In AUTO mode, when ice is detected, all the ice protection systems are
automatically activated – see Figure 7.14.2, and ICE DETECTED is displayed in
the CAS window.
Figure 7.14.2 - DE ICE SYSTEM Panel – AUTO Mode with Ice Detected
C4300001AAABMA8100
ON
DE ICE SYSTEM
A I R F R A M E
D E I C E
D E I C E
P R O P
W I N D
S H I E L D
I N E R T
S E P
P I T O T L / R &
S T A L L H T R
I C E
L I G H T
AUTO
ON
Pilot action is required to revert the system in MAN mode by pressing the DE ICE
SYSTEM mode switch. When
MAN mode is selected, all deicing systems turn on
– see
Figure 7.14.3.
In MAN mode, all
the ice protection systems can be activated/deactivated
individually.
Figure 7.14.3 - DE ICE SYSTEM Panel – MAN Mode Activated
C4300001AAABMA8200
ON
DE ICE SYSTEM
A I R F R A M E
D E I C E
D E I C E
P R O P
W I N D
S H I E L D
I N E R T
S E P
P I T O T L / R &
S T A L L H T R
I C E
L I G H T
MAN
ON
When icing conditions are no longer detected by the ice detector for 60 seconds
after the last detection, NO ICE DETECTED is displayed in the CAS window and
the system may be
reverted in AUTO mode by pressing the DE ICE SYSTEM
mode switch. Then all the ice protection systems turn off.
ICE DETECTION FAIL is displayed in the CAS window in the following cases:
Section 7
Description
Pilot's Information Manual
PIM TBM 960 - Edition 0
Rev. 00
Page 7.14.2
PIM - DO NOT USE FOR FLIGHT OPERATIONS
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