What was found
DURING D-CHECK, RT FUSELAGE SIDE SKIN FOUND CHAFED AND CORRODED FROM WING FILLET PANEL AT STA 813 AND LONG 26R. REPAIRED DAMAGED AREA IAW DAC TELEX SVC-MSP-0335/DLP DATED 6 MAY 96.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING D-CHECK, RT FUSELAGE SIDE SKIN FOUND CHAFED AND CORRODED FROM WING FILLET PANEL AT STA 813 AND LONG 26R. REPAIRED DAMAGED AREA IAW DAC TELEX SVC-MSP-0335/DLP DATED 6 MAY 96.