MD-80 Flight Manual 麦道80飞行手册 2(113)

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Forward Accessory and Electrical / Electronics Compartments
Two pressurized compartments are located in the forward section of the fuselage. The forward accessory compartment houses electronic and electrical equipment. The compartment is accessible through a plug-type door in the ceiling of the nose-gear wheel well.
The electrical / electronics compartment is located between the nose gear wheel well and the forward lower cargo compartment. The compartment houses the rack-mounted electronic components and is ventilated with exhausted air from the flight compartment. A ground access door for the compartment is located aft of the nose gear wheel well, and an in-flight access door is located in the fight compartment floor behind the Captain’s seat. Both of the forward compartments are equipped with lights. The external doors to the forward accessory and electrical / electronics compartment have door warning lights on the annunciator panel which remain on when the doors are not closed and locked.
Main Gear Wheel Well Accessory Compartments
The main gear wheel wells are located in the lower segment of the fuselage aft of the wing center section. In addition to housing the wheels when retracted, the wells house such hydraulic system components as reservoirs, filters, accumulators, pressure gauges, pumps, and service panels. The inboard wheel well doors can be opened for access to the hydraulic components while the airplane is on the ground.
Aft Accessory Compartments
The aft accessory compartment is located in the tail section of the airplane, aft of the pressure bulkhead. The air conditioning equipment and engine fire extinguishing equipment are installed in the compartment. Access to the compartment is made through the aft cabin door, through the tail cone access door, the aft stairway door, or through the opening with the tail cone removed.
A walkway is provided in the compartment. The walkway is down when the Ventral stairs are retracted. When the Ventral stairs are extended, the walkway is raised for form the ceiling of the stairway area.
The APU compartment is located in the bottom of the aft accessory compartment, immediately aft of the pressure bulkhead. The APU installation is shrouded with a fireproof cover. Servicing access to the APU is provided on the fuselage exterior.
The aft accessory compartment is non-pressurized.

Continental
Rev. 12/01/00 #29 Flight Manual

CARGO AND ACCESSORY COMPARTMENTS
PASSENGER ENTRANCE DOORS AND STAIRS
AND SERVICE DOORS

Passenger Forward Entrance Door and Forward Service Door
The passenger forward entrance door is installed on the left side of the fuselage, and the forward service door is installed on the right side. Either door can be opened from either inside or outside the airplane. The doors swing outward after the hinge has moved inward permitting the doors to move edgewise through the doorway. An evacuation slide is installed on each door. Operating instructions for the door and the slide are stenciled on the door and slide container, respectively. Door warning lights on the annunciator panel will remain on when either door is not closed and locked.
Passenger Forward Entrance Stair
The forward entrance stair is removed from all CAL aircraft.
A mechanical interlock, which is part of the stairwell door latching mechanism, prevents the stairwell door from being opened when the passenger door is locked closed and prevents the passenger door from being locked when the stair door is opened.
Forward Stairwell Door Latch Inspection Viewer
An inspection viewer is installed in the left side of the floor beam immediately forward of the stairwell, in the electrical / electronics compartment.
The viewer is used to determine that the stairwell door is latched if the STAIR DOOR light on the annunciator panel and / or the STAIR DOOR OPEN light on the forward attendant’s panel inadvertently come on. The viewer installation consists of a small door in the floor beam, and a light switch to turn on the stair lights. Access to the electrical / electronics compartment is gained through the door in the floor of the flight compartment, just aft of the Captain’s seat or through the external electrical / electronics access door aft of the nose gear well. (See illustration title Forward Stairwell Door Latch Inspection Viewer.)

Continental
Rev. 12/01/00 #29 Flight Manual
Passenger Aft Entrance Door
The passenger aft entrance door is mounted on the aft pressure bulkhead and hinged on the right side to swing forward against the lavatory wall. A viewing window is installed in the door handle recess to allow inspection of the stairway area with the door closed. The door provides access to the forward end of the passenger aft stair passageway, where the internal stairway control panel is located. The aft flight attendant’s seat is attached to the door and automatically folds into a recess in the door when not in use. The seat bottom must be folded into the recess when the door is opened. A barrier strap is installed to be placed across the aisle forward of the door for takeoff and landing, to preclude passenger interference when opening the door. A hold open latch is installed on the right side of the aisle to hold door in the open position.
　
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