Service difficulty report · Control Cable · Cndair CL2151A10

Difficulty date
May 3, 2004
Submitted
November 2, 2004
Operation
General aviation
Make and model
Cndair CL2151A10
Aircraft time
1,984 hours
Engine
Pwa R2800*
Part
Control Cable
Part number
215903812
Condition
Corroded
Location
Rudder Control
Stage of operation
IN
How discovered
9
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

DURING A STRUCTURAL REPAIR TO THE RT REAR WING-TO-FUSELAGE FRAME ANGLE A PANEL AT WS 60.80, ADJACENT TO REAR SPAR, HAD TO BE DRILLED OFF TO FACILITATE THE REPAIR. IT WAS AT THIS TIME CORROSION WAS DISCOVERED ON THE RUDDER/AILERON INTERCONNECT CABLE P/N 215-90381-2 WHICH LIES DIRECTLY UNDER THIS PANEL. THE CORROSION WAS REMOVED AND UPON A CLOSER INSPECTION SEVERAL BROKEN STRANDS WERE NOTICED. THE MM WAS CONSULTED AND IT WAS DETERMINED THAT THE CABLE WAS BEYOND LIMITS. THE CABLE WAS REMOVED AND REPLACED WITH A SERVICEABLE UNIT AND THE WING PANEL WAS SEALED WITH AN APPROVED SEALANT. ITS WORTH NOTING THAT THE DAMAGE WOULD BE IMPOSSIBLE TO SPOT HAD IT NOT BEEN FOR THE REMOVAL OF THE RIVETED PANEL. THIS IS AN AR