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GF0310_023
FDR/CAIMS Event Button
Used to store information in
Line Replaceable Units
(LRUs), which report to CAIMS.
Landing Gear Control Panel
NOSE STEER LDG GEAR
HORN PILOT
EVENT
MUTED
AURAL AND VISUAL WARNINGS
Flight Crew Operating Manual Rev 2A, Apr 11, 2005
CSP 700−5000−6
Volume 2
03−10−22
FLIGHT DATA RECORDER
EICAS channels aircraft systems data (including altitude, airspeed, heading, acceleration and radio
communications events) to the Flight Data Recorder (FDR). DAU 4B gathers sensor data for
transmission to the FDR.
DAU 4 is fully selfmonitoring
and provides CAS messages in the event of a failure. If DAU 4B
channel fails, FDR information is not available.
To record an additional event, in the FDR push the PILOT EVENT button on landing gear control
panel, located on the pedestal. Pushing the PILOT EVENT will also encode the Central Aircraft
Information Maintenance System (CAIMS).
GF0310_024
Landing Gear Control Panel
FDR/CAIMS
Event Button
NOSE STEER LDG GEAR
HORN PILOT
EVENT
MUTED
STALL WARNING
Warning of an impending stall is provided by independent stall protection systems. Both systems are
energized in flight and deactivated on the ground through air/ground logic. The flight displays indicate
airplane approach to stall speed by low speed cues (red band) and a TBD VS indicator on the
primary flight displays (PFDs) airspeed tape.
Stall warnings are provided by an aural “STALL”, a STALL icon appears on the PFD and vibration of
both control columns. If the airplane angleofattack
continues to increase, a stick pusher then
pushes the control column forward to prevent further development of a stall. For more information
refer to Chapter 10, FLIGHT CONTROLS.
AURAL AND VISUAL WARNINGS
Rev 2A, Apr 11, 2005 Flight Crew Operating Manual
CSP 700−5000−6
Volume 2
03−10−23
TAKE-OFF CONFIGURATION WARNINGS
Takeoff
configuration warnings are armed when the airplane is on the ground and both engines are
accelerated towards takeoff
thrust (throttle position ³ 30°). A voice warning, EICAS warning
message, and both MASTER WARNING lights come on for any of the following:
Condition Voice Message EICAS Message
Aileron trim outside of takeoff
range
“NO TAKEOFF” CONFIG AIL TRIM
Parking brake on during takeoff
“NO TAKEOFF” PARK BRAKE ON
Rudder trim outside of takeoff
range
“NO TAKEOFF” CONFIG RUD TRIM
Flaps not in takeoff
position “NO TAKEOFF” CONFIG SLATS/FLAPS
Spoilers not in takeoff
position “NO TAKEOFF” CONFIG SPOILERS
Horizontal stabilizer outside of
takeoff
range (“green band”)
“NO TAKEOFF” CONFIG STAB TRIM
All configuration warning indications are cancelled when the configuration error is corrected, or the
airplane is airborne or either thrust lever is retarded.
Note: NO TAKEOFF advisory message will appear during taxi, prior to advancing throttles.
AURAL AND VISUAL WARNINGS
Flight Crew Operating Manual Rev 2A, Apr 11, 2005
CSP 700−5000−6
Volume 2
03−10−24
LANDING CONFIGURATION WARNING
The “GEAR” aural will sound if any gear is not down and locked and the airplane is below 16,500 feet
and:
· The radio altitude is less than 1,000 feet AGL and the descent rate is more than 400 feet per
minute.
OR
· The radio altitude is less than 500 feet AGL and either throttle is below 25° throttle lever angle
and the flap position is 30°.
OR
· The radio altitude is less than 500 feet AGL and both throttles are below 25° throttle angle and
the flap posiion is not at 30°.
NOTE
The “GEAR” aural can not be muted during any of these conditions.
The “Too low gear” (EGPWS) aural warning is heard if any landing gear is not down and locked with
the radio altitude less than 500 feet AGL and the indicated airspeed at less than 190 knots.
If neither radio altimeter is valid, the “GEAR” aural will sound if any gear is not down and locked and
the airplane is below 16,500 feet. The landing gear horn may be muted by pressing the mute hornn
swith/ light on the landing gear control panel. With both thrust levers at IDLE, (less than three
degrees throttle lever angle) the horn cannot be muted.
AURAL AND VISUAL WARNINGS
Rev 2A, Apr 11, 2005 Flight Crew Operating Manual
CSP 700−5000−6
Volume 2
03−10−25
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