tool.
 NOTE : You must use the roller along the hose sections in both

____ directions. The joints of the hose sections must not be aligned with the joints between the panels.
 (4)
 Lift the inboard side of the emergency oxygen container (5) and engage it in the rail (1).

 (5)
 Remove the vinyl bags from the disconnected line ends.

 (6)
 Remove the blanking plugs from the disconnected line ends.

 (7)
 Put the hose (3) in position and fasten the bayonet lock (4).

 (8)
 Make sure that the work area is clean and clear of tool(s) and other items.

 (9)
 Lift the inboard side of the PSU/filler panel aft from the emergency oxygen container (5) and engage it in the rail (7).

 (10) Install the hose section (6) with the PULLEY ASSEMBLY - SEALING CORD tool.
 NOTE : You must use the roller along the hose sections in both
____ directions. The joints of the hose sections must not be aligned with the joints between the panels.
 Subtask 35-22-54-420-051
 B. Installation of the emergency oxygen containers in the Aft Utility Area (5030WR and 5033WR) (Ref. Fig. 402/TASK 35-22-54-991-006, 403/TASK 35-22-54-991-002)
 NOTE : Only the correct P/N of the emergency oxygen container must be
____ installed. The hoses have a specified length for each location in the aircraft und they must not be cut.
 NOTE : The installation procedure is the same for all the emergency
____
 oxygen containers in the aft utility areas.

 (1)
 Do an inspection of the component interface and/or the adjacent area.

 (2)
 Put the oxygen container (5) in position in the rail (1).

 (3)
 Install the hose section (2) with the PULLEY ASSEMBLY - SEALING CORD

 tool.
 NOTE : You must use the roller along the hose sections in both

____ directions. The joints of the hose sections must not be aligned with the joints between the panels.
 (4)
 Lift the inboard side of the emergency oxygen container (5) and engage it in the rail (1).

 (5)
 Remove the vinyl bags from the disconnected line ends.

 (6)
 Remove the blanking plugs from the disconnected line ends.

 (7)
 Put the hose (3) in position and fasten the bayonet lock (4).

 (8)
 Make sure that the work area is clean and clear of tool(s) and other items.

 (9)
 Lift the inboard side of the PSU/filler panel aft from the emergency oxygen container (5) and engage it in the rail (7).

 (10) Install the hose section (6) with the PULLEY ASSEMBLY - SEALING CORD tool.
 NOTE : You must use the roller along the hose sections in both
____ directions. The joints of the hose sections must not be aligned with the joints between the panels.
 Subtask 35-22-54-420-052
 C. Installation of the emergency oxygen containers in the Lavatory D/E
 (5031WR and 5034WR)
 (Ref. Fig. 402/TASK 35-22-54-991-006, 404/TASK 35-22-54-991-003)

 NOTE : Only the correct P/N of the emergency oxygen container must be
____ installed. The hoses have a specified length for each location in the aircraft and they must not be cut.
 (1)
 Do an inspection of the component interface and/or the adjacent area.

 (2)
 Put the oxygen container (5) in position, install the screws (1) and the washers (2).

 (3)
 Remove the vinyl bags from the disconnected line ends.

 (4)
 Remove the blanking plugs from the disconnected line ends.

 (5)
 Put the hose (6) in position and fasten the bayonet lock (7).

 (6)
 Make sure that the work area is clean and clear of tool(s) and other items.

 (7)
 Close the access cover (5) and install the screws (3) and the caps (4).

 Subtask 35-22-54-420-053
 D. Installation of the emergency oxygen containers in the Lavatory A
 (5029WR)
 (Ref. Fig. 402/TASK 35-22-54-991-006, 405/TASK 35-22-54-991-004)

 NOTE : Only the correct P/N of the emergency oxygen container must be
____ installed. The hoses have a specified length for each location in the aircraft and they must not be cut.
 (1)
 Do an inspection of the component interface and/or the adjacent area.

 (2)
 Put the oxygen container (8) in position, install the screws (6) and the washers (5).

 (3)
 Remove the vinyl bags from the disconnected line ends.

 (4)
 Remove the blanking plugs from the disconnected line ends.
　
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