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7452, 7455, 7457 and subsequent
Passenger Door -- EICAS Indications 06--20--18
GALLEY/SERVICE DOOR
Figure 06--30--1 Airplanes 7002 to 7125
Interior Galley/Service Door 06--30--2
Figure 06--30--1 Airplanes 7126, 7128 and subsequent
Interior Galley/Service Door 06--30--3
Figure 06--30--2 Exterior Galley/Service Door 06--30--4
Figure 06--30--3 Service Door -- EICAS Indications 06--30--7
AVIONICS BAY DOOR
Figure 06--40--1 Avionic Bay Door 06--40--2
Figure 06--40--2 Avionic Bay Door -- EICAS Indications 06--40--4
CARGO BAY DOORS
Figure 06--50--1 Aft Cargo Bay Door 06--50--2
Figure 06--50--2 Cargo Compartment Door
EICAS Indications 06--50--3
AFT EQUIPMENT BAY DOOR
Figure 06--60--1 Aft Equipment Compartment Door 06--60--2
EMERGENCY EXITS
Figure 06--70--1 Cockpit Escape Hatch 06--70--2
Figure 06--70--2 Overwing Emergency Exits 06--70--5
Figure 06--70--3 Emergency Doors EICAS Indications 06--70--7
REV 56, Jan 31/03
Vol. 1 06--00--4
DOORS
Table of Contents
Flight Crew Operating Manual MASTER
CSP A--013
THIS PAGE INTENTIONALLY LEFT BLANK
Vol. 1 06--10--1
REV 56, Jan 31/03
DOORS
Introduction
Flight Crew Operating Manual
CSP A--013
MASTER
1. INTRODUCTION
The aircraft has the following fuselage doors:
S Passenger door (type I exit)
S Galley service door (type I exit)
S Two overwing emergency exits (type III exit)
S Flight compartment overhead escape hatch
S Cargo door
S Avionics compartment door
S Aft equipment compartment door.
The passenger door and the galley service door can be operated from inside or outside of
the aircraft and can also be used for emergency evacuation. The flight compartment escape
hatch and the overwing emergency exits can also be operated from inside or outside of the
aircraft. The cargo door, aft equipment compartment door and the avionics compartment
door can only be operated from outside the aircraft. All doors, except the aft equipment
compartment door and the cockpit overhead escape hatch are monitored by the proximity
sensing electronic unit (PSEU).
The PSEU provides door status information for display on the EICAS.
The doors aural and visual indication system is triggered by signals received from position
sensors and switches. Inputs from the position sensors and switches are processed by the
proximity sensing electronic unit (PSEU) and transmitted to the EICAS. Door warning and
caution messages are displayed on the EICAS primary page and door status is displayed on
the DOORS synoptic page.
REV 56, Jan 31/03
Vol. 1 06--10--2
DOORS
Introduction
Flight Crew Operating Manual MASTER
CSP A--013
Doors --- General
Figure 06---10---1
GALLEY
SERVICE
DOOR
COCKPIT
ESCAPE
HATCH
PASSENGER
DOOR
AVIONICS
BAY DOOR
RH OVERWING
EMERGENCY EXIT
LH OVERWING
EMERGENCY EXIT
CARGO
BAY DOOR
AFT EQUIPMENT
BAY DOOR
Vol. 1 06--10--3
REV 56, Jan 31/03
DOORS
Introduction
Flight Crew Operating Manual
CSP A--013
MASTER
A. System Circuit Breakers
SYSTEM SUB--SYSTEM CB NAME BUS BAR CB
PANEL
CB
LOCATION
NOTES
Doors Proximity
Sensing DOOR IND DC
ESSENTIAL 4 B12
REV 56, Jan 31/03
Vol. 1 06--10--4
DOORS
Introduction
Flight Crew Operating Manual MASTER
CSP A--013
THIS PAGE INTENTIONALLY LEFT BLANK
Vol. 1 06--20--1
REV 56, Jan 31/03
DOORS
Passenger Door
Flight Crew Operating Manual
CSP A--013
MASTER
1. PASSENGER DOOR
The passenger door is located at the forward left side of the fuselage and is the main
entrance and exit to the cabin area.
The passenger door incorporates integral stairs with a retractable lower step and folding
handrails. The door is hinged at the cabin floor level and opens outward. A
counter--balance mechanism with gas springs is used to take the weight of the door and to
dampen the door movement At the fully open position, the door rests on a support wheel.
Handrails are provided to assist passengers in boarding and disembarking. Mechanical
linkages raise the handrails when the door is opened and collapse them when the door is
closed. When a jetway is used, the handrails must be collapsed. Collapsing of the handrails
is done by removing the forward and aft handrail quick--release pins (Refer to Lowering the
Stair Handrails).
Closing the passenger door from inside the aircraft is normally accomplished using the
power assist system which is controlled from a DOOR ASSIST switchlight on the forward
　
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