(b)
 On the electrical test plug, push the pushbutton switch, the light comes on.

 (c)
 Connect the voltmeter to the electrical test plug and make sure that the voltage is 115VAC.

 (d)
 Disconnect the voltmeter.

 (e)
 Release the pushbutton switch, the light goes off.

 (f)
 Disconnect the tool from the CAPT outlet (5NA).

 (2)
 On the F/O hand-microphone panel 16VU:

 (a)
 Connect the TBD (99D24003000) to the F/O outlet (4NA).

 (b)
 On the electrical test plug, push the pushbutton switch, the light comes on.

 (c)
 Connect the voltmeter to the electrical test plug and make sure that the voltage is 115VAC.

 (d)
 Disconnect the voltmeter.

 (e)
 Release the pushbutton switch, the light goes off.

 (f)
 Disconnect the tool from the F/O outlet (4NA).

 5. Close-up
________ Subtask 25-18-51-410-050
 A. Close Access
 (1)
 Make sure that the work area is clean and clear of tool(s) and other items.

 (2)
 Close the access door 811.

 (3) Remove the access platform(s). Subtask 25-18-51-862-050
 B. De-energize the ground service network
 (Ref. TASK 24-42-00-862-001).

 PASSENGER COMPARTMENT - DESCRIPTION AND OPERATION_________________________________________________
 1. General_______ The passenger compartment is in the upper fuselage section. It is between the partition on FR12/13 of the flight compartment and the aft pressure bulkhead on FR70.
 2. Component Location__________________ 
R  **ON A/C 001-049, 101-105,
 (Ref. Fig. 001) 
R  **ON A/C 051-099,
 (Ref. Fig. 001A) 
R  **ON A/C 151-199,
 (Ref. Fig. 001B) 
R  **ON A/C 201-210, 
R  (Ref. Fig. 001C)
 **ON A/C ALL
 3. System Description__________________
 A. The cabin is divided into utility areas and seating areas. The passenger/crew doors and emergency exits are also included in the cabin area. The utility areas are adjacent to the cabin entrances. The passenger seating area is between the forward utility area and the aft utility area. Partitions and curtains divide the utility areas from the seating areas.
 (1) Seating area The equipment and furnishings which are installed in the passenger seating area are: - Passenger seats (Ref. 25-21-00). - Cabin attendant seats (Ref. 25-22-00).

 EFF : ALL

25-20-00Page 1

 Cabin Layout GW1/CES(MU1) Figure 001 
R  EFF :  001-049, 101-105,  25-20-00 Page 2 May 01/05
 CES 

R R  Cabin Layout WH1 Figure 001A 
R  EFF :  051-099,  25-20-00 Page 3 May 01/05
 CES 

R  Cabin Layout - GW05/CES Figure 001B 
R  EFF :  151-199,  25-20-00 Page 4 May 01/05
 CES 

R  Cabin Layout - MU1(CES01) Figure 001C 
R  EFF :  201-210,  25-20-00 Page 5 May 01/05
 CES 

 -Linings and furnishings that cover the compartment structure (Ref. 25-23-00).
 -Overhead stowage compartments are for stowage of passenger carry-on baggage and other equipment (Ref. 25-24-00).
 -Passenger service/information units (Ref. 25-25-00).
 -Textile floor coverings (Ref. 25-28-00).
 (2)
 Utility area The equipment and furnishings which are installed in the utility areas are:

 -Cabin attendant seats (Ref. 25-22-00).
 -Passenger Service Units (PSUs) are installed at passenger and attendant locations throughout the cabin (Ref. 25-25-00).
 -Curtains and partitions are used to divide the utility areas and the seating sections (Ref. 25-26-00).
 -Ancillary equipment has different stowage units (Ref. 25-27-00).
 -Nontextile floor coverings (Ref. 25-28-00).
 -Vacuum cleaner sockets give electrical power to clean the cabin interior (Ref. 25-29-00).
 -Galleys (Ref. 25-30-00).
 -Lavatories (Ref. 25-40-00).

 (3)
 Additional equipment Additional equipment also installed in the cabin is:

 -Emergency escape slide/slide rafts (Ref. 25-62-00).
 -First aid equipment (Ref. 25-64-00).
 -Miscellaneous emergency equipment (Ref. 25-65-00).
 -Flotation and survival Equipment (Ref. 25-66-00).
 EFF : ALL

25-20-00Page 6

 PASSENGER COMPARTMENT SEATS - DESCRIPTION AND OPERATION
　
中國航空網(wǎng) www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機維護手冊 AMM EQUIPMENT/FURNISHINGS 設(shè)備1(134)