Installation Manual

CONFIDENTIAL UNDER NON-DISCLOSURE AGREEMENT (NDA)

Rev A1

Document:

WSS 4G Aircraft Installation Manual 750-

00003-00 Reva1.Docx

July -30

2020

Figure 5.2.2-1 P1-B Shield Terminations

Note 11: After stripping cable outer jacket, secure ends of braided shield and foil shield using insulation

sleeving indicated.

Note 12: Fit a length of braid wire, IN (ITEM NUMBER) 17, such that it covers the cable outer jacket, the

exposed cable shield, and the connector chimney or back-shell.

Secure one end of IN 17 on the cable shield using IN 8 and secure the other end of IN 17 to the

connector chimney or back-shell, again using IN 8.

Completely cover IN 17 using boot seal, IN 18, or sleeving, IN 27, 28 as indicated.

Note 20: Cables are cinched together when IN 8 is crimped.

NOTE: Wire listed is for reference only. Wires used for the installation are to be

determined by the installer as applicable to the aircraft.