What was found
FUSELAGE EXTERIOR SKIN CRACKED 1/2 INCH LONG AT STA 1746 L15L. REMOVED DAMAGED AREA FAB`D FILLER, DOUBLER AND FINGER DOUBLER AND INSTALLED IAW SRM 53-2-1 AND 53-2-1 FIG 7.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE EXTERIOR SKIN CRACKED 1/2 INCH LONG AT STA 1746 L15L. REMOVED DAMAGED AREA FAB`D FILLER, DOUBLER AND FINGER DOUBLER AND INSTALLED IAW SRM 53-2-1 AND 53-2-1 FIG 7.