What was found
WHILE IN FOR D-CHECK, MAINTENANCE FOUND RT FRAME CHORD SPLICE FITTING CORRODED AT STA 99 AS SEEN THROUGH PANEL 90B. MAINTENANCE FABRICATED SPLICE AND INSTALLED IAW SRM 51-1-20D, 51-1-20, 51-1-21, AND DC8-53-1476.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
WHILE IN FOR D-CHECK, MAINTENANCE FOUND RT FRAME CHORD SPLICE FITTING CORRODED AT STA 99 AS SEEN THROUGH PANEL 90B. MAINTENANCE FABRICATED SPLICE AND INSTALLED IAW SRM 51-1-20D, 51-1-20, 51-1-21, AND DC8-53-1476.