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DOOR HANDLE RECESS
PUSH TRIGGER
OUTER HANDLE
CARGO DOOR OPEN
STOWED POSITION
GF0110_043
The latch mechanism consists of inner and outer handles directly coupled together and mounted on
the forward and aft sides of the door. The handle assembly contains a trigger lock which holds the
handle in the stowed position. The door is latched when the exterior handle is rotated to engage latch
pins and locked when the handle is stowed and latched in its housing recess.
AIRPLANE GENERAL
Flight Crew Operating Manual REV 51, Aug 14, 2006
CSP 700−6
Volume 2
01−10−58
BAGGAGE COMPARTMENT DOOR (CONT'D)
A vent door is located in the upper portion of the door and will not close until the door is fully closed
and the handle stowed in the locked position.
VENT DOOR/SEAL
INTERIOR
DOOR HANDLE
DETENT BUTTON
GF0110_044
Baggage Door Operation
CLOSING THE BAGGAGE DOOR EXTERNALLY − Rotate the outer handle 90 degrees to latch
the door. Push the handle into the recessed housing until the trigger button is latched into the
trigger mechanism.
CLOSING THE BAGGAGE DOOR INTERNALLY − Rotate the inner handle 90 degrees counter
clockwise to latch the door. Pull the handle until the outer handle trigger latches into the trigger
mechanism and the handle is stowed into the recessed housing.
OPENING THE BAGGAGE DOOR EXTERNALLY − Press the trigger button to release and eject
the outer handle from the recessed housing. Rotate the handle 90 degrees counter clockwise to
unlatch and open the door.
OPENING THE BAGGAGE DOOR INTERNALLY − Press the release button on the inside handle
to unlock the handle from the trigger. Rotate the handle 90 degrees clockwise to open the door.
Baggage Door Indication
Visual indication of a locked condition is the baggage door secured in position and the exterior
handle stowed and locked in the handle recess.
AIRPLANE GENERAL
REV 51, Aug 14, 2006 Flight Crew Operating Manual
CSP 700−6
Volume 2
01−10−59
DOOR INDICATION AND CONTROL
The airplane door position and locked indication is provided to the EICAS by the LGECU. The
LGECU provides data that is used to generate alerts and synoptic displays for the fuselage doors.
Door position information is displayed on the STAT page and message information is displayed on
the PRIMARY page.
The STAT page presents the following doors:
• PASSENGER
• EMERGENCY OVERWING EXIT
• BAGGAGE
• SERVICE DOORS
STAT Page
BAGGAGE DOOR PASSENGER DOOR
OVER WING EMERGENCY EXIT
SERVICE DOOR
ANNUNCIATION
Airplane Door Position Airplane Door Graphic
CLOSED
OPEN
INVALID
GF0110_045
SERVICE DOORS
Passenger Door
The passenger door is monitored by three proximity sensors to determine the locked and handle
stowed position. Proximity sensors (one at each location) are located on the passenger door
forward and aft latch to monitor the “G” latch position. A proximity sensor is mounted in the
passenger door to monitor the outer handle stowed condition.
The sensor information is used by the Landing Gear Electronic Control Unit (LGECU) for door
position and locked indication and sends the results to EICAS for position and locked displays.
Emergency Exit
One proximity sensor is installed at the top of the door position and senses the door in the closed
position.
AIRPLANE GENERAL
Flight Crew Operating Manual REV 51, Aug 14, 2006
CSP 700−6
Volume 2
01−10−60
DOOR INDICATION AND CONTROL (CONT'D)
Baggage Door
Two proximity sensors monitor the door position and provide signals to the LGECU which in turn
provides the EICAS display.
Large Maintenance Doors
Two (optional third) separate large hinged and latched maintenance hatches, are monitored by the
LGECU. Each door is monitored by one proximity sensor to determine the door closed condition.
In each case, the proximity sensor is mounted on the airplane structure and monitors a sensor on
the hatch. The information is used by the LGECU for door position indication.
The LGECU combines the status of the aft equipment bay door with the status of the maintenance
hatches to produce a single EICAS indication.
The maintenance hatches that are monitored are:
• Rear hydraulic system access door.
• Refuel/defuel station door.
• Optional belly fairing stowage access door.
Aft Equipment Bay Door
An electrical proximity sensor provides indication to the EICAS system when the door is properly
closed. The LGECU monitors the signals and provides the input to EICAS.
　
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