What was found
CRACK ON RH WING UPPER SKIN PANEL 2 AT FRONT SPAR PITCH LOAD FITTING BETWEEN WSTA 375.8 / WSTA 404.4.(IT WAS REPAIRED IN ACCORDANCE WITH TLS EO NO. 6757A024)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK ON RH WING UPPER SKIN PANEL 2 AT FRONT SPAR PITCH LOAD FITTING BETWEEN WSTA 375.8 / WSTA 404.4.(IT WAS REPAIRED IN ACCORDANCE WITH TLS EO NO. 6757A024)