(f)
Remove and discard the tape from the harness 13QT1(13QT2) and remove the harness from the string.
(g)
Remove the harness 13QT1(13QT2) from the aircraft.
(h)
Leave the string in position for the installation.
R 1EFF : 106-149, 229-299, 401-499, 1 28-42-43Page 418 1 1 Aug 01/05 1 1 1CES 1R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
TASK 28-42-43-400-006
Installation of the Wing-Tank Inner-Cell Group A Harness 13QT1(13QT2)
WARNING : MAKE SURE THAT THE FLIGHT CONTROL SAFETY-LOCKS AND THE WARNING
_______
NOTICES ARE IN POSITION.
WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
_______
GEAR.
1. Reason for the Job
__________________
Self Explanatory
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific cable-ties
No specific crimping tool
No specific lint-free cloth
No specific plastic spatula
No specific safety barriers
No specific tape
No specific Torque Wrench : range 0.00 to 1.20 m.daN
(0.00 to 9.00 lbf.ft)
No specific Torque Wrench : range 0.20 to 3.60 m.daN
(2.00 to 26.00 lbf.ft)
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 28-42-43Page 419 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1 B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 08-013 USA MIL-R-46082 TYPE I MIL-S-22473 SEALANT, ANAEROBIC (Ref. 20-31-00) Material No. 09-001 USA MIL-S-8802 TYPE I CLASS A FUEL TANK SEALANTPOLYSULFIDE (Ref. 20-31-00) Material No. 11-026 GB DEF-STAN 68-148/1 SOLVENT GENERAL PURPOSE (Ref. 20-31-00)
Material No. 15-008 AIB TN 10138 TYPE II GRADE 2 CORROSION PREVENTIVE TEMPORARY PROTECTIVE COMPOUND (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. Expendable Parts
-------------------------------------------------------------------------------
FIG.ITEM --------- |DESIGNATION ---------------------------------------- |IPC-CSN------------------------------
1 cable-ties 28-42-05 20 -010
30 O-ring 28-42-43 01A-015
D. Referenced Information
------------------REFERENCE -------------------------------DESIGNATION ------------------------------
-------------------------------------------------------------------------------
12-11-28-650-003 Pressure Refuel with Automatic Control 28-10-00-910-001 Safety Procedures When You Do Work in a Fuel Tank 28-10-00-910-002 Access to the Fuel Tanks and the Work Areas 28-25-00-650-001 Pressure Defuel 28-25-00-650-003 To Drain Remaining Fuel from the Wing Tanks and the
Center Tank 28-25-00-869-001 Fuel Transfer 28-42-00-740-001 Status Report (BITE) 28-46-00-740-001 Functional (BITE) Test
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 28-42-43Page 420 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1
-------------------------------------------------------------------------------
REFERENCE DESIGNATION -------------------------------------------------------------------------------
R R 57-27-11-000-001 57-27-11-000-002 57-27-11-400-001 57-27-11-400-002 ESPM 203222 WL 912840 28-42-43-991-004 Removal of the Access Panel (540AB, 540BB, 540CB, 540DB, 540EB, 540FB, 540GB, 640AB, 640BB, 640CB, 640DB, 640EB, 640FB, 640GB)Removal of the Access Panel (540HB, 540JB, 540KB, 540LB, 540MB, 540NB, 540PB, 540QB, 540RB, 550AB, 550BB, 550CB, 550DB, 560AB, 640HB, 640JB, 640KB, ....)Installation of the Access Panel (540AB, 540BB, 540CB, 540DB, 540EB, 540FB, 540GB, 640AB, 640BB, 640CB, 640DB, 640EB, 640FB, 640GB)Installation of the Access Panel (540HB, 540JB, 540KB, 540LB, 540MB, 540NB, 540PB, 540QB, 540RB, 550AB, 550BB, 550CB, 550DB, 560AB, 640HB, 640JB, ....) Fig. 402
**ON A/C 001-049, 051-099, 101-105, 151-199, 201-228,
28-42-43-991-006 Fig. 403
R **ON A/C 106-149, 229-299, 401-499,
28-42-43-991-006-A Fig. 403A
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
28-42-43-991-007 28-42-43-991-009 Fig. 404Fig. 405
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 28-42-43Page 421 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1 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 FUEL 燃油5(87)
