What was found
CRACK WAS FOUND AT FUSELAGE SKIN UPPER FWD CORNER, DOOR JAMB BS 375 BETWEEN LONGERONS 19-20R, REPAIRED IAW ETI-88-15-261, REV ORIG AND ER/A 536516-14AD, REV ORIG.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK WAS FOUND AT FUSELAGE SKIN UPPER FWD CORNER, DOOR JAMB BS 375 BETWEEN LONGERONS 19-20R, REPAIRED IAW ETI-88-15-261, REV ORIG AND ER/A 536516-14AD, REV ORIG.