SDR 99ZZZX916

Service difficulty report · Clevis · Gulstm AA5

Difficulty date
July 9, 1998
Submitted
March 26, 2000
Operation
General aviation
Make and model
Gulstm AA5
Part
Clevis
Condition
Worn
Location
Rudder
Stage of operation
IN
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

SUBMITTER HAS FOUND MANY CLEVIS BOLTS WORN AT LEAST 1/3 THROUGH WHERE CLEVIS BOLT ATTACHES CABLE FROM RUDDER TO RUDDER BAR. THE RUDDER BAR HOLE ALSO IS ELONGATED EXCESSIVELY. IF UNDETECTED THIS WILL CAUSE SEPARATION OF RUDDER CABLE FROM RUDDER BAR/RUDDER PEDALS. HARD TO FIND AS THIS IS UNDER CONSTANT TENSION BY RUDDER SPRINGS. NEED TO RELAX SPRING TENSION IN ORDER TO THOROUGHLY INSPECT THESE BOLTS. RECOMMEND AD BE ISSUED MANDATING A THOROUGH INITIAL INSPECTION AND THEN REPETITIVE INSPECTION SAY EVERY 500 HRS TO ENSURE INTEGRITY OF PART. BOLT, PN AN2311. BAR, PN 601031501.