What was found
CRACKED STRUT, LT WING OTBD L/E CAVITY, INNER RIB LWR STRUT, NEAR OSS 531, ACCESS PANEL 521HB. INSTALL NEW STRUT IAW SRM 51-40-02-0G, REV.94, DWG 114T2206, SH 1, REV B, & DWG 112T2000, SH 12, REV B.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACKED STRUT, LT WING OTBD L/E CAVITY, INNER RIB LWR STRUT, NEAR OSS 531, ACCESS PANEL 521HB. INSTALL NEW STRUT IAW SRM 51-40-02-0G, REV.94, DWG 114T2206, SH 1, REV B, & DWG 112T2000, SH 12, REV B.