What was found
(CAN) TWO INCH CRACK WAS FOUND ON OUTER FUSELAGE BETWEEN STA 727A, 727B AT STR. 16L. FUSELAGE CRACK REPAIRED IAW SRM 53-30-3 FIG.48 SHEET 34 DETAIL XII. TIMES- 59472:22 CYCLES- 54285.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
(CAN) TWO INCH CRACK WAS FOUND ON OUTER FUSELAGE BETWEEN STA 727A, 727B AT STR. 16L. FUSELAGE CRACK REPAIRED IAW SRM 53-30-3 FIG.48 SHEET 34 DETAIL XII. TIMES- 59472:22 CYCLES- 54285.