What was found
DURING D-CHECK, FOUND THAT THE FUSELAGE SKIN HAS A 40 INCH CREASE AT STA 190 - 229 NEAR LONGERON 24R. COLD FORMED THE DENT PER SRM 53-04, FIG 38, AND INSTALLED A DOUBLER IAW DAC TELEX.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING D-CHECK, FOUND THAT THE FUSELAGE SKIN HAS A 40 INCH CREASE AT STA 190 - 229 NEAR LONGERON 24R. COLD FORMED THE DENT PER SRM 53-04, FIG 38, AND INSTALLED A DOUBLER IAW DAC TELEX.