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SWITCH PANEL
AFT EQUIPMENT
BAY DOOR
REV 1
AIRPLANE GENERAL
Volume 2 Flight Crew Operating Manual Sep 13/2004
01-05-10 CSP 100-6 REV 1
SERVICE DOORS (Cont)
COMPONENTS AND OPERATION
GROUND-POWER DOOR
The ground-power door is located on the right side of the aircraft in the aft wing-fuselage fairing, and allows access to the
service panel for ground power supply.
OXYGEN FILL/INDICATOR DOOR
The oxygen fill/indicator door is located on the right side of the fuselage at the aft edge of the wing, and allows access for
the oxygen indicator and servicing.
REFUEL/DEFUEL DOOR
The refuel/defuel door is located in the forward right wing-fuselage fairing, and allows access to the refuel/defuel adapter.
REFUEL/DEFUEL CONTROL PANEL DOOR
The refuel/defuel control panel door is on the right side of the aircraft in the forward wing-fuselage fairing, and allows
access to the computer control panel for refueling and defueling.
LAVATORY WASTE DOOR
The lavatory waste door is located on the right side of the aircraft in the aft wing-fuselage fairing, and allows access to the
lavatory-waste service panel.
COMMUNICATION PANEL DOOR
The communication door is located left of the nose wheel, and allows access to the ground communication panel.
OUTFLOW VALVE DOOR
The outflow valve door is located in the forward right wing-fuselage fairing and allows access to the outflow valve panel.
BATTERY BAY DOOR
The battery bay door is located on the left side of the aircraft in the aft wing-fuselage fairing, and allows access to the aircraft
main batteries.
A proximity sensor on the battery access door prompts BATTERY BAY DOOR (C) CAS message if the door is not closed.
GROUND AIR SERVICING DOOR
The ground-air servicing door is located right of the centerline toward the rear of the fuselage, and allows access to the
ground air servicing connection.
REV 1
AIRPLANE GENERAL
Sep 13/2004 Flight Crew Operating Manual Volume 2
REV 1 CSP 100-6 01-05-11
SERVICE DOORS (Cont)
AFT EQUIPMENT BAY DOOR
The aft equipment bay door is located on the centerline of the aircraft at the rear of the fuselage. The door is hinged in front
and opens downward. The door has a lever-type latch mechanism. A support strut on the door can be connected to the fairing
bracket to stabilize the door in the open position. The strut must be disconnected from the fairing bracket to close the
door.
AFT EQUIPMENT BAY DOOR ANNUNCIATION
An AFT EQPT BAY DOOR (C) CAS message is displayed if the aft equipment bay door is not closed.
CFO0105002_001
HINGES
LATCH
LEVER
FAIRING
BRACKET
STRUT
CLIP
REV 1
AIRPLANE GENERAL
Volume 2 Flight Crew Operating Manual Feb 22/2006
01-05-12 CSP 100-6 REV 5
DOOR WARNING SYSTEM
DESCRIPTION
The door warning system monitors the position of the following doors while the aircraft is on the ground or in flight:
- Passenger door
- Emergency exit hatch
- Cargo bay door
- Aft equipment bay door
- Battery bay door
COMPONENTS AND DESCRIPTION
A magnet with an electronic proximity sensor is mounted at each door. The proximity sensors interface with the proximity
sensor electronic unit (PSEU), data concentrator unit (DCU), and the multifunction display. The flight crew receives a single
chime and a visual CAS annunciation if a door is not in the correct position under specific conditions. For the specific
conditions, refer to the annunciation description for each door in this section.
On the ground the CAS displays EMERGENCY EXIT (C) and other door warnings in amber. However, if the left engine
is set to RUN, the PASSENGER DOOR (C) and CARGO DOOR (C) will also be illuminated. In flight, the door warnings
on the CAS are displayed in amber.
1
PROXIMITY-SENSOR ELECTRONIC UNIT
(PSEU)
DATA
CONCENTRATOR
UNIT
(DCU)
GROUND IN FLIGHT
PASSENGER
DOOR
HANDLE
EMERGENCY
EXIT HATCH
PASSENGER
DOOR
BAGGAGE
DOOR
BAGGAGE
DOOR
HANDLE
AFT
EQUIPMENT
COMPARTMENT
DOOR
BATTERY
BAY
DOOR
PASSENGER
DOOR
LOCK
AFT EQPT BAY DOOR
CARGO DOOR
PASSENGER DOOR
BATTERY BAY DOOR
EMERGENCY EXIT
PASSENGER DOOR
CARGO DOOR
EMERGENCY EXIT
AFT EQPT BAY DOOR
BATTERY BAY DOOR
REV 5
AIRPLANE GENERAL
Sep 14/2005 Flight Crew Operating Manual Volume 2
REV 4 CSP 100-6 01-05-13
EICAS MESSAGES
The following door and exit messages are shown on the EICAS. In the table below are the messages, meanings, inhibits,
and aural warnings along with a brief explanation of each message.
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Bombardier 300 airplane general(11)
