Service difficulty report · Connector · Cessna 206H

Difficulty date
April 2, 2015
Submitted
April 7, 2015
Operation
General aviation
Aircraft
N238D
Make and model
Cessna 206H
Aircraft serial
20608238
Aircraft time
2,278 hours
Engine
Lyc IO540AC1A5
Engine time
2,278 hours
Part
Connector
Part number
KTKSAD10280X3
Condition
Melted
Location
Electrical
Part time
2,278 hours
Stage of operation
TX
How discovered
O
Nature of condition
B, G, H
Precautionary procedure
D

As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.

What was found

ALL APPLIANCES AND SYSTEMS ON ACFT ESSENTIAL BUS 2 POWERED OFF WITH THE SWITCH ON. ITEMS ON BUS 2 INCLUDE: THE TURN COORDINATOR, NAV LIGHTS, INTERIOR LIGHTS, STROBE LIGHTS, TAXI LIGHT, PITOT HEAT, TRANSPONDER, AND AUTOPILOT ALL FAILED. THE 40 AMP. BUS 2 CIRCUIT BREAKER IN THE J-BOX DID NOT TRIP OPEN. THE MALE AND FEMALE PINS A IN THE J-BOX TO POWER DISC PLUG, J2-PB017 GOT VERY HOT AND SMOLDERED IN THE MELTING PLUG UNTIL THE BUS 2 POWER SUPPLY CIRCUIT WAS ELECTRICALLY OPEN. SUSPECT THE CAUSE TO BE AN UNDERRATED 30AMP. DELPHI METRI-PACK 280 SERIES CONNECTOR BEING USED IN A CIRCUIT WIRED WITH TEN GAUGE WIRE, PROTECTED BY A 40 AMP CIRCUIT BREAKER. THIS PLUG IS DISCONNECTED AND RECONNECTED EVERY TIME THE RECOMMENDED ANNUAL ESSENTIAL AND CROSS FEED BUS DIODE CHECKS ARE ACCOMPLISHED USING A TE04 MCU TEST SET, POTENTIALLY INCREASING THE RESISTANCE AT THE CONNECTION EVERY TIME THAT IT DISTURBED. RECOMMEND THAT THIS PLUG IS EITHER ELIMINATED ENTIRELY AND THE 10 GAUGE WIRES FROM THE J-BOX AND TO THE BUS BARS BE SPLICED TOGETHER, OR A HIGHER AMPERAGE RATED CONNECTOR BE INSTALLED IN THIS LOCATION, BECAUSE AT THIS TIME, THIS CONNECTOR IS THE WEAK LINK IN THE CIRCUIT. ALSO WHEN THE CONNECTOR WAS HANDLED DURING REPAIR OF THE WIRES, TWO OF THE 10 GAUGE CABLES PULLED OUT OF THEIR RESPECTIVE PIN CRIMPS, INDICATING INADEQUATE CRIMPING AT MANUFACTURE. ANOTHER POTENTIAL CAUSE FOR HIGH RESISTANCE AT THIS JUNCTION. MFG WAS NOTIFIED.

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