What was found
AT C-CHECK, UPPER FUSELAGE STA 1038 RT BETWEEN LONGS 2 AND 3 SPLICE FITTING ATTACH FUSELAGE SKIN HAS .75 INCH CRACK. REMOVED AND REPLACED FITTING PER SRM 51-1-20.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AT C-CHECK, UPPER FUSELAGE STA 1038 RT BETWEEN LONGS 2 AND 3 SPLICE FITTING ATTACH FUSELAGE SKIN HAS .75 INCH CRACK. REMOVED AND REPLACED FITTING PER SRM 51-1-20.