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
Fig. 1
Pre termination distance between
conical end and cable jacket
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
Cable Jacket
Strip-length
Mark
Fig. 2
Assembly Overview
Fig. 3
SERIES 390
BacNav™ OFS
Assembly Instructions
The following suggested procedure serves as a guide
for proper assembly and termination of Glenair P/N’s
390A084, 390G084, 390G084(-761) and 390H084
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, compression-nut and
gland-nut assembly rst, 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.
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).
Remove outer cable jacket exposing cable-shield
(braid) or Kevlar strength members (ber-optic
applications).
Shielded 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 (See gure 3).
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 teeth/splines to determine the
rotational orientation of the backshell as the coupling
nut is hand tightened (See Figure 4).
Step 7.
Verify cable jacket strip length, and terminate cable-
shield/Kevlar® strength members according to
following instructions. (See banding tool instructions
for banding termination process)
©  GLENAIR, INC •  AIR WAY • GLENDALE, CA  • -- • WWW.GLENAIR.COM • U.S. CAGE CODE  • U.S. PATENT NO. 
Braid/Kevlar® Folded Back
Flat Over Cable
Insert Retainer
(Fiber-optic)
O-ring
(Fiber-optic and
MIL-DTL-��)
Shielded cable applications: End of cable jacket
should measure 3/8” ±1/8” from conical end of main
backshell body assembly to cable jacket with service
loop length contained inside backshell. 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 center of banding platform (See gure 5).
Complete band termination (See gure 6), ensuring
cable jacket end remains ” ± ��� from conical end of
main backshell body (See Figure 2).
Fiber-optic applications: Prior to banding, end of
cable jacket should measure ½” ± with ber-optic
conductors pulled taught (See gure 7). 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 ber
slack is provided inside the backshell.
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. Finish assembly by tightening all threaded
couplings including connector to adapter/backshell
coupling nut (if applicable), torque intermediate
compression-nut, gland nut and cable clamps (if
applicable) to appropriate torque values, refer to SAE
AIR6151 for appropriate values (See gure 9).
BacNav OFS is now assembled.
Fig. 8 Fig. 9
Fig. 6Fig. 5
Fig. 7
Fig. 4
*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
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)
©  GLENAIR, INC •  AIR WAY • GLENDALE, CA  • -- • WWW.GLENAIR.COM • U.S. CAGE CODE  • U.S. PATENT NO. 