What was found
CRACK IN FUSELAGE SKIN AT THE UPPER CORNER OF L-2 DOOR HINGE CUTOUT. DAMAGED MATERIAL REMOVED, FABRICATED REPAIR DOUBLER OF 301 1/2 HARD 2660361 AND FILLER 2024-T3 .071 QQA250/5 R700681. INSTALLED REPAIR IAW 53-69-01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK IN FUSELAGE SKIN AT THE UPPER CORNER OF L-2 DOOR HINGE CUTOUT. DAMAGED MATERIAL REMOVED, FABRICATED REPAIR DOUBLER OF 301 1/2 HARD 2660361 AND FILLER 2024-T3 .071 QQA250/5 R700681. INSTALLED REPAIR IAW 53-69-01.