Service difficulty report · Control Cable · Beech B300C

Difficulty date
March 17, 2011
Submitted
March 17, 2011
Operation
General aviation
Aircraft
N927KA
Make and model
Beech B300C
Aircraft serial
FM27
Aircraft time
200 hours
Part
Control Cable
Condition
Binding
Location
Elevator
Part time
200 hours
Stage of operation
IN
How discovered
V
Nature of condition
W
Precautionary procedure
K

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

What was found

ACFT WAS MODIFIED IAW STC SA00047MC BY A REPAIR STATION ON MAY 28, 2010. DURING THE FIRST PHASE INSP AT 200 HRS, IT WAS DISCOVERED THAT THE ELEVATOR TRIM CABLE TURNBUCKLE WAS DRAGGING ON THE BULKHEAD INSTALLED AT STA 414 AS PART OF THIS STC. THIS REPORT IS TO MAKE KNOWN THAT THERE IS A DESIGN DEFICIENCY WITH THIS STC, AND THAT THE REPAIR STATION THAT INSTALLED THE STC OVERLOOKED THIS DEFICIENCY AND RETURNED THE ACFT TO SERVICE WITH THE POTENTIAL FOR THE ELEVATOR TRIM SYS TO JAM. AC 43.13-1B CLEARLY STATES THAT CONTROL CABLE SPLICES ARE TO REMAIN AT LEAST 2 INCHES FROM FAIRLEADS OR PULLEYS. WHILE NOT A FAIRLEAD IAW SE, RIDING ON THE BULKHEAD STRUCTURE COULD BE CONSIDERED A FAIRLEAD. THE MM ALSO STATED IN CHAP 20 THAT CONTROL CABLES ARE NOT SUPPOSED TO HAVE INTERFERENCE WITH ACFT STRUCTURE. ONCE THIS DEFICIENCY WAS IDENTIFIED, 5 ADDITIONAL ACFT WERE INSPECTED FOR THIS CONDITION, AND AN ADDITIONAL 4 SHOWED THE SAME DISCREPANCY.

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