Service difficulty report · Wire Harness · Airbus BD5001A11

Difficulty date
August 31, 2025
Submitted
September 15, 2025
Operation
Air carrier
Aircraft
N305DU
Make and model
Airbus BD5001A11
Aircraft serial
55084
Aircraft time
13,597 hours, 6,098 cycles
Engine
PW1524G3
Engine time
9,011 hours, 3,974 cycles
Part
Wire Harness
Condition
Shorted
Location
Zone 400
Stage of operation
TX
How discovered
O
Nature of condition
J
Precautionary procedure
O

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

What was found

AFTER LEFT ENGINE START, ELECTRICAL FAULT LT FBW PC PMG INOPERATIVE. T/S IAW EFIM, FAULT CODE 2401F3249, RELAY PREVIOUSLY CHANGED, WIRING CHECK FOR PINS X1 & X2 AT K17 RELAY OK, WIRING CHECK FROM A276P1 PIN 1 TO 38 SHOWS 28 VDC. R & R CDC1 LRM09 IAW AMP 24- 01-25. FAULT CONFIRMATION STILL SHOWS CASS MESSAGE FOR ELECTRICAL FAULT & INFO MESSAGE FOR LT FWB PC PMG INOP. LRU OPS MAINT PAGE SHOWS FAULT CODE 2401F3249 & 2401F3247. END OF EFIM PROCEDURE FOR FAULT CODE 2401F3249. REAPPLIED M PROC, CONTINUE ON MEL. REPLACED IIM NR 1 IAW AMP 27-04-01 ALL TESTED GOOD ON BOX, LT PMG INOPERATIVE MESSAGE CAME BACK. FOUND WIRE WPC0001 -EIP 12WH, WPC0001-EIP-12B2 AND WPC0001-E1P-120R SHORTED TOGETHER & SHORTED TO GROUND. FOUND EVIDENCE OF ARCING AT P6027 PIN22, REMOVED PYLON ACCESS PANELS & BEGAN REMOVAL OF HARNESSES IAW AWDP 24-33-01AAA-051A-A . INSTALLED NEW WO8 HARNESS & SECURED FROM PMA TO P6027. INSTALLED NEW UPPER HARNESS OF J6027 BRACKET. INSTALLED UPPER HARNESS AT P5029 & CLAMPED ON TOP OF PYLON. CONTINUED INSTALLING OF UPPER HARNESS THROUGH SEALING PADS IAW AMP 51-23-00 & ESPP 20-10-01. INSTALLED NEW FBWPC & RAN ENG, NO FAULTS MLL M PROCEDURES WERE REVERSED.

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