SECTION 7
DESCRIPTION
T B M
850
PILOT’S OPERATING HANDBOOK
Page 7.13.3
Edition 1 -- June 22, 2007
Rev. 13
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.
The system condition messages (”PITOT NO HT L” or ...R”, ”PITOT HT ON L”
or ...R”, ”STALL HEAT ON” or ”STALL NO HEAT”) are displayed on the GDU
1500 MFD CAS window. Refer to the “GARMIN” G1000 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
Summary of Contents for TBM 850
Page 1: ...PILOT S INFORMATION MANUAL TBM 850 Edition 1 PIM DO NOT USE FOR FLIGHT OPERATIONS ...
Page 142: ...3 1 PIM DO NOT USE FOR FLIGHT OPERATIONS ...
Page 146: ...3 2 PIM DO NOT USE FOR FLIGHT OPERATIONS ...
Page 150: ...3 3 PIM DO NOT USE FOR FLIGHT OPERATIONS ...
Page 164: ...3 4 PIM DO NOT USE FOR FLIGHT OPERATIONS ...
Page 170: ...3 5 PIM DO NOT USE FOR FLIGHT OPERATIONS ...
Page 178: ...3 6 PIM DO NOT USE FOR FLIGHT OPERATIONS ...
Page 184: ...3 7 PIM DO NOT USE FOR FLIGHT OPERATIONS ...
Page 196: ...3 8 PIM DO NOT USE FOR FLIGHT OPERATIONS ...
Page 202: ...3 9 PIM DO NOT USE FOR FLIGHT OPERATIONS ...
Page 216: ...3 10 PIM DO NOT USE FOR FLIGHT OPERATIONS ...
Page 228: ...3 11 PIM DO NOT USE FOR FLIGHT OPERATIONS ...
Page 236: ...3 12 PIM DO NOT USE FOR FLIGHT OPERATIONS ...