What was found
CRACK ON EXTERNAL FUSELAGE SKIN BS 1309, LONGERONS 6R TO 7R. THE CRACK WAS .500 INCH. AREA WAS REPAIRED IAW ER/A 559535-14, REV ORIG, AND ETI -88-17-206, REV 2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK ON EXTERNAL FUSELAGE SKIN BS 1309, LONGERONS 6R TO 7R. THE CRACK WAS .500 INCH. AREA WAS REPAIRED IAW ER/A 559535-14, REV ORIG, AND ETI -88-17-206, REV 2.