Service difficulty report · Wire Harness · Piper PA28140

Difficulty date
February 28, 2016
Submitted
March 8, 2016
Operation
General aviation
Aircraft
N7168R
Make and model
Piper PA28140
Aircraft serial
2821877
Engine
Lyc O320*
Part
Wire Harness
Condition
Chafed
Location
Instrument Panel
Stage of operation
CL
How discovered
O
Nature of condition
B, A
Precautionary procedure
A

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

What was found

AS THE AIRCRAFT WAS CLIMBING THROUGH 400 FEET AGL, THE PILOT DETECTED SMOKE COMING FROM UNDERNEATH THE LT HALF OF THE INSTRUMENT PANEL. THE PILOT DECLARED AN EMERGENCY AND RETURNED FOR LANDING ON RUNWAY 22R. AFTER LANDING, THE PILOT STATED THAT MELTED WIRING INSULATION HAD DRIPPED ONTO THE FLOORBOARD CARPET AND STARTED A SMALL FIRE. THE PILOT WAS ABLE TO EXTINGUISH THE FIRE WITH HIS FEET. THIS ACFT WAS INSPECTED BY PERSONNEL OF THE FSDO ON 02/29/2016. THE INSPECTION SHOWED THAT ELECTRICAL ARCHING WAS EVIDENT UPON REMOVAL OF THE NAV II INSTRUMENT ON THE LT SIDE OF THE INSTRUMENT PANEL. THERE WAS EVIDENCE OF 2 CONTACT POINTS ON THE LOWER RT CORNER OF THE INSTRUMENT CASE. THE 2 WIRES THAT CAME INTO CONTACT WITH THE INSTRUMENT WERE CHAFED INTO THE CONDUCTOR OF THE WIRES. THE WIRES WERE IDENTIFIED AS A GENERATOR FIELD AND A GENERATOR OUTPUT WIRE. ONCE THE WIRES CHAFED THROUGH THE INSULATION, CURRENT FROM THE GENERATOR SYS, TRAVELED THROUGH THE NAV II CASE AND INTO THE ANTENNA COAX CABLE SHIELDING, CAUSING THE BURNING AND MELTING OF THE PLASTIC CASING ON THE COAX CABLE. THE INSULATION ABOVE THE COAX CABLE HAD THE ODOR OF HAVING BEEN EXPOSED TO FIRE.

More about the Piper PA-28-140