
© 2020 Glenair, Inc • 1211 Air Way, Glendale, CA 91201 • 818-247-6000 • www.glenair.com • U.S. CAGE code 06324 • BacNav OFS
Dimensions in Inches (millimeters) are subject to change without notice.
© 2020 Glenair, Inc • 1211 Air Way, Glendale, CA 91201 • 818-247-6000 • www.glenair.com • U.S. CAGE code 06324 • BacNav OFS
Dimensions in Inches (millimeters) are subject to change without notice.
SERIES 390
BacNav™ OFS
Assembly Instructions
SERIES 390
BacNav™ OFS
Assembly Instructions
3/8" ±1/8" (Electrical)
1/2" ±1/8" (Fiber-optic)
Calculate Length
For Contact
Termination
To Rear Of
Connector Shell
Connector-coupling-nut
Engagement Length
Main Body Assembly
Overall Length
Eective Main Body
Assembly Length
Connector
Length
The Following suggested assembly procedure serves as a guide for proper assembly and installation of Glenair P/N 390G084
Compression-nut and
Gland-nut Assembly
Main Body
Assembly
Loosen with 7/64” Hex-Wrench
to Reposition Angle
O-ring
(If Applicable)
Insert-retainer
(If Applicable)
Braid/Kevlar® Folded
Back Flat Over Cable
Tape
Contacts/OFC's
Step 1
Cut cable to desired length, making sure to include contact
termination length and desired service loop length (Note:
service loop not applicable for ber termination.)
Step 2
Slide BacNav OFS backshell assembly onto cable-end being
terminated. Slide insert-retainer and o-ring or adapter (as
applicable) onto cable following the backshell. (Note: Adapter
may be coupled to backshell.) Unscrew and separate intermediate
compression nut and gland assembly from main body assembly.
(See gure 1)
Step 3
Prepare cable end for termination.
a. Determine cable jacket strip length. For precise
determination, it is recommended to terminate a connector
using a minimum strip length, then mark the cable jacket
at the required distance behind the main body assembly.
Length will include contact termination length, desired
service loop length (not applicable for ber) and eective
main body assembly length (includes installed adapter
length if present). (See gure 2)
b. Remove outer cable jacket exposing cable-shield (braid) or
Kevlar® strength members (ber-optic applications).
c.
Shielded electrical cable applications: Remove any water-
block material from cable-shield. Trim cable shield to 3-4
inch length (optional) then fold back at over outer cable
jacket and tape down.
Fiber-optic applications: Leave Kevlar® strength members
long, fold back over outer cable jacket and tape down
(See gure 3)
Step 4
Prepare conductor/bers and terminate contacts/OFCs according
to specic connector requirements.
Step 5
Insert contacts/OFCs into connector according to specic connector
requirements.
Step 6
Move backshell main body assembly (with adapter if present,
or insert-retainer/o-ring if present) towards cable end to mate
with connector. Position insert-retainer and o-ring if applicable,
then thread backshell/adapter-to-connector coupling nut onto
connector ensuring proper alignment/orientation with respect
to connector master-key, and verifying proper engagement of
clocking teeth or splines as the coupling nut is hand tightened.
(See Figure 4)
Step 7
Verify cable jacket strip length, and terminate cable-shield/
Kevlar® strength members. (Refer to banding tool instructions for
additional details).
Shielded electrical cable applications: End of cable jacket should
measure " ± " from conical end of main backshell body assembly
to cable jacket (with service loop length contained inside backshell).
(See gure 2) Un-tape cable-shield and fold forward over conical
end and banding platform, ensuring even 360° distribution.
Prepare termination-band and installation tool, positioning
over shield in the center of the banding platform. (See gure 5)
Complete band termination, ensuring cable jacket end remains
” ± from conical end of main backshell body. (See gure 6)
Fig. 4
Fig. 6
Fig. 5
Assembly Overview
Fig. 1
Fig. 2
Fig. 3

© 2020 Glenair, Inc • 1211 Air Way, Glendale, CA 91201 • 818-247-6000 • www.glenair.com • U.S. CAGE code 06324 • BacNav OFS
Dimensions in Inches (millimeters) are subject to change without notice.
© 2020 Glenair, Inc • 1211 Air Way, Glendale, CA 91201 • 818-247-6000 • www.glenair.com • U.S. CAGE code 06324 • BacNav OFS
Dimensions in Inches (millimeters) are subject to change without notice.
