Continental
Rev. 12/01/00 #29 Flight Manual
FLIGHT COMPARTMENT ARRANGEMENT PILOT EYE LOCATOR
(Left Side Shown - Right Side Opposite) Installed on Some Airplanes
Continental
Rev. 12/01/00 #29 Flight Manual
PILOT SEATS
(Installed on Some Airplanes)
PILOT SEATS
(Installed on Some Airplanes)
Continental
Rev. 12/01/00 #29 Flight Manual
FLIGHT COMPARTMENT DOOR AFT OVERHEAD PANEL
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FORWARD OVERHEAD PANEL GLARESHIELD AND UPPER INSTRUMENT PANEL
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MD806055
CENTER INSTRUMENT PANEL
PEDESTAL (FORWARD)
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Rev. 12/01/00 #29 Flight Manual
PEDESTAL (AFT) CAPTAIN’S INSTRUMENT PANEL
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Rev. 12/01/00 #29 Flight Manual
FIRST OFFICER’S INSTRUMENT PANEL
PASSENGER COMPARTMENT
General
The passenger compartment arrangement, interior furnishings, and equipment are designed to provide a high level of comfort and versatility in
seating arrangements.
Door Dimensions
Approximate door dimensions are as follows:
Passenger Forward Entrance Door (34 x 72 inches)
Forward Service Door (27 x 48 inches)
Overwing Emergency Exit (20 x 36 inches)
Passenger Aft Entrance Door (28 x 72 inches)
Aft Service Door (27 x 60 inches)
Flight Attendants’ Stations
Three flight attendants’ stations are provided with seating for 5 flight attendants. Two flight attendants’ seats are located forward at the left of the flight compartment door in the forward entryway area, two are located aft at the passengers’ aft entrance door, and one is located inboard on the galley G4 wall. A flight attendant’s control panel and oxygen service is installed at each attendant’s station.
Passenger Utilities
Passenger utilities, consisting of reading lights, cold air outlets, attendant call buttons, and oxygen masks, are grouped on panels mounted on the overhead stowage rack lower surface.
Passenger Seats
Each seat is equipped with a seat belt, ashtray, folding utility tray, and literature stowage pocket. All seat backs, except on the outboard seats adjacent to each overwing exit, are adjustable in the recline position by means of a push-button control in the armrest. The seat will return to the normal upright position when the push-button is pressed and no backward force is present.
Continental
Rev. 12/01/00 #29 Flight Manual
Each seat back, except on the outboard seats adjacent to each overwing exit, can be forced by twenty-five pounds of force (approximate) to fold from its normal upright position to lay flush with the seat cushion. The seats may be returned to normal upright position by manually lifting with approximately ten pounds of force.
All armrests, except the one adjacent to the aisle, may be folded up, flush with the seat back. The seat bottom cushions are equipped with hand straps to facilitate use as flotation gear.
Galleys
Four galley units are installed in the passenger compartment. Galleys G1 and G2 are located forward on the right side of the passenger compartment adjacent to the forward service door. Galleys G3 and G4 are located aft on the left side of the passenger compartment near the aft service door. Galleys G1 and G4 are wet galleys and water is supplied from the pressurized potable water system. Galley sinks drain overboard through heated drain masts.
See Airplane General - Interior Arrangement for galley arrangement and location.
Lavatories
Three lavatories are installed in the passenger compartment. One is located forward just aft of the forward passenger entryway and two are located aft on either side of the aft passenger entrance door.
Note: A locked lavatory door can be unlocked from the outside by
inserting a screwdriver or other sharp instrument into a slot on the
occupied sign on the door latch and sliding the sign to the vacant
position.
Water is supplied to the lavatories from the pressurized potable water system. A water shutoff valve is located under the washbasin to shut-off or adjust flow of water to the basin. Hot water is provided by a water heater located under the wash-basin in each lavatory.
The lavatories contain integral waste tanks which are drained through exterior service panels.
Potable Water System
A 47 gallon pressurized potable water tank, located in the fuselage right tunnel just forward of the mid compartment door, supplies water to the wet galleys and lavatories.
The potable water tank is normally pressurized from the airplane air conditioning system. On the ground when the air conditioning system is not operating, the tank can be pressurized from a ground source through the fill valve nipple on the water service panel.
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