SDR 99ZZZM10

Service difficulty report · Bolt · Bbavia 8GCBC

Difficulty date
June 4, 1997
Submitted
March 26, 2000
Operation
General aviation
Aircraft
N778AC
Make and model
Bbavia 8GCBC
Aircraft serial
38197
Part
Bolt
Part number
AN621A
Condition
Improper Part
Location
Strut
Part time
32 hours
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

FOUND INCORRECT HARDWARD HAD BEEN INSTALLED IN THE UPPER END OF THE LEFT REAR LIFT STRUT. THE BOLT THROUGH THE UPPER END OF THE LIFT STRUT WAS APPROXIMATELY 1.5 INCHES PLUS TOO LONG. THE NUT HAD BEEN TIGHTENED UNITL IT BOTTOMED OUT ON THE THREADS, LEAVING THE LIFT STRUT FREE TO SLIDE ON THE BOLT. FLIGHT LOADS HAD BENT THE BOLT AND ELONGATED THE HOLE THROUGH THE STRUT ATTACH FITTING AND THE REAR SPAR. THESE PARTS ARE NOT REPAIRABLE PER AMERICAN CHAMPION AIRWORTHINESS LIMITATIONS LIMITATIONS, AND THE LEFT WING WAS REPLACED UNDER FACTOR WARRANTY. (M)