What was found
CRACK ON SUPPORT ANGLE OF ACCESS PANEL 651FB RT WING T/E. REPLACED THE SUPPORT ANGLE LOCATED AT ACCESS PANEL 651FB IAW SRM 51-10-02, ITEM 9, AND DWG 115A2710, SHEET 6, REV B. MEASURE OF CRACK IS: 0.112 INCH.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK ON SUPPORT ANGLE OF ACCESS PANEL 651FB RT WING T/E. REPLACED THE SUPPORT ANGLE LOCATED AT ACCESS PANEL 651FB IAW SRM 51-10-02, ITEM 9, AND DWG 115A2710, SHEET 6, REV B. MEASURE OF CRACK IS: 0.112 INCH.