Installation Manual

53
CONFIDENTIAL UNDER NON-DISCLOSURE AGREEMENT (NDA)
Rev A1
Document:
WSS 4G Aircraft Installation Manual 750-
00003-00 Reva1.Docx
July -30
2020
Table 5.2.5-1 P2-C and P2-D Parts List
Quantity
Manufacturer & Description
Part Number
Drawing Item
Number (IN)
2
TE Connectivity/Deutsch DMC
Chimney, Non-rotation
732-8052-18A
7
4
GlenAir
Tie-down Strap
600-057 or equivalent
8
1
Braid Wire (36AWG, .500DIA)
AA59569R36T0500 or
equivalent
17
A/R
Insulation Sleeving (.500-.195DIA)
M23053/4-105-0 or equivalent
28
A/R
Insulation Sleeving (.750- .313)
M23053/4-106-0 or equivalent
29
A/R
Cable, 24AWG/8 COND
E50824 or equivalent
13
Figure 5.2.5-1 P2-C and P2-D 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: Wire listed is for reference only. Wires used for the installation are to be
determined by the installer as applicable to the aircraft.