As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
ANGLE IS BROKEN C/TO EXTERNAL FUSELAGE SKIN B/T STA 1239 AND STA 1256 STR 27L AND STR 28L. BROKEN ANGLE WAS REMOVED AND REPLACED WITH NEW PN OAI 53-0007 FABRICATED AND INSTALLED IAW SRM VOL 3, 53-53-01 FIG 3A AND CMM 4-45 USING FASTENERS PN HL18PBS-4 BN 58513-01 IAW SRM VOL 2 51-33-01.