Service difficulty report · Rod · Cndair CL6002B19

Difficulty date
April 19, 2001
Submitted
May 11, 2001
Operation
General aviation
Make and model
Cndair CL6002B19
Engine
Ge CF343B1
Part
Rod
Part number
A33721
Condition
Loose
Location
Nacelle Door
Stage of operation
CR
How discovered
O
Nature of condition
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) AIRCRAFT ENROUTE TO MONTERREY, THE CREW WERE UNABLE TO RETARD THE LEFT HAND THROTTLE LOWER THAN 95 PERCENT. THE CREW RETURNED TO MEMPHIS AND CARRIED OUT QRH ABNORMAL 1-14. MECHANICS FOUND THE HOLD OPEN STRUT OF THE LT ENGINES UPPER CORE COWL JAMMED BETWEEN THE FUEL CONTROL UNIT INPUT SHAFT AND THE COWLING. THE STRUT WAS REMOVED (DMI) AND THE AIRCRAFT RETURNED TO SERVICE.DURING THE PRELIMINARY INVESTIGATION THE BALL WITHIN THE PIN BLC38C11SL5C4 WAS FOUND TO BE MISSING. THE STRUT STOWING END, BRACKET 228-50182-585 AND THE CLIP 228-50583-101 WILL BE VERIFIED UPON INSTALLATION OF NEW ROD TO CONCLUDE THE INVESTIGATION.