What was found
INSPECTION FOUND A 1.75 INCH AND 5.75 INCH CRACK IN RT FUSELAGE SKIN BETWEEN BS 188 AND 251, WL 207 TO 234. THE CRACKED AREA WAS CUT OUT. A FILLER AND DOUBLER WERE FABRICATED AND INSTALLED IAW EA 5310-01188.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 1.75 INCH AND 5.75 INCH CRACK IN RT FUSELAGE SKIN BETWEEN BS 188 AND 251, WL 207 TO 234. THE CRACKED AREA WAS CUT OUT. A FILLER AND DOUBLER WERE FABRICATED AND INSTALLED IAW EA 5310-01188.