What was found
CLT - C-6 - SUPPORT ANGLE, .75 INCH CRACK. SUPPORT ANGLE FOR UPPER FIXED T/E PANEL OB OF NACELLE, LT WING. FABRICATED AND INSTALLLED NEW ANGLE, SRM. (K)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CLT - C-6 - SUPPORT ANGLE, .75 INCH CRACK. SUPPORT ANGLE FOR UPPER FIXED T/E PANEL OB OF NACELLE, LT WING. FABRICATED AND INSTALLLED NEW ANGLE, SRM. (K)