What was found
CRACKED RIB , LT WING OTBD L/E CAVITY INNER RIB , NEAR OSS 514 , ACCESS PANEL 521HB. INSTALL NEW RIB IAW SRM 51-40-02-0G, REV 94, AND DWG 114T2205, SH 1, REV B.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACKED RIB , LT WING OTBD L/E CAVITY INNER RIB , NEAR OSS 514 , ACCESS PANEL 521HB. INSTALL NEW RIB IAW SRM 51-40-02-0G, REV 94, AND DWG 114T2205, SH 1, REV B.