CAUTION
Do not rely on PFD indications when the alternate static source is selected.
Only refer to the standby instrument for airspeed and altitude.
The alternate line has a drain plug located under the instrument panel on the right
side.
Dynamic Pressure Systems
Dynamic pressure is provided
by two heated pitot probes, one installed under
each wing.
The left probe supplies ADC 1 and the standby instrument.
The right probe supplies ADC 2.
Each line has a drain plug located in the root of the wing.
Pitot Heating
Pitot heating is controlled by the PITOT L/R & STALL HTR switch located on the
DE-ICE SYSTEM panel. For further details, refer to
Subsection Ice Protection
Equipment.
CAUTION
To avoid probe overheating while on the ground, do not turn on the pitot heat
for long periods.
Section 7
Description
Pilot's Information Manual
PIM TBM 960 - Edition 0
Rev. 00
Page 7.12.2
PIM - DO NOT USE FOR FLIGHT OPERATIONS
To Next Page
Loading...