What was found
INSPECTION FOUND A 1 INCH CRACK ON FAIRING SUPPORT ANGLE AT STA 1421, STRINGER 32R. THE SUPPORT ANGLE WAS REMOVED. A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-20-00, 51-31-01, AND 53-53-01, FIGURE 3.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 1 INCH CRACK ON FAIRING SUPPORT ANGLE AT STA 1421, STRINGER 32R. THE SUPPORT ANGLE WAS REMOVED. A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-20-00, 51-31-01, AND 53-53-01, FIGURE 3.