What was found
FUSELAGE EXTERNAL SKIN SHOWS CRACK (0.500 IN LENGTH) AT STA -13.000, L-1DR. CUT OUT DAMAGED SKIN PER SRM 53-2-1 FIG 7 SHEET 4.5. INSTALLED FILLER AND DOUBLER AND NEW FASTENERS PER SRM 51-20-20D PG 9.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE EXTERNAL SKIN SHOWS CRACK (0.500 IN LENGTH) AT STA -13.000, L-1DR. CUT OUT DAMAGED SKIN PER SRM 53-2-1 FIG 7 SHEET 4.5. INSTALLED FILLER AND DOUBLER AND NEW FASTENERS PER SRM 51-20-20D PG 9.