A320飞机维护手册 AMM EQUIPMENT/FURNISHINGS 设备3(25)_航空信息_民用航空_通用航空

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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 galley splitline screws are painted red.____
R (1) Disconnect the Splitline Electrical Connections
R (Ref. Fig. 407A/TASK 25-33-41-991-031)
R (a) Disconnect the electrical plug (154) from the connector (155).
R (b) Put blanking caps on the disconnected electrical connectors.
R (c) Remove the screws (153), the washers (152), the spacers (150) and
R loosen the clamps (151), as necessary.
R (2) Disconnect the Splitline Supply Connections
R (Ref. Fig. 406A/TASK 25-33-41-991-032)
R (a) Loosen the clamp (164) and disconnect the hose (165) from the
R sink (163).
R (b) Loosen the nut (171) and disconnect the hose of the fresh water
R system from the faucet (173).
R (c) Remove the nut (172) from the faucet (173).
R (d) Remove the faucet (173).
R (e) Loosen the clamp (167) and disconnect the ventilation hose (166)
R from the air-outlet (169).
R (f) Remove the nuts (168), the screws (170) and the air-outlets
R (169).
R (g) Disconnect the ring (161) of the control cable (162) from the
R drain valve (160).
R (h) Disconnect the other splitline supply connections, if necessary.

CES

R (i) Put blanking plugs on the disconnected line ends.
R (3) Disconnect the Galley at the Splitline
R (Ref. Fig. 405B/TASK 25-33-41-991-014-A)
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 bolts (112) and the pelmet (111).
R (b) Remove the screws (114) and the upper side cover (113).
R (c) Remove the screws (124) and the upper side cover (123).
R (d) Remove the screws (120) and the washers (121).
R (e) Remove the screws (118) and the washers (117).
R (f) Remove the screws (119).
R (g) Remove the screws (116) and the washers (115).
R (h) Carefully disengage the upper section (110) from the middle
R section (122).
R (i) Prevent damage to the component interface and the adjacent area.
R (j) Remove the screws (126) and the washers (127).
R (k) Remove the screws (128).
R (l) Carefully disengage the middle section (122) from the lower
R section (125).
R (m) Remove the screws (131), the washers (132) and the plate (133).
R (n) Remove the screws (134) and the lower side panel (130).
R (o) Remove the screws (135) and the lower side panel (136).
R (p) Remove the screws (138), the washers (137) and the doors (139).
R (q) Remove the screws (141), the strips (142) and the doors (140).
R (r) Carefully lift the galley sections (110), (122) and (125) and
R remove them from the aircraft.

**ON A/C ALL
TASK 25-33-41-400-002
Installation of the AFT Galley Unit (6481MM or 6483MM)
1. Reason for the Job
__________________
Self Explanatory
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific lint-free cloth
No specific nonmetallic-scraper R No specific Torque Wrench : range 0.00 to 1.20 m.daN R (0.00 to 9.00 lbf.ft)
B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 04-004A INFORMATION TRANSFERRED TO 04-022 (Ref. 20-31-00)
Material No. 04-022 USA MIL-PRF-81322 GRADE 2
SYNTHE.HYDROCARBON GREASE HIGH PRESSURE
(Ref. 20-31-00)

Material No. 08-002 USA MIL-R-46082 TYPE I GENERAL PURPOSE DIMETHACRYLATE GREEN (Ref. 20-31-00) Material No. 08-004A USA MIL-A-46106 TYPE I ADHESIVE SEALANT (Ref. 20-31-00) Material No. 11-003 USA ASTM D 740 METHYL-ETHYL-KETONE (Ref. 20-31-00)
Material No. 19-010 USA AMS 5687
　
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