Service difficulty report · Control Cable · Cessna 310N

Difficulty date
December 28, 2005
Submitted
January 30, 2006
Operation
General aviation
Aircraft
N4110Q
Make and model
Cessna 310N
Aircraft serial
310N0010
Engine
Cont IO470*
Part
Control Cable
Part number
08602073
Condition
Broken
Location
Lt Rudder
Part time
6,986 hours
Stage of operation
NR
How discovered
9
Nature of condition
O
Precautionary procedure
O

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

What was found

THE LT RUDDER CABLE BROKE AT THE CLEVIS THAT ATTACHES IT TO THE RUDDER TORQUE TUBE ARM. UNDER NORMAL OPERATING CONDITIONS, DURING THE 37 YEARS AND HOURS THAT THE AIRCRAFT HAS BEEN IN SERVICE. THE RT RUDDER CABLE HAD ABOUT 25 PERCENT OF THE STRANDS BROKEN. THE BOLT FOR THE CLEVIS WAS SO TIGHT THAT THE CLEVIS COULD NOT PIVOT ON THE BOLT ATTACHING IT TO THE RUDDER TORQUE TUBE ARM. THE CONSTANT UP AND DOWN PULL ON THE CABLE BALL SWEDGE SEEMS TO HAVE BROKEN THE STRANDS OF THE CABLE A FEW AT A TIME. THE CLEVISES NEED TO BE INSPECTED FOR FREEDOM OF MOVEMENT ON THE BOLTS THAT ATTACH THEM TO ARMS. (K)

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