Daher TBM 960 - Page 226

MAIN GEN and LOW VOLTAGE 2 / 3
► Continuing
If VMC and non-icing conditions are possible:
11 - ESS
BUS TIE switch ................................................. EMER
The battery supplies only the ESS BUS and
BATT BUS in this configuration
► Land as soon as possible ◄
If use of other than essential 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:
14 - PFD 2 .......................................................... Pull
15 - ADC 2 ......................................................... Pull
16 - TAS ............................................................. Pull
17 - DATA LINK .................................................. Pull
18 - XPDR 2 ....................................................... Pull
Switches / pushbuttons / selector:
19 - DE ICE SYSTEM mode ............................ MAN
All deicing systems turn on
20 - ICE LIGHT ................................................. OFF
Status light in white
21 - INERT SEP ..................................... As required
22 - AIRFRAME DE ICE ................................... OFF
Status light in white
23 - PROP DE ICE ............................................ OFF
Status light in white
Continue ►
Pilot's Information Manual
Section 3A
Abnormal Procedures
PIM TBM 960 - Edition 0
Rev. 00
Page 3A.9.6
PIM - DO NOT USE FOR FLIGHT OPERATIONS