A320飞机维护手册 AMM EQUIPMENT/FURNISHINGS 设备2(66)

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 1. General_______ 
R  Dividers are installed to divide the utility areas and the passenger seating 
R  areas in the cabin. 
R  2. Component Location__________________ 
R  (Ref. Fig. 001)
 3. Component Description_____________________ 
R 
R  A. Curtains 
R  Curtains divide the utility areas from the passenger seating area. 
R  The curtains hang on hooks which slide in light alloy rails. Brackets 
R  attach the rails to the galleys, lavatories, stowage compartments and/or 
R  the overhead stowage compartments. 
R  B. Partitions (if installed) 
R  The partitions can be installed in the cabin between FR20 and FR66. 
R  Special fittings attach the partitions to the seat tracks of the cabin 
R  and on top to the overhead stowage compartment or the ceiling. 
R  Each partition is made of a composite structure material and has a 
R  decorative cover. The edges of the partitions have a light alloy profile. 
R  The supports which hold the attach fittings are bonded into the composite 
R  structure of the partition. 
R  C. Movable Class Divider (if installed) 
R  The movable class divider has a center part and two lateral parts with 
R  curtains. You can relocate the parts in the cabin without tools quickly. 
R  (1) Center part 
R  A quick release mechanism attaches the beam of the center part on top 
R  of the overhead stowage compartments. 
R  Curtains are attached to the curtain rail of the beam with hocks. 
R  (2) Lateral part 
R  A quick release mechanism attaches each of the lateral supporting 
R  beams to the connection panels installed in the lower part of the 
R  overhead stowage compartments. 
R  Curtains are attached to the curtain rail of the beam with hocks. 
R  No Smoking/Fasten Seat Belt signs are installed in each supporting 
R  beam and electrically connected to the aircraft system via the 
R  connection panels. 
R  The connection panels are located at each seat row between frames 22 
R  and 64 except in the area of the emergency exits.

 EFF : ALL
25-26-00Page 1
May 01/98

R R  Dividers - Component Location Figure 001
 EFF :  ALL  25-26-00 Page 2 May 01/98
 CES 

 

 CURTAINS - REMOVAL/INSTALLATION
_______________________________
 TASK 25-26-41-000-001
 Removal of the Forward Curtain Rail
 1.
 Reason for the Job

__________________
 Self Explanatory

 2.
 Job Set-up Information

______________________
 A. Referenced Information
 -------------------------------------------------------------------------------
REFERENCE  DESIGNATION
 -------------------------------------------------------------------------------
23-73-22-000-001  Removal of the Attendant Indication Panel 320RH
 24-42-00-861-001  Energize the Ground Service Network from the External Power
 25-26-41-000-013  Removal of the Curtains
R **ON A/C 001-049, 101-105, 201-210,
 25-26-41-991-001-B Fig. 401
 **ON A/C 151-199,

 25-26-41-991-001-A Fig. 401A
 **ON A/C 301-399,

 25-26-41-991-001-C Fig. 401B
 **ON A/C ALL

 3. Job Set-up
__________
 Subtask 25-26-41-861-051

 A. Energize the ground service network
 (Ref. TASK 24-42-00-861-001)

 EFF : ALL
25-26-41Page 401

 Subtask 25-26-41-010-074
 B. Get Access
 (1) Remove the FWD Curtains (Ref. TASK 25-26-41-000-013)
 4. Procedure
_________ R **ON A/C 001-049, 101-105, 201-210,
 Subtask 25-26-41-020-050
 A. Removal of the Curtain Rail:
 (Ref. Fig. 401/TASK 25-26-41-991-001-B)

 (1)
 Remove the attendant indication panel 320RH1 (Ref. TASK 23-73-22-000-001).

 (2)
 Remove the end panel(s) (7) of the overhead stowage compartments.

 (a)
 Open the door(s) (3) of the overhead stowage compartment(s) on the left and/or the right side.

 (b)
 Remove the screw(s) (5) and the washer(s) (6).

 (c)
 Pull the end panel(s) (7) to the centerline of the aircraft until they are free of the holders (4) and remove them.
　
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