What was found
AT D-CHECK, FUSELAGE CRACKED AT BS 251.6 BETWEEN STR 15L AND STR 16L. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER, 8 INCHES BY 9 INCHES AND FILLER, 1.5 INCH BY .5 INCH, PER SRM 53-30-3.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AT D-CHECK, FUSELAGE CRACKED AT BS 251.6 BETWEEN STR 15L AND STR 16L. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER, 8 INCHES BY 9 INCHES AND FILLER, 1.5 INCH BY .5 INCH, PER SRM 53-30-3.