What was found
DURING VISUAL INSPECTION AFTER SCUFF PLATE REMOVAL, FOUND SCRIBE LINES IN THE AREA UNDER SCUFF PLATE AT FUSELAGE SKIN 1L DOOR FWD & AFT LOWER CORNER. LOCATED BTW BS 287 & 347 BTW S20L & 21L. THIS IS A CATEGORY B REPAIR. PERFORMED INTERIM REPAIR OF FUSELAGE SKIN 1L DOOR, FWD AND AFT CORNER CRACKS & LOWER PERIMETER SCRIBE LINES AS PER EC/RA 5331- INTERIM REPAIR OF THE FUSELAGE SKIN 1L DOOR WAS SATISFACTORY. PERFORMED & INSPECTED PER ECRA 5331-03104. PER ECRA 5331-03104 AFTER ACCOMPLISHMENT OF INTERIM REPAIR; INITIATE A DTA DIP LOGPAGE TO ACCOMPLISH INSPECTION REQUIREMENTS ON FWD LH ENTRY DOOR CUTOUT LOWER CORNER REPAIR AREA AS PER PART 2 OF LATEST REVISION OF EC5331-03104 ON OR BEFORE THE AIRCRAFT REACHES 37,500 TOTAL FLIGHT CYCLES. LOG 8066917 TOMC APPROVED: QC REVIEWED CREATED TO CONTACT ENGINEERING AFTER AIRCRAFT REACHES 32,000.