What was found
WHILE AT VT MAE BFM REF N/R #0013859 (EA 5341-01231 REV ORIG) DURING HFEC INSPECTION OF THE LH FR68WEB AT DOOR STOP FITTING #1 A CRACK INDICATION WAS NOTED AT STGR 22 WEB HORIZONTAL FLANGE UPPER & BOTTOM RADUIS, CRACK LENGHT APPROX 0.663IN BEFORE 29-MAR-2022. ACCOMPLISHED INTERIM REPAIR AT FR68 FLANGE WEB STGR22 IAW ECRA 5341-01271 PER PART 1 WITH NO DEVIATIONS. ACCOMPLISH A PERMANENT REPAIR PER PART 3 OF LATEST REVISION OF ECRA 5341-01271 ON OR APPROVED FOR CARRY TO ACCOMPLISH A PERMANENT REPAIR PER PART 3 TOMC-APPROVAL FROM SC1ELBYC COMMENT OF LATEST REVISION OF EC/RA 5341-01271 ON OR BEFORE 29-MAR-2022." PERMANENT REPAIR TBD BY AIRBUS/EG. Q/C REVIEWED. Q/C REVIEWED. INSPECTIONS CREATED BY AUTODIP PENDING AIRCRAFT RECORDS AUDIT & UPDATE.