Service difficulty report · Harness · Cndair CL6002B19

Difficulty date
December 4, 2000
Submitted
January 19, 2001
Operation
General aviation
Make and model
Cndair CL6002B19
Engine
Ge CF343B1
Part
Harness
Condition
Arced
Location
Rt Engine
Stage of operation
CL
How discovered
O
Nature of condition
B, E
Precautionary procedure
A

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

What was found

(CAN) AFTER TAKEOFF, THE CREW REPORTED HIGH RT N1 VIBRATION, THE FLIGHT CREW DECIDED TO RETURN TO THE BASE.THE MAINTENANCE FOUND THE RED ENGINE HARNESS, THE IDG CABLES, THE THERMOCOUPLE HARNESS AND THE RT LOWER CORE COWL WITH BURNT MARKS. THEY FOUND THE IDG CABLE SHROUD SOAKED WITH FUEL. THE FUEL LEAK PASSING BY THE RT MFC THROTTLE SHAFT BODY. THEY REPLACED THE RT ENGINE. 2001-01-03TC: MANUFACTURE OF AIRCRAFT AND ENGINE HAS DISCUSSED SDR WITH TC.FAA ASB PENDING, AND AIRWORTHINESS LIMITATION SECTION BEING REVISED IN TYPE CERTIFICATE.THIS OCCURRENCE IS ASSOCIATED WITH SDR 20010102009