Daher TBM 940 - Page 175

Pilot's Operating Handbook
Section 3
Emergency procedures
EASA Approved
Edition 0 - March 05, 2019
Rev. 2
Page 3.9.5
and 2/3
MAIN GEN LOW VOLTAGE
an
► Continuing
9 - GENERATOR selector OFF. . . . . . . . . . . . . . . . . . . . . . . . . . . . .
If altitude > 10000 ft :
10 - OXYGEN switch ON. . . . . . . . . . . . . . . . . . . . . . . . . . . . .
If VMC and non-icing conditions are possible :
11 - ESS BUS TIE switch EMER. . . . . . . . . . . . . . . . . . . . . . . .
In this configuration, only both ESS BUS bars and
BATT BUS bar are directly supplied by the battery.
► Land as soon as possible ◄
If use o
f other systems is required :
12 - ESS BUS TIE switch NORM. . . . . . . . . . . . . . . . . .
End of procedure ■
If VMC and non-icing conditions are not possible :
13 - Manually disconnect systems as follows :
Breakers :
- PFD 2 Pull. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
- ADC 2 Pull. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
- TAS Pull. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
- DATA LINK Pull. . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
- XPDR 2 Pull. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Switches :
- DE ICE SYSTEM mode MAN. . . . . . . . . . . . . . . . . . .
All deicing systems turn on
- ICE LIGHT OFF. . . . .
. . . . . . . . . . . . . . . . . . . . . . . . .
- INERT SEP As required. . . . . . . . . . . . . . . . . . . . . . .
- AIRFRAME DE ICE OFF. . . . . . . . . . . . . . . . . . . . . .
- PROP DE ICE OFF. . . . . . . . . . . . . . . . . . . . . . . . . . .
Continue ►
PIM - DO NOT USE FOR FLIGHT OPERATIONS