Service difficulty report · Control Cable · Cessna 172S

Difficulty date
August 23, 2010
Submitted
September 9, 2010
Operation
General aviation
Aircraft
N556ER
Make and model
Cessna 172S
Aircraft serial
172S10561
Engine
Lyc IO360L2A
Propeller
Mcauly 1A170E
Part
Control Cable
Part number
0510105364
Condition
Frayed
Location
Aileron
Part time
2,095 hours
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

CABIN OVERHEAD CTR PANEL REMOVED FOR PROGRESSIVE INSP. DURING FLAP & AILERON CABLE INSPECTION, FLAT SPOTS WERE NOTICED ON 2 AILERON CONTROL CABLES. ROLLED CABLES FOR BETTER VIEW OF CONTACT POINT WITH PULLEYS, WAS ABLE TO CATCH FRAYED WIRES WITH A RAG & COULD SEE A SUBSTANTIAL GROOVE IN THE CARRY-THRU CABLE. CABLE TENSIONS WERE WITH PROPER SPECS & AREA CLEAN & FREE OF DIRT/DEBRIS. PLASTIC PULLEYS INSPECTED, THEY WERE CLEAN & FREE TO ROLL. PROBLEM SEEMS TO HAPPENING DURING NORMAL FLT TRAINING SCHOOL USE & HAS BEEN NOTICED TO BE HAPPENING WITH ALL OF OUR ACFT WITH SIMILAR ACFT TT. CAUSE OF PROBLEM CAN BE ATTRIBUTED TO PULLEYS, THEY ARE MADE FROM A HARD WHITE PLASTIC MATERIAL. BRAIDED STAINLESS STEEL CABLES ARE RUBBING AGAINST PULLELYS INSTEAD OF ROLLING ON THEM. THIS CAUSES THE CABLES TO FLAT SPOT AT FIRST & THEN CUT A GROOVE DEEP INTO THE CABLE. THERE IS ALSO NO NOTICEABLE CABLE DEFLECTION WHERE CABLES CONTACT PULLEYS, SEEMS PULLEY DIAMETER IS TOO SMALL. SUGGEST REPLACING PLASTIC PULLEYS WITH A STANDARD PHENOLIC PULLEYS THAT ARE USED IN ALL OTHER AREAS OF THE ACFT.

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