Page 34 Vision Microsystems Incorporated
probe as the alignment guide. Bond the bushing to the rib / baffle
using the techniques recommended in your aircraft construction
manual.
NOTE 3: End supports (white bushing)
The probe end must be supported if more than 4 inches of length
remains after the last support point. Position a bushing near the
end of the probe so that the edge of the probe is approximately
1/8 inch from the wing skin. Secure the bushing at the surface of
the wing using potting mixture. Lay up two layers over the
bushing while the potting mixture is still soft to hold the bushing in
place. Use the bonding techniques recommended in your aircraft
construction manual.
For final installation, prepare the pipe threads of the probe with an
aviation fuel proof thread sealant/lubricant according to sealant
manufacturers’ directions. Insert the probe into the tank and through the
bushings until the threads engage. Hand tighten the probe. Now tighten
the probe with a torque wrench to 230 INCH POUNDS.
Use the J5 connector harness 700719-2 labeled LEFT TNK and
RT TANK. After senders are installed, connect them to the J5
FP/FQ/AMP wiring harness as shown below (only the right tank sender is
shown for illustration purposes). Trim the longest pair of gray cables
labeled LEFT TNK and RT TANK to length, then crimp the three sockets
onto the harness wire, and insert them into the connector housing.
Connect this to the capacitive sender pod cable and connect the white
wire of the pod cable to the center, insulated terminal on the sender, and
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