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FGF0310_006
Pilot Event Marker (located on the landing gear control panel).

FDR/CAIMS Event Button
Used to store information in Line Replaceable Units (LRUs), which report to CAIMS.
GF0310_023

Landing Gear Control Panel

Volume 2 Flight Crew Operating Manual Rev 2A, Apr 11, 2005

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 self-monitoring 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).

FDR/CAIMS
Event Button

GF0310_024
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 angle-of-attack 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.
Rev 2A, Apr 11, 2005 Flight Crew Operating Manual Volume 2

TAKE-OFF CONFIGURATION WARNINGS
Take-off configuration warnings are armed when the airplane is on the ground and both engines are accelerated towards take-off thrust (throttle position ≥ 30°). A voice warning, EICAS warning message, and both MASTER WARNING lights come on for any of the following:

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.
Volume 2 Flight Crew Operating Manual Rev 2A, Apr 11, 2005

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°.
　
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