R EFF : 001-049, 101-105, 107-107, 151-199, 49-16-41Page 404 201-210, Config-2 Aug 01/05
CES
C. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
20-28-00-720-005 Check of the Electrical Bonding of the Different Components (But not the Fluid Systems and the Components Installed on Composite materials)
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)-
24-41-00-861-002 Energize the Aircraft Electrical Circuits from the External Power 24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied
from the External Power 29-14-00-614-001 Depressurization of the Hydraulic Reservoirs 29-14-00-614-002 Pressurization of the Hydraulic Reservoirs through
the Ground Connector 49-16-41-991-004-A Fig. 401
3. Job Set-up
__________
Subtask 49-16-41-860-057-A
A. Aircraft Maintenance Configuration
(1)
Make sure that the warning notice is in position on panel 25VU to tell persons not to start the APU.
(2)
Energize the ground service network
(Ref. TASK 24-41-00-861-002).
(3)
Make sure that hydraulic systems are depressurized
(Ref. TASK 29-14-00-614-001).
(4)
Make sure that the access platform is in position below the access door 314AR.
(5)
Make sure that the access door 314AR is open.
(6)
Make sure that the air intake-flap is removed.
R EFF : 001-049, 101-105, 107-107, 151-199, 49-16-41Page 405 201-210, Config-2 Aug 01/05
CES 4. Procedure
_________
(Ref. Fig. 401/TASK 49-16-41-991-004-A) Subtask 49-16-41-140-052-A
A. Preparation for installation. WARNING : OBEY THE MANUFACTURER'S INSTRUCTIONS WHEN YOU USE THIS/THESE
_______ MATERIAL/S. USE PROTECTIVE CLOTHING, RUBBER GLOVES, GOGGLES AND A MASK.
(1)
Remove all used sealant from component interface and/or adjacent area of the aircraft structure with a non-metallic scraper.
(2)
Clean the component interface of the aircraft structure with CLEANING AGENTS (Material No. 11-004) and a lint-free cloth.
(3)
Make sure that the component interface of the fixed diverter (12) is clean of sealant.
NOTE : If there is sealant on the component interface of the fixed
____ diverter, clean it with CLEANING AGENTS (Material No. 11-004) and a lint-free cloth.
Subtask 49-16-41-420-056-A
B. Installation of the fixed Diverter. WARNING : OBEY THE MANUFACTURER'S INSTRUCTIONS WHEN YOU USE THIS/THESE
_______ MATERIAL/S. USE PROTECTIVE CLOTHING, RUBBER GLOVES AND GOGGLES.
(1)
Apply SPECIAL MATERIALS (Material No. 05-013) with a non-metallic scraper to the surfaces of the fixed diverter (12) and the component interface of the aircraft structure.
(2)
Apply SEALANTS (Material No. 09-019) with a non-metallic scraper to the surfaces of the fixed diverter (12) and the component interface of the aircraft structure.
NOTE : Make sure that the screw holes do not show any signs of
____
sealant.
(3) Put the fixed diverter (12) in position and install the screws (6) and the washers (7) and tighten the screws. 中國(guó)航空網(wǎng) www.k6050.com 航空翻譯 www.aviation.cn 本文鏈接地址：A320飛機(jī)維護(hù)手冊(cè) AMM 機(jī)載輔助動(dòng)力 AIRBORNE AUXILIARY POWER2(154)
