Heating Of Pitots And Stall Warning Sensor ("Pitot L Htr" And "Pitot R & Stall Htr"); Turbine Air Inlet Protection - Daher-Socata TBM 900 Pilot's Information Manual

SECTION 7
PILOT'S OPERATING HANDBOOK
DESCRIPTION
HEATING OF PITOTS AND STALL WARNING SENSOR ("PITOT L HTR" AND
"PITOT 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.
"PITOT NO HT L" "PITOT NO HT R" "PITOT HT ON L"
The system condition messages ( or , or
"PITOT HT ON R" "STALL HEAT ON" "STALL NO HEAT"
, or ) are displayed on the GDU 1500
MFD CAS window. Refer to the "GARMIN" G1000 Cockpit Reference 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".
Page 7.13.2 Edition 0 -- October 31, 2013
Rev. 1