What was found
LONGERON 9L HAD A .25 INCH CRACK ON UPPER FLANGE AT ATTACHMENT TO FUSELAGE FRAME AT STA 617. SPLICED IN NEW LONGERON PER SRM 53-02, FIG 18. CHECK-C 3-15-99 STL.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LONGERON 9L HAD A .25 INCH CRACK ON UPPER FLANGE AT ATTACHMENT TO FUSELAGE FRAME AT STA 617. SPLICED IN NEW LONGERON PER SRM 53-02, FIG 18. CHECK-C 3-15-99 STL.