As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FUSELAGE, LEFT EXTERIOR SURFACE LONGERON END CAP FITTING AT STA 1521 LONGERON 30L FOUND CRACKED. 08/31/07 REMOVED AS PER SRM 51-33-01 VOLUME II. NEW SPLICE END CAP FITTING FABRICATED AS PER DOUGLAS DRAWING AEA7643 AND INSTALLED AS PER SRM 51-33-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.