Mil-Spec Connectors and Components Aimed at
Reducing Downtime and Improving Performance
Glenair innovations in composite thermoplastic materials and unique
backshell assemblies, optimize shield termination performance
SUPERSEAL™ RJ45 CONNECTORS
Superior sealing—IP68 when mated—for complete
system protection against water, sand and dust
Shielded/grounded coupler designs in both receptacle
and plug connectors
Crimp, solder-cup, PC tail, and Quadrax contact/wire
termination options
RJ45 plug and/or jack interface options available in
Cat 5e or Cat 6a in D38999, D5015 and D26482 type
packages
Series 970 contacts are
precision-machined using
high conductivity copper
alloy.
Stamped and formed spring
(“Louverband”) installed
into socket contact.
Spring is made from 6 mil beryllium copper (BeCu).
Louverband spring provides many points of electrical
contact with the mating pin
Testing shows, Louverband contact system outperforms
conventional aerospace-grade contact systems.
Metal and composite solutions
Glenair is the world leader in the supply of shield termination
backshell technology to the aerospace industry. Our expertise
extends from conventional conductive metal-shell solutions to
innovative lightweight composite solutions such as the Swing-
Arm with its integrated EMI/RFI shield sock or special Do-Drop-
In insert.
POWERTRIP™ CONNECTORS
EMI/RFI SHIELD TERMINATION COMPONENTS
Band-Master™ ATS provides quick, easy,
cost-effective and reliable termination
of metallic shielding or fabric braid to
connectors and backshells.
Precision hand-held tool and bands deliver reliable,
repeatable performance
Single piece stainless steel bands in various sizes
and lengths
Clamp both small and large diameters easily and
reliably
Pneumatic banding tool for high-speed mass
production
Qualified for both military and commercial aviation
Band-Master® ATS, Band
SERIES 390
BacNav™ OFS
Assembly Instructions
Fiber-optic applications: End of cable jacket should measure
½” ± with ber-optic conductors pulled taught (See gure 2).
Un-tape Kevlar® strength members and fold forward over conical
end and banding platform, ensuring even 360º distribution.
Prepare termination-band and installation tool, positioning over
cable jacket. Ensuring bers are pulled taught, remove all slack
from Kevlar® strength members as they are dressed forward
over the main backshell body intermediate compression-nut
threads. Holding Kevlar® strength members tightly around the main
backshell body intermediate compression-nut threads, move band
and tool into position over banding platform (See gure 7). Tighten
termination band allowing the Kevlar® to pull the cable jacket end
towards the conical end of main backshell body a minimum of ¼”
when the band is fully tightened (See gure 8).
IMPORTANT! This procedure ensures the Kevlar® strength member
is pre-loaded and adequate fiber slack is provided inside the
backshell. (See gures 7 and 8)
Step 8
Trim cable-shield or Kevlar® strength members to the end of
the intermediate compression-nut threads. Note: If desired,
some extra length of cable-shield or strength members may be
tucked away in the pocket behind banding platform under the
intermediate compression-nut threads. (See gure 8)
Step 9
Move intermediate compression nut and gland assembly
into place and thread onto main body assembly. Tighten all
threaded couplings including connector to adapter/backshell
coupling nut, adapter to backshell coupling nut (if applicable),
intermediate compression-nut, gland nut and cable clamps (if
applicable) to appropriate torque values, refer to SAE AIR6151
for appropriate torque values. (See gure 9)
Fig. 9
Fig. 7
*IMPORTANT: Do not pull
F/O conductors beyond
Taught causing preload
On F.O.C. Spring component
Fiber-optic
Conductors
Pulled Taught
(No Slack)*
Kevlar Strength
Members
Pulled Taught
(No Slack)
Hold Kevlar
Firmly In
This Area
Band In
Ready
Position
1/2"±1/8"
Before
Tightening
Band
Fig. 8
Remaining Kevlar
Trimmed and
Tucked In This Area
Completed
Band
Termination
1/4"±1/8" After
Tightening Band
Proper Termination Will
Leave Approx 1/4" Slack In
Fiber-optic Conductors
Kevlar Strength Members
Must Remain Taught
(No Slack)
MIL-DTL-38999 MIL-DTL-5015 MIL-DTL-26482