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FlightSafety LEARJET 45 - Page 375

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In addition, both PFD’s will indicate 40 knots
and the Vspeed digits will be replaced by the
Low Speed Awareness cues which appear on
the airspeed tape during the test. A satisfac-
tory test is indicated when:
Master Caution Chime and Lights.
“L AOA HT FAIL” amber CAS message
illuminates.
Low Speed Awareness (LSA) Indicator
rises to the airspeed pointer on the left
PFD as the AOA pointer (if installed)
sweeps the indicator scale.
Stick shaker activates when LSA reaches
the indicated airspeed pointer.
Aural master warning tone sounds fol-
lowed by a “STALL” voice message.
The above test takes approximately 5 seconds
to complete, and after a slight pause, the same
sequence occurs for the right side if the test
button is held depressed. When the right side
is testing, a “R AOA HT FAIL” CAS message
will be displayed.
STALL WARNING ELECTRICAL
POWER
The left and right stall warning systems are
power by the L and R Essential Busses re-
spectively. The circuits are protected by the L
STALL WARN and R STALL WARN circuit
breakers located in the FLIGHT group on the
pilot’s and copilot’s circuit breaker panels.
Since the left and right stall warning systems
do not have on-off switches, the correspond-
ing circuit breaker would have to be pulled to
turn off a malfunctioning system.
15-32
FOR TRAINING PURPOSES ONLY
LEARJET 45 PILOT TRAINING MANUAL
FlightSafety
international

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