What was found
REAR FUSELAGE INTERNAL STRUCTURE FOUND S-39R WEB PLATE DEFORM BETWEEN FR86 & FR87 AREA INSTALLED THE NEW STRAP WITH RIVETS I.A.W A300-600F SRM 51-72-10-001, PAGE.2 AND 51-40-21- 001, PARA6, PAGE.7B-23
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
REAR FUSELAGE INTERNAL STRUCTURE FOUND S-39R WEB PLATE DEFORM BETWEEN FR86 & FR87 AREA INSTALLED THE NEW STRAP WITH RIVETS I.A.W A300-600F SRM 51-72-10-001, PAGE.2 AND 51-40-21- 001, PARA6, PAGE.7B-23