(3)
 Remove the Air Supply Connections (Ref. Fig. 402/TASK 25-33-41-991-006)

 (a)
 Release the clamp (6) and disconnect the ventilation hose (5).

 (b)
 Release the clamp (7) and disconnect the exhaust air hose (10).

 (c)
 Put blanking plugs on the disconnected line ends.

 (4)
 Remove the Upper Attachments (Ref. Fig. 403/TASK 25-33-41-991-012)

 (a)
 Remove the screws (2) and the panels (1).

 (b)
 Remove the screws (4) and the panels (3).

 (c)
 Release the quick-release pins (6) and disconnect the tie rod (5) from the aircraft structure and the bracket (7).

 (d)
 Remove the tie rod (5).

 (e)
 Remove the bolts (8) and the brackets (7).

 (5)
 Remove the Lower Attachments (Ref. Fig. 404/TASK 25-33-41-991-013)

 (a)
 Remove the screws (1) and the rub strips (2).

 (b)
 Remove the screws (4) and the covers (3).

 (c)
 Remove the screws (6) and the covers (5).

 (d)
 Remove the bolts (8) and the washers (9).

 (e)
 Remove the plates (11).

 (f)
 Remove the eccentric bushes (12) and the eccentric plugs (13).

 (g)
 Remove the galley unit. WARNING : SUPPORT THE UNIT/ASSEMBLY OR IT WILL FALL AND BECOME

 (h)
 If installed, remove the shims (14). NOTE : Identify the position and number of the shims for the

 Electrical Connections Figure 401/TASK 25-33-41-991-022- 12 (SHEET 1) 
R  EFF :  001-049, 101-105,  25-33-41 Page 410 May 01/05
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 Electrical Connections Figure 401/TASK 25-33-41-991-022- 22 (SHEET 2) 
R  EFF :  001-049, 101-105,  25-33-41 Page 411 May 01/05
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R R  Electrical Connections - G5 Figure 401A/TASK 25-33-41-991-022-C12 (SHEET 1) 
R  EFF :  051-099,  25-33-41 Page 412 May 01/05
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R R  Electrical Connections - G5 Figure 401A/TASK 25-33-41-991-022-C22 (SHEET 2) 
R  EFF :  051-099,  25-33-41 Page 413 May 01/05
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 Electrical Connections - G5 Figure 401B/TASK 25-33-41-991-022-A12 (SHEET 1) 
R  EFF :  106-149, 201-299,  25-33-41 Page 414 May 01/05
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 Electrical Connections - G5 Figure 401B/TASK 25-33-41-991-022-A22 (SHEET 2) 
R  EFF :  106-149, 201-299,  25-33-41 Page 415 May 01/05
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R  Electrical Connections - G5 Figure 401C/TASK 25-33-41-991-022-B12 (SHEET 1)
 EFF :  151-199,  25-33-41 Page 416 May 01/05
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R  Electrical Connections - G5 Figure 401C/TASK 25-33-41-991-022-B22 (SHEET 2) 
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 Supply Connections Figure 402/TASK 25-33-41-991-006 
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_______
 DAMAGED OR INJURE PERSONNEL. THE UNIT/ASSEMBLY IS
 HEAVY.
 1_ Carefully lift the galley off the blocks (15) and the fittings
 (20) and move it to the center of the aircraft.

____ installation procedure.
 (i)
 Remove the bolts (7) and the washers (10).

 (j)
 Remove the blocks (15).

 (k)
 Remove and discard the packings (16).

 (l)
 Remove the bushes (21).

 (m)
 Remove the bolts (17) and the washers (18).

 (n)
 Remove the fittings (20).

R R  Supply Connections - G5 Figure 402A/TASK 25-33-41-991-006-C 
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 Supply Connections - G5 Figure 402B/TASK 25-33-41-991-006-A 
R  EFF :  106-149, 201-299,  25-33-41 Page 421 May 01/05
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R  Supply Connections - G5 Figure 402C/TASK 25-33-41-991-006-B 
R  EFF :  151-199,  25-33-41 Page 422 May 01/05
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 Upper Attacment of the Galley 6483MM Figure 403/TASK 25-33-41-991-012 
R  EFF :  001-049, 101-105,  25-33-41 Page 423 May 01/05
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R R  Upper Attachment - G5 Figure 403A/TASK 25-33-41-991-012-B 
　
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