What was found
INSPECTION FOUND A 0.15 CRACK IN FUSELAGE SKIN AT STA 1338, BELOW L5L. THE CRACK WAS CUT OUT. DOUBLERS AND FILLER PLUG WERE INSTALLED IAW DAC DRAWING J060138.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 0.15 CRACK IN FUSELAGE SKIN AT STA 1338, BELOW L5L. THE CRACK WAS CUT OUT. DOUBLERS AND FILLER PLUG WERE INSTALLED IAW DAC DRAWING J060138.