B. Consumable Materials
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 05-013 Material No. 09-016  D TV-53-3507/73 RELEASE AGENT (OBSOLETE USE 05-013A) (Ref. 20-31-00)USA MIL-PRF-81733D TYPE II CLASS B
 CORROSION INHIBITING FILLET CONSISTENCY
 Material No. 09-019  (Ref. 20-31-00)USA AMS 3267/3 LOW ADHESION CORROSION INHIBITING SEALANT
 Material No. 11-004  (Ref. 20-31-00)USA MIL-T-81533
 Material No. 19-016  1.1.1TRICHLOROETHANE (METHYL CHLOROFORM) (Ref. 20-31-00)USA BMS 8-98 TYPE 3 CLASS 1
 POLYVINYL FLUORIDE FILM (Ref. 20-31-00)

 C. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
20-28-00-720-005 20-28-00-912-004 24-42-00-861-001  Check of the Electrical Bonding of the Different Components (But not the Fluid Systems and the Components Installed on Composite materials)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)-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
 29-14-00-614-001 29-14-00-614-002  Depressurization of the Hydraulic ReservoirsPressurization of the Hydraulic Reservoirs through the Ground Connector
 49-16-43-000-002 49-16-43-400-002 52-41-00-010-001 52-41-00-410-001  Removal of the Air Intake Flap (APS 3200)Installation of the Air Intake Flap (APS 3200)Open the APU Doors for AccessClose the APU Doors after Access
 49-16-41-991-005  Fig. 401 

 3. Job Set-up
__________ Subtask 49-16-41-860-060
 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)
 Make sure that the ground service network is energized (Ref. TASK 24-42-00-861-001) .

 (3)
 Make sure that the hydraulic systems are depressurized (Ref. TASK 29-14-00-614-001).

 (4)
 Make sure that the access platform is in position below the access doors 312AR and the maintenance door 314AR.

 (5)
 Make sure that the access door 312AR is open.

 (6)
 Make sure that the LIGHT control switch 3LJ is set to the ON position.

 (7)
 Make sure that the maintenance door 314AR is open.

 (8)
 Make sure that the access platform is in position below the APU access doors 315AL and 316AR.

 (9)
 Make sure that the APU access doors 315AL, 316AR are open (Ref. TASK 52-41-00-010-001) .

 (10)
 Make sure that the LIGHT control swtich 11LJ is set to the ON position.

 (11)
 Make sure that the air intake flap is removed (Ref. TASK 49-16-43-000-002).

 4. Procedure
_________
 (Ref. Fig. 401/TASK 49-16-41-991-005) Subtask 49-16-41-140-051
 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 49-16-41-420-054
 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.
　
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 機載輔助動力 AIRBORNE AUXILIARY POWER3(2)