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SUBJECT_______ CH/SE/SU________ C_ PAGE EFFECTIVITY____ ___________
SEALING PLUG PART NUMBERS 70-71-43
DESCRIPTION AND OPERATION 1 ALL
Connector sealing plug part 1 ALL
numbers.
General 1 ALL
Sealing Plug Part Number - List 1 ALL
Sealing Plug Part Number - List 2 ALL
Sealing Plug Part Number - List 2 ALL
Sealing Plug Part Number - List 3 ALL
CONNECTORS INSERT ARRANGEMENT 70-71-44
DESCRIPTION AND OPERATION 1 ALL
General 1 ALL
Procedure 1 ALL
EN2997 Series Connectors: 1 ALL
EN2997 1 ALL
MIL-C-83723 1 ALL
EN2997SE61212 4 ALL
MS3459 Series Connectors: 7 ALL
MS3459 7 ALL
BACKSHELL LOCKWIRE PROCEDURE 70-71-45
DESCRIPTION AND OPERATION 1 ALL
General 1 ALL
Procedure 1 ALL
Tools and Equipment 1 ALL
Consumable Material 1 ALL
Reference Information 2 ALL
Standard practices for Lockwire 2 ALL
Procedure 2 ALL
Safety wiring procedure 6 ALL
Procedure 6 ALL
CONTINUITY AND RESISTANCE TESTS 70-71-46
DESCRIPTION AND OPERATION 1 ALL
General 1 ALL
CONNECTOR CLOCKING 70-71-47
DESCRIPTION AND OPERATION 1 ALL
General 1 ALL
Procedure 1 ALL
JACKET AND/OR INSULATION STRIPPING 70-71-48
DESCRIPTION AND OPERATION 1 ALL
General 1 ALL
Procedure 1 ALL
Stripping Practices: 3 ALL
Procedure 3 ALL
Quality Assurance 10 ALL
Procedure 10 ALL
HARNESS OUTER JACKET REPAIR 70-71-53
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DESCRIPTION AND OPERATION 1 ALL
General 1 ALL
The harness outer jacket is 1 ALL
installed over the metal
overbraid to protect the
overbraid from wear, and to
protect the harness from
moisture
This procedure may be used to 1 ALL
perform a temporary, on-wing
repair to a damaged outer
jacket.
Consumable Materials 1 ALL
Harness Outer Jacket Repair 1 ALL
Use isopropyl alcohol to clean 3 ALL
the harness outer jacket for a
distance of 3 inches (76.20 mm)
on each side of the damage area.
Double Wrap the damage area with 3 ALL
high temperature insulation
tape.
To assure that the tape will 3 ALL
stay in place, tie the tape wrap
with tie tape.
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1. General
_______
(Ref. Fig. 001)
A. Engine directional references Clockwise, counterclockwise, clock position and other directional references apply to the engine in a horizontal position, viewed from the rear, and with the accessories section at the bottom. When components or struts are numbered in a circumferential direction the No.1 position is at 12 o'clock, or immediately clockwise from 12 o'clock. The remaining positions increase arithmetically in a clockwise direction. 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 STANDARD PRACTICES - ENGINES(3)
