Pilot's Operating Handbook
Supplement 64
Stick shaker
Edition 1 - May 29, 2017
Rev. 1
Page 9.64.10
7.14 - Miscellaneous equipment
Sta
ll warning system
The airplane is equipped with an electrically deiced stall sensor in the leading edge of
the right wing. This sensor fitted with a vane is electrically connected to an audible
warning. The vane senses the change in airflow over the wing and operates the
warning unit, which produces an alert over the alarm speaker. This warning tone
begins between 5 and 10 knots above the stall in all configurations.
The stall warning system should be checked during the preflight inspection by
momentarily turning on the SOURCE selector and by manipulating the vane in the
wing.
>> Before v15.11 GARMIN software (Pre-MOD70-0407-00D)
The system is operational if a continous tone (low-pitched sound) is heard on the
alarms speaker and the stick shaker simultaneously vibrates.
>> After v15.11 GARMIN software (Post-MOD70-0407-00D)
The system is operational if a stall aural warning alert is heard on the alarms speaker
and the stick shaker simultaneously vibrates.
>> All
● NOTE ●
The audible stall warning may be altered by severe or prolonged icing.
●
SECTION 8
Handling, servicing and maintenance
Operation of the stick shaker does not change the basic handling, servicing and
maintenance of the airplane described in section 8 Handling, servicing and
maintenance of the basic POH.
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