(2)
For panel 191JB:
(a)
Disconnect the electrical connector from the anti collision light 6LV.
(b)
Put blanking caps on the disconnected electrical connectors.
(c)
Remove the bonding strap from the anti collision light.
(3)
Remove the panel (3).
**ON A/C ALL
TASK 53-35-13-400-001
Installation of the Belly Fairing Access Panels
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU
_______
START A TASK ON OR NEAR:
-
THE FLIGHT CONTROLS
-
THE FLIGHT CONTROL SURFACES
-
THE LANDING GEAR AND THE RELATED DOORS
-COMPONENTS THAT MOVE.
NOTE : The installation procedure for one panel is given; the procedure is
____
almost the same for all panels.
1. Reason for the Job
__________________
Self Explanatory
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific emery cloth grade 120 to 240.
No specific emery cloth grade 400
No specific emery cloth, grade 120 to 240
No specific emery cloth, grade 400
No specific 2 SPATULA - WOODEN
R No specific Torque Wrench : range 0.00 to 1.20 m.daN
R (0.00 to 9.00 lbf.ft)
EFF : ALL
53-35-13Page 414
B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 07-006 AIB TN 10106 TYPE II ANTISTATIC PAINT (HIGH RESISTIVITY) (Ref. 20-31-00) Material No. 08-004 USA MIL-A-25457 ADHESIVE SEALANT (Ref. 20-31-00) Material No. 08-004A USA MIL-A-46106 TYPE I ADHESIVE SEALANT (Ref. 20-31-00) Material No. 08-033 USA MIL-A-46050 TYPE I CLASS 3 CYANO - ACRYLATE ADHESIVE (Ref. 20-31-00) Material No. 11-003 USA ASTM D 740 METHYL-ETHYL-KETONE (Ref. 20-31-00) Material No. 16-024A F AIMS 04-04-002 PRIMER FOR COMPOSITE PARTS (Ref. 20-31-00) Material No. 19-003 USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00)
C. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
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)-
29-10-00-864-001 Depressurize the Green Hydraulic System
29-10-00-864-002 Depressurize the Yellow Hydraulic System
29-10-00-864-003 Depressurize the Blue Hydraulic System
32-12-00-410-001 Close the Main Gear Doors after Access
ASRM 514200
**ON A/C 001-049, 051-099, 101-149, 201-299,
53-35-13-991-001 Fig. 401
R **ON A/C 151-199, 401-499,
53-35-13-991-001-A Fig. 401A
EFF : ALL
53-35-13Page 415
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
**ON A/C 301-399,
53-35-13-991-001-B Fig. 401B
**ON A/C 001-049, 051-099, 101-149, 201-299,
53-35-13-991-002 Fig. 402 R **ON A/C 151-199, 401-499,
53-35-13-991-002-A Fig. 402A
**ON A/C 301-399,
53-35-13-991-002-B Fig. 402B
**ON A/C 001-049, 051-099, 101-149, 201-299,
53-35-13-991-003 Fig. 403
**ON A/C 301-399,
53-35-13-991-003-A Fig. 403A
**ON A/C 002-049, 051-051, 053-099, 101-105, 151-199, 201-214,
53-35-13-991-010 Fig. 404
EFF : ALL
53-35-13Page 416
**ON A/C ALL
3. Job Set-up
__________
Subtask 53-35-13-860-051
A. Aircraft Maintenance Configuration
(1)
Make sure that the aircraft is in the same configuration as for the removal task.
(2)
Make sure that the Green, Blue and Yellow hydraulic systems are depressurized (Ref. TASK 29-10-00-864-001), (Ref. TASK 29-10-00-864-002) and (Ref. TASK 29-10-00-864-003).
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 FUSELAGE 機身2(122)
