Daher TBM 940 - Page 308

Pilot's Operating Handbook
Section 4
Normal procedures
EASA Approved
Edition 0 - March 05, 2019
Rev. 3
Page 4.4.35
After engine start 2/2
► Continuing
17 - Oxygen Check. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Verify quantity available for the planned flight.
See tables of paragraph In-flight available oxygen quantity
in this chapter and chapter 7.10 for a FAR 135 type operation
PFD 1, MFD and PFD 2
● NOTE ●
Detailed control procedures of avionics system are described in the GARMIN
Integrated Flight Deck Pilot's Guide.
●
18 - Brightness Adjust. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
19 - DISPLAY BACKUP push-button Check. . . . . . . . . . . . . . . . . . . . . . . . . .
Then return to NORMAL mode
20 - CAS Check.
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Check engine parameters
21 - A/C switch As required. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
● NOTE ●
A good cabin temperature regulation will only be obtained if A/C switch is set to
PILOT or PLT + PAX.
●
22 - TEMP selector Adjust. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
23 - SEATS HTRS MASTER switch As required. . . . . . . . . . . . . . . . . . . . . . . . . . . .
24 - BLEED switch AUTO. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
The MAX DIFF mode is available through the GTC
25 - HOT AIR FLOW distributor As required. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
● NOTE ●
HOT AIR FLOW distributor is usually set fully turned to the right. However, if
canopy misting is evident, set it fully turned to the left.
●
End of procedure.
PIM - DO NOT USE FOR FLIGHT OPERATIONS