Daher TBM 930 - Heating of Pitots and Stall Warning Sensor (PITOT L HTR and PITOT R & STALL HTR); Turbine Air Inlet Protection

Pilot's Operating Handbook
Section 7
Description
Edition 1 - January 15, 2018
Rev. 2
Page 7.13.3
Heating of pitots and stall warning sensor (PITOT L HTR and
PIT
OT R & STALL HTR)
The two pitots, which supply ADCs, the airspeed indicator and the stall warning
sensor are electrically heated. This deice equipment must be used even during flight
into non-icing conditions.
The system condition messages PITOT NO HT L or PITOT NO HT R ,
PITOT HT ON L or PITOT HT ON R , STALL HEAT ON or
STALL NO HEAT are displayed on the MFD CAS window. Refer to the GARMIN
Pilot's Guide for further details.
● NOTE ●
Correct operation of the audible stall warning may be altered by severe or
prolonged icing.
●
Turbine air inlet protection
Operation and description are set forth in chapter 7.6 paragraph Engine air inlet.
PIM - DO NOT USE FOR FLIGHT OPERATIONS