What was found
INSPECTION FOUND A .5 INCH CRACK IN STRINGER 15L AND 15R AT STA 720B. THE CRACKED AREAS WERE CUT OUT, REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 51-10-2 AND 53-10-3, FIGURE 5.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A .5 INCH CRACK IN STRINGER 15L AND 15R AT STA 720B. THE CRACKED AREAS WERE CUT OUT, REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 51-10-2 AND 53-10-3, FIGURE 5.