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R  drain pipe (5). 
R  (d) Disconnect the drain pipe (5) from the pipe (7). 
R  (e) Push up the insulation (11), loosen the nut (9) and disconnect 
R  the potable water pipe (10) from the fitting (8). 
R  (f) Put blanking plugs on the disconnected line ends. 
R  (3) Disconnect the Exhaust Air Connection 
R  (Ref. Fig. 402A/TASK 25-31-41-991-014-C) 
R  (a) Remove the clamp (13) and disconnect the exhaust air hose (12) 
R  from the manifold (14). 
R  (b) Put blanking plugs on the disconnected line ends. 

 

R  (4) Remove the Upper Attachments 
R  (Ref. Fig. 403A/TASK 25-31-41-991-018-C) 
R  (a) Remove the screws (3) and the access panel (4). 
R  (b) Remove the screws (2) and the pelmet (1). 
R  (c) Remove the quick-release pins (13) and disconnect the tie rods 
R  (14) from the aircraft structure. 
R  (d) Remove and discard the cotter pins (7). 
R  (e) Remove the washers (6), the bolts (5) and disconnect the tie rods 
R  (14) from the brackets (6). 
R  (f) Remove the nuts (9), the washers (10), the bolts (12), the bushes 
R  (11) and the brackets (8). 
R  (5) Remove the Lower Attachments 
R  (Ref. Fig. 404A/TASK 25-31-41-991-019-C) 
R  WARNING : SUPPORT THE UNIT/ASSEMBLY OR IT WILL FALL AND BECOME_______ 
R  DAMAGED OR INJURE PERSONNEL. THE UNIT/ASSEMBLY IS HEAVY. 
R  (a) Remove the screws (1) and (11) and the covers (2) and (12). 
R  (b) Remove the bolts (16), the nuts (7), the washers (8) and the 
R  plates (15). 
R  (c) Remove the eccentric plugs (13) and the eccentric bushes (14). 
R  (d) Carefully lift the galley off the blocks (4) and move it to the 
R  center of the aircraft. 
R  (e) Remove the shims (3). 
R  NOTE : Identify the position and number of the shims for the____ 
R  installation procedure. 
R  (f) Remove the bolts (10) and the washers (9). 
R  (g) Remove the blocks (4). 
R  (h) Remove and discard the packings (5). 
R  (i) Remove the bushes (6). 

 

R  Subtask 25-31-41-020-050-C 
R  B. Disconnect the Galley Splitline 
R  NOTE : This procedure is only necessary if you must remove the galley____ 
R  from the cabin. 
R  NOTE : The splitline screws and bolts are painted red.____ 
R  (1) Disconnect the Splitline Electrical Connections 
R  (Ref. Fig. 406/TASK 25-31-41-991-053) 
R  (a) Remove the bolts (1) and the bonding strap (2). 
R  (b) Remove the screws (4) and the clamps (3). 
R  (c) Remove the screws (6) and the covers (7). 
R  (d) Remove the nuts (8), the washers (9) and the wires (5). 
R  (2) Disconnect the Splitline 
R  (Ref. Fig. 405A/TASK 25-31-41-991-020-B) 
R  WARNING : SUPPORT THE UNIT/ASSEMBLY OR IT WILL FALL AND BECOME_______ 
R  DAMAGED OR INJURE PERSONNEL. THE UNIT/ASSEMBLY IS HEAVY. 
R  (a) Remove the screws (26) and the door (25). 
R  (b) Remove the screws (22) and the plate (24). 
R  (c) Remove the clamp (18) and disconnect the sink drain (19) from the 
R  drain pipe (17). 
R  (d) Remove the screws (16) and the worktop (30) with the plate (29). 
R  (e) Remove the screws (20) and the shelf (23). 
R  (f) Remove the bolts (27) and the casting (11). 
R  (g) Remove the screws (12) and the strips (28). 
R  (h) Remove the screws (21) and the strips (14) and (15). 
R  (i) Carefully separate the galley modules (10) and (13) and remove 
R  them from the aircraft. 

 CES

R R  Splitline Connections Figure 405A/TASK 25-31-41-991-020-B 
R  EFF :  051-099,  25-31-41 Page 436 May 01/05
 CES 

 

 INTENTIONALLY BLANK

 

R  Splitline Connections - G1 Figure 405B/TASK 25-31-41-991-020-A13 (SHEET 1) 
R  EFF :  106-149, 201-299,  25-31-41 Page 438 May 01/05
 CES 

 

R  Splitline Connections - G1 Figure 405B/TASK 25-31-41-991-020-A23 (SHEET 2) 
R  EFF :  106-149, 201-299,  25-31-41 Page 439 May 01/05
 CES 

 

　
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