 4
Normal procedures
EASA Approved
Edition 1 - January 15, 2018
Rev. 2
Page 4.4.22
Before starting engine 2/3
Continuing
15 - O2 CYL CLOSED Check OFF. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
If O2 CYL CLOSED is ON :
16 - Open isolation valve of the oxygen cylinder in R.H. Karman.
17 - TEST push-button Press. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Audio / DE ICE SYSTEM lights / stick shaker
18 - DUMP switch NORM / Guarded. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
19 - LANDING GEAR light / CHECK DOWN Test
. . . . . . . . . . . . . . . . . . . . . . . . . . .
20 - MFD Initialize. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
21 - Fuel onboard Check. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
- Quantity Check. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
- FUEL TANK SELECTOR L or R. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
22 - Residual ITT Check. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
If residual ITT > 150°C :
23 - Perform procedure Motoring. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Refer to this chapter
NOTE
A start up procedure with an engine residual ITT above 150°C may generate
an ITT exceedance.
Particular monitoring of ITT will have to be performed during start up to ensure
to keep the temperature within ITT envelope.
24 - VOLTS : BAT > 24.5 V / GPU 28 V Check. . . . . . . . . . . . . . . . . . . . . . . . . . .
25 - CAS display Check. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
26 - PARK BRAKE Check ON
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Last check before proceeding to engine start
Continue
PIM - DO NOT USE FOR FLIGHT OPERATIONS

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