Service difficulty report · Wire · Cndair CL6002B19

Difficulty date
August 26, 2011
Submitted
January 23, 2013
Operation
Air carrier
Make and model
Cndair CL6002B19
Aircraft time
34,636 hours
Engine
Ge CF343A1
Part
Wire
Condition
Damaged
Location
Te Flaps
Stage of operation
IN
How discovered
V
Nature of condition
O
Precautionary procedure
K

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

What was found

(CAN) DURING TESTING OF THE FLAP ELECTRICAL SYS FOR AN UNRELATED REASON, MX FOUND AN OPEN CIRCUIT BETWEEN THE NR 1 FLAP POWER DRIVE UNIT (PDU) THERMISTOR AND THE FLAP ELECTRONIC CONTROL UNIT (FECU). FURTHER INVESTIGATION REVEALED THAT ELECTRICAL WIRE, 1CE46A22WHT, WAS BROKEN BETWEEN CONNECTOR 1J6CE PIN F AND CONNECTOR P4CE-A PIN 15 (FECU), REF WIRING DIAGRAM 27-51-00 SHEET 4 AND 5. WIRE 1CE46A22BLU WAS ALSO FOUND WITH SUBSTANTIAL DAMAGE. THE WIRES WERE PART OF A BUNDLE LOCATED BEHIND THE FECU RACK. THE BROKEN/DAMAGED WIRES WERE LIKELY THE RESULT OF TOO TIGHT PLASTIC TIE WRAP. THE WIRES WERE REPAIRED, THE SYS TESTED AND THE ACFT RELEASED FOR SERVICE. THE THERMISTOR PROVIDES OVERHEAT PROTECTION FROM THE PDU ELECTRICAL MOTOR. THE LOST OF THE THERMAL PROTECTION WILL NOT TRIGGER ANY CAUTION/STATUS MESSAGE.