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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.
Volume 2 Flight Crew Operating Manual Rev 12, Aug 14, 2006
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
STAT Page
BAGGAGE DOOR PASSENGER DOOR
SERVICE DOOR
ANNUNCIATION
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.
Rev 12, Aug 14, 2006 Flight Crew Operating Manual Volume 2
AIRPLANE GENERAL
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
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