What was found
EXTERIOR FUSELAGE SECTION 41, LEFT FUSELAGE SKIN CRACKED AT FASTENER HOLE LOCATION, STA 227.8 AND WL 214. POSSIBLE CAUSE OF THE CRACK WAS SKIN FATIGUE. (X)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
EXTERIOR FUSELAGE SECTION 41, LEFT FUSELAGE SKIN CRACKED AT FASTENER HOLE LOCATION, STA 227.8 AND WL 214. POSSIBLE CAUSE OF THE CRACK WAS SKIN FATIGUE. (X)