What was found
PREVIOUS REPAIR LOCATED AT FRAME 80/82 AFT PRESSURE BULKHEAD FORWARD SIDE CIRCUMFERENTIAL STRAP AND FRAME WEB REPAIR BETWEEN STR 48 LT AND 48 RT WITH 2 EA FRAME WEB REPAIR PLATES, 2 CIRCUMFERENTIAL REPAIR SPLICE STRAPS AND 1 CIRCUMFERENTIAL REPAIR SECTION REPAIR NOT IAW SRM REQUIREMENTS. REMOVED PREVIOUS INSTALLED LOCK FASTENER COLLARS ON REPAIR AT FR 80/82 BETWEEN STR 48 LT TO STR 48 RT CIRCUMFERENTIAL STRAP AND INSTALLED CORRECT COLLARS IAW FEDEX EA 6-5310-121308, RELEASE DATE 18 JUNE, 2008. THIS IS AN AIRBUS REPAIR AND IS A RESULT OF AGING AIRCRAFT INSPECTION.