As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LEFT WING INBD L/E PANEL 516 HB IS CHAFED. BLENDED AREA IAW SRM 57-00-01 VOL I, CHECKED LIMITS, FOUND TO BE OUT OF LIMITS, ORIG THICKNESS .090 BLEND LIMITS 20 PERCENT OR .072 WAS .067 IAW SRM 51-31- 01 VOL II FIG 1. FABRICATED DOUBLER IAW SRM 57-00-01 VOL I FIG 4 PG 12. ALODINED AND PRIMED IAW SRM 51-21-01 VOL II. INSTALLED DOUBLER IAW SRM 57-00-01 VOL I FIG 4 PG 12.