(j)
 Remove the subassemblies from the aircraft.

 (k)
 Remove the stepladder.

 EFF : ALL
25-43-41Page 416
Config-2 May 01/04
R
 CES

 INTENTIONALLY BLANK

 Lavatory Subassemblies Figure 407/TASK 25-43-41-991-024- 12 (SHEET 1)
R  EFF : CES  ALL  Page 41825-43-41 Config-2 Feb 01/03 

 Lavatory Subassemblies Figure 407/TASK 25-43-41-991-024- 22 (SHEET 2)
R  EFF : CES  ALL  Page 41925-43-41 Config-2 Feb 01/03 

 TASK 25-43-41-400-001
 Installation of the Lavatory D
 1. Reason for the Job
__________________
 Self Explanatory
 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific 1 SCRAPER - NON METALLIC
 No specific 1 STEPLADDER 1.0 M (3.3 FT)
 No specific 1 WARNING NOTICE

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 -------------------------------------------------------------------------------
No specific cable ties
 No specific rubber profile
 Material No. 04-004A

 INFORMATION TRANSFERRED TO 04-022 (Ref. 20-31-00) Material No. 05-002 USA MIL-P-8116 PUTTY, ZINC CHROMATE GENERAL PURPOSE (Ref. 20-31-00)
 Material No. 05-005D  USA MIL-C-16173 GRADE II
 CORROSION PREVENTIVE (OBSOLETE USE 15-007)
 (Ref. 20-31-00)

 Material No. 08-004  USA MIL-A-25457
 ADHESIVE SEALANT (Ref. 20-31-00)

 Material No. 08-066  D DAN 319, DAN 1202
 ACRYLIC PRESSURE SENSITIVE ADHESIVE FILM
 (Ref. 20-31-00)

 Material No. 09-016  USA MIL-PRF-81733D TYPE II CLASS B
 CORROSION INHIBITING FILLET CONSISTENCY
 (Ref. 20-31-00)

 Material No. 09-036
 SILICONE SEALANT (1 PART) (Ref. 20-31-00)

 EFF : ALL
25-43-41Page 420

 -------------------------------------------------------------------------------
REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 11-003 USA ASTM D 740
 METHYL-ETHYL-KETONE (Ref. 20-31-00) Material No. 19-003 USA AMS 3819
 LINT-FREE COTTON CLOTH (Ref. 20-31-00) Material No. 19-010 USA AMS 5687
 LOCKWIRE STAINLESS STEEL ANNEALED 0.8MM DIA
 (Ref. 20-31-00)
 C. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
11-00-00-400-007  Installation of the ESSO (Scotchcal Labels)
 12-24-38-680-001  Draining of the Potable Water System (with Electrical
 Power)
 20-28-00-912-004  Electrical Bonding of Components With Conductive
 Bolts and Screws and Bonding Straps in the Fuselage
 and in the Wings (this does not include the tanks)-
21-23-00-720-002  Functional Test of an Air Extraction Point
 23-73-00-710-005  Operational Test of the Passenger Address (PA) System
 23-73-00-710-007  Operational Test of the Passenger Call System
 23-73-00-710-022  Operational Test of the Passenger Address (PA) System
 23-73-00-710-024  Operational Test of the Passenger Call System
 24-42-00-861-001  Energize the Ground Service Network from the External
 Power
 24-42-00-862-001  De-energize the Ground Service Network Supplied from
 the External Power
 25-22-41-000-001  Removal of the Wall-Mounted Cabin-Attendant Seats
 25-22-41-400-001  Installation of the Wall-Mounted Cabin-Attendant
 Seats
 25-22-42-400-001  Installation of the Free-Standing Cabin-Attendant
 Seat(s)
 25-23-41-000-001  Removal of the Ceiling Panels
 25-23-41-400-001  Installation of the Ceiling Panels
 25-23-42-000-002  Removal of the Ceiling Panels - Aft Utility Area
 25-23-42-400-002  Installation of the Ceiling Panels - Aft Utility Area
 25-23-43-000-001  Removal of the Upper Sidewall Panel(s)
 25-23-43-400-001  Installation of the Upper Sidewall Panel(s)
　
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機維護手冊 AMM EQUIPMENT/FURNISHINGS 設備3(87)