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1. STALL PROTECTION (CONT'D)
A. Stall Protection System – First Flight of the Day (Cont’d)
Airplanes 5301 to 5560 NOT incorporating Service Bulletin 604–27–005:
(1) Stabilizer trim switch.............................................Select to NOSE DN and hold until
trim is 0 units.
(2) FLIGHT CONTROLS page...................................Select
(3) STALL PROT, PUSHER switches........................Select to ON.
(4) SPS TEST, L and R switches...............................Select TEST and hold.
Check STALL FAIL and ALT
COMP FAIL caution
messages come on.
(5) SPS TEST INDICATORs .....................................Check during test:
• IGNITION A, B and CONT
ON lights come on.
• IGNITION A and B advisory
messages come on.
within the yellow region:
• Stick shakers are activated.
within the red region:
• Stick pusher is activated.
• STALL lights flash.
• Stall aural warning sounds.
While in stick pusher mode:
(a) Pilot’s AP/SP DISC switch.............................Press Stick pusher is de-activated,
(b) Pilot’s AP/SP DISC switch.........................Release Stick pusher is re-activated.
(c) Copilot’s AP/SP DISC switch.........................Press Stick pusher is de-activated.
NOTE
During copilot’s AP/SP DISC test, the control column will
take several seconds to go back to neutral position.
Copilot should pull (override) control column and note
diminished feel force loads while pressing the AP/SP
DISC switch.
(d) Copilot’s AP/SP DISC switch.....................Release Stick pusher is re-activated.
(e) FLIGHT CONTROLS page...........................Check right elevator surface pointer
indicates full travel or copilot
control column is against
forward stop.
NORMAL PROCEDURES
Stall Protection
04−18−3
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
1. STALL PROTECTION (CONT'D)
A. Stall Protection System – First Flight of the Day (Cont’d)
(f) G SWITCH.................................................... Select TEST and hold.
Stick pusher is de-activated.
(g) G SWITCH.................................................Release Stick pusher is re-activated.
(6) SPS TEST, L and R switches............................Release Check the following:
• STALL FAIL and ALT
COMP FAIL caution
messages out.
• Stick pusher de-activated.
• Stick shakers de-activated.
• IGNITION A, B and CONT
ON lights out.
• IGNITION A and B advisory
messages out.
• STALL lights out.
• Stall aural warning stops.
NORMAL PROCEDURES
Stall Protection
04−18−4
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
1. AURAL/VISUAL WARNING SYSTEM
A. Lamp Test – First Flight of the Day
(1) LAMP TEST switch ..............................................Select to 1 and hold.
Check all switch/lights come
on.
Release switch and check all
switch/lights go out.
(2) LAMP TEST switch ..............................................Select to 2 and hold.
Check all switch/lights come
on.
Release switch and check all
switch/lights go out.
B. Aural Warning System – First Flight of the Day
(1) AURAL WARN TEST switch ................................Select to 1 and release.
Check that all dedicated
tones, chimes and voice
messages within data
concentrator unit 1 come on.
(2) AURAL WARN TEST switch ................................Select to 2 and release.
Check that all dedicated
tones, chimes and voice
messages within data
concentrator unit 2 come on.
NOTE
Re-selection of the TEST switch during the test will cancel the aural
messages.
C. Before Take-Off
(1) Crew alerting system (CAS) .................................Check that T/O CONFIG OK advisory
(green) message on.
NOTE
Both EICAS primary and secondary displays must be selected on.
(2) EICAS page..........................................................Check that stabilizer trim setting is in
the correct position (refer to
FLIGHT CONTROLS – Before
Take-Off in this chapter).
D. Before Landing
NOTE
Both EICAS primary and secondary displays must be selected on.
(1) PRI page ..............................................................Check that stabilizer trim setting is in
the correct range.
NORMAL PROCEDURES
Aural/Visual Warning System
04−19−1
　
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