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| Sleeve | Outer | Coaxial Connector | | Code | Diameter | P/N Type | | | (Max.) | | |-----------|-------------------|------------------------| | MA1500 | 14mm (0.5511 in.) | E0460 BNC | | ME1300 | | | |-----------|-------------------|------------------------| | MA1600 | 19mm (0.7480 in.) | E0461 TNC | | |-------------------|------------------------| | | 21mm (0.8267 in.) | E0462 N | | |-------------------|------------------------| | MA1700 | 19mm (0.7480 in.) | E0463 C | ----------------------------------------------------------
R R R  - Position of the identification means Install the identification means at each repair operation near each end of the cable. Put the identification means on the cable immediately after the identification sleeve. 
R  (c) Type 3 (Ref. Fig. 005) For a cable assembly from a vendor, refer to the vendor documentation related to cable repair or replace the cable. 
R  B. Quad Cables 
R R R R  (1) Procedure (Ref. Fig. 002, 006) This paragraph gives the general description and conditions of application for each repair type.
R R  ____NOTE : For more data, refer to 20-48-36 ABS0973 AND ABS0974 PROCEDURE.

 

20-53-23 Page 8

 Repair of Coaxial Cables - Type 3 Cable Table
 Figure 005

 

20-53-23 Page 9

R Repair of Coaxial Cables - Repair Procedure Table R KB and KD R Figure 006

20-53-23 Page 10

R Layout and Table for Damage Assessment R KB and KD R Figure 007

20-53-23 Page 11

 _________________________________________________________
REPAIR OF THERMOCOUPLE CABLES - DESCRIPTION AND OPERATION
 _______

1. General
 This chapter gives the technical requirements for repair of the cables. These cables intalled on aircraft have P/Ns: E0527 HM E0528 HN NSA935291 YB NSA935292 YC
 ______________________2. Damage Check Procedure
 A. Cable Layout
 (Ref. Fig. 001)

 B. Table for Damage Assessment
 (Ref. Fig. 001)

 C. When the repair type is selected, refer to:
 (1)
 Para. 3 Repair Procedure for the general description and conditions of application.

 (2)
 20-53-29 GENERAL REPAIR PROCEDURE for more data.

 

20-53-24 Page 1

R Layout and Table of Damage Assessment R HM, HN, YB and YC
 Figure 001

20-53-24 Page 2

 ________________3. Repair Procedure
 A. Procedure
 (Ref. Fig. 002, 003)
 This paragraph gives the general description and conditions of
 application for each repair type.

 ____NOTE : You must use parallel splices.
 B. Allocation Table of Heat-Shrink Repair Sleeves (Ref. Fig. 004) The table that follows gives the different types of sleeves that you can use for repair, in relation to the type and gauge of the cable . (Refer to Chapter 20-42-12 for SLEEVE SRHINKING PROCEDURE).
 ____
NOTE : Make sure you use the correct sleeve for the aircraft temperature zone.
 C. Allocation Table of Repair Splices (Ref. Fig. 005) The table that follows gives the different types of sleeves you can use for repair, in relation to the type and gauge of cable (Refer to Chapter 20-43-1X for SPLICE CRIMPING PROCEDURE).
 ____
NOTE : Make sure you use the correct sleeve for the aircraft temperature zone.
 ____
NOTE : For detailed description and additional information, refer to 20-53-29 GENERAL REPAIR PROCEDURE.

20-53-24 Page 3

R Repair of Thermocouple Cables - Repair Procedure Table R HM, HN, YB and YC
 Figure 002

20-53-24 Page 4

R Repair of Thermocouple Cables - Repair Procedure Table R HM, HN, YB and YC
 Figure 003

20-53-24 Page 5

 Repair Sleeves - Allocation Table
 Method 5B only
 Figure 004

 

20-53-24 Page 6

 Repair Splices - Allocation Table
 Figure 005

 

20-53-24 Page 720-53-25 Page 1

R  _____________________________________________________REPAIR OF ALUMINUM CABLES - DESCRIPTION AND OPERATION
 _______1. General 
R  This chapter gives the technical requirements for repair of the Single-Core 
R  and multi-core Aluminum type cables. 
R  - Cables, Unscreened, Low-Temperature 180 deg.C (356.00 deg.F) ,these cables 
R  have P/Ns: 
R  ABS0949 AD 
R  ABS1354 ADA/ADB/ADC/ADD/ADE 
R  - Cables, Screened, Low-Temperature 180 deg.C (356.00 deg.F) ,these cables 
R  have P/Ns: 
R  ABS1356 VNA/VNB/VNC/VND
 - Aluminum Feeder Cables
 These cables installed on aircraft have P/Ns:
　
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