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The customer arrives at Penn Avionics, Inc with a communication radio problem. The #2 com radio has poor range on both transmitting and receiving. The radio is pulled for a bench test, and no problems are found. Output power is good, receiver sensitivity is better than spec.
We have an aircraft wiring problem. Using our advanced test equipment, we can track it down quickly.
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The customer's aircraft is a Cessna C-182 which has the
antenna coax
running from the radio tray, along the lower inside windshield edge, then
up the door post to connect to the antenna mounted on top over the cabin.
The TDR has told us to start looking at the com#2 coax about 3.5 feet
from the tray. That location would be around the lower windshield area
near the door post. Ken opens up the left side interior panel to inspect
the coax.
This photo is a close up of the lower inside windshield edge. The rivets you see are holding the outer windshield attach faring. The coax has a tear in the outer jacket that is shorting the coax shield to the center conductor. This short is causing the poor performance of the #2 com radio. The damage to the coax was caused when the rivets were drilled out to replace the windshield (the windshield was replaced about 1 year before the #2 com radio began having problems). The drill bit grabbed the coax and nicked it, but the mechanic did not realize it had happened. Rather than trying a repair to the old coax, Ken ran a fresh piece from the radio tray to the antenna. The #2 comm radio was tested again and checked out good for power and receive sensitivity. The customer was on his way with a minimum down time.
Copyright 2003 Penn Avionics, Inc Rev 7/5/2003 |

