DA 40 AFM
Airplane
Description
Doc. # 6.01.01-E
Rev. 8
01-Dec-2010
Page 7 - 45
Pitot Heating
The Pitot probe, which provides measurement for the Pitot-static system, is electrically
heated. The heating is activated with a switch (PITOT) on the row of switches on the
instrument panel. The temperature is automatically kept constant by means of a thermal
switch on the Pitot probe, and as an additional safety measure a thermal fuse is built in.
If this thermal fuse is activated, the Pitot heating can no longer be switched on, and the
Pitot heating caution will be displayed. In this case the system should be serviced.
NOTE
The Pitot heating caution will also be displayed whenever the
Pitot heating system is switched OFF.
Summary of Contents for DA 40
Page 1: ......
Page 37: ...DA 40 AFM General Doc 6 01 01 E Rev 8 01 Dec 2010 Page 1 21 1 7 THREE VIEW DRAWING ...
Page 182: ...Performance DA 40 AFM Page 5 12 Rev 8 01 Dec 2010 Doc 6 01 01 E ...
Page 184: ...Performance DA 40 AFM Page 5 14 Rev 8 01 Dec 2010 Doc 6 01 01 E ...
Page 186: ...Performance DA 40 AFM Page 5 16 Rev 8 01 Dec 2010 Doc 6 01 01 E ...
Page 190: ...Performance DA 40 AFM Page 5 20 Rev 8 01 Dec 2010 Doc 6 01 01 E ...
Page 288: ...Handling DA 40 AFM Page 8 6 Rev 8 01 Dec 2010 Doc 6 01 01 E ...