What was found
A CRACK WAS FOUND AT HOLE 28, EXTENDING FWD, EXCEEDS THE AUTHORIZED REPAIR AREA AT THE PRESSURE PANEL BETWEEN FRAMES 35 AND 36, REPAIRED IAW PRI 542042-14AD, REV B, PRI REV 0 , 1, 2, 3, 4, AND COMPLIED WITH ER/A 542042-14AD, REV B.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
A CRACK WAS FOUND AT HOLE 28, EXTENDING FWD, EXCEEDS THE AUTHORIZED REPAIR AREA AT THE PRESSURE PANEL BETWEEN FRAMES 35 AND 36, REPAIRED IAW PRI 542042-14AD, REV B, PRI REV 0 , 1, 2, 3, 4, AND COMPLIED WITH ER/A 542042-14AD, REV B.