What was found
FOUND .25 INCH CRACK ON FUSELAGE SKIN AT BS 160 LONGERON 23L. CUT OUT CRACKED AREA, FABRICATED REPAIR DOUBLERS AND INSTALLED IAW DCI SRM 53-01 FIGURE 38, DRAWING 3R09530129 AND EO 09-5330-E1714.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FOUND .25 INCH CRACK ON FUSELAGE SKIN AT BS 160 LONGERON 23L. CUT OUT CRACKED AREA, FABRICATED REPAIR DOUBLERS AND INSTALLED IAW DCI SRM 53-01 FIGURE 38, DRAWING 3R09530129 AND EO 09-5330-E1714.