What was found
A 1 INCH LONG CRACK IN FUSELAGE SKIN AT BS 737E PLUS 3 INCHES, S-24L. FILLER AND DOUBLER INSTALLED PER SRM 53-00-01 FIG 201.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
A 1 INCH LONG CRACK IN FUSELAGE SKIN AT BS 737E PLUS 3 INCHES, S-24L. FILLER AND DOUBLER INSTALLED PER SRM 53-00-01 FIG 201.