As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
UPPER FUSELAGE STA1008; LBL15; FUSELAGE TO VERTICAL STAB SKATE ANGLE; OTBD SIDE; CHAFE WEAR; MRK'D. / EVALUATED WEAR AT B.S. 1008 ORIG THICKNESS .070 MAX WEAR DOWN TO .056 NO PUBLISHED LIMITS FOR LOSS OUT ANGLE I/A/W SRM 51-10-02-0G-0; REMOVED AND INSTALLED NEW UPPER FUSELAGE STA 1008 LBL 15 FUSELAGE TO VERTICAL STAB SKATE ANGLE OTBD SIDE I/A/W SRM 51-40-02-0G-0 AND BOEING DWG # 147A0030 REV: - A-TAG # A53993