(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)
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：A320飞机维护手册 AMM EQUIPMENT/FURNISHINGS 设备3(87)
