Service difficulty report · Control Cable · Cndair CL604

Difficulty date
March 7, 2002
Submitted
April 26, 2002
Operation
General aviation
Make and model
Cndair CL604
Aircraft time
80 hours
Part
Control Cable
Condition
Failed
Location
Rt Wing Aileron
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

(CAN) DURING ROUTINE INSPECTION FOUND RT WING OUTBOARD AILERON CONTROL CABLE RUBBING AGAINST TOP AILERON FUEL SYNC TRANSMITTER LINK. FURTHER DETAIL INSPECTION DISCOVERED AILERON DUAL SYNC TRANSMITTER LEVER INSTECTED APPROX 180 DEG. OUT OF NORMAL POS. PERFORMED VISUAL INSPECTION OF RT WING OUTBOARD CONTROL CABLE PER M/M 20-40-00 NO DISCREPANCY FOUND. DETAIL INSPECTION OF AILERON DUAL SYNCHRO LEVER, FOUND SMALL GROOVE OF 0.010 ON EDGE OF LINK. INSPECTED SURROUNDING STRUCTURE FOR ABNORMALITIES, NO DISCREPANCY FOUND. ADJUSTED AILERON DUAL SYNCHRO TRANSMITTER PER M/M 22-11-11. SECURED AILERON DUAL SYNCHRO TRANSDUCER LINK PER M/M 22-11-11.