What was found
(A3NB-53-4-6179) AFT CRG COMPT: STR42 LH BETWEEN FR63 AND FR64 H AS CORROSION EVIDENCE. DOT 61-055 IAW SRM 51-42-11/001 AND NDT''D CUT OUT IAW NTM 51-10-08 PART 6. SRM 53-00-13-300-001 FIG 001 SHEET 5. INSTALLED STRINGER REPAIR INSPECTION THRESHOLD FROM TIME OF ADL/REPAIR EMBODIMENT FC FABRICATED REPAIR PARTS: STRINGER DAN50B-11 BATCH 0003841248 AND IAW SRM 53-0013-300-001 FIG 001 SHEETS 02,03,04,05 & 06. THIS 60000 / FH 120000 WHICHEVER ACHIEVED FIRST SUBSEQUENT INSP TBD. COUPLING A53986212 BATCH 0003839519 IAW SRM 53-41-13-07-A AND REPAIR REQUIRES REPETITIVE INSP IAW SRI 53-00-13-205-001 TABLE 6 WORK ACCOMPLISHED BY VT MAE EMP V934344. BLENDED CORROSION ON STR42L @ FR63 AND 64 IAW SRM 51-74-00. ORG MATERIAL 0.110 AFTER REWORK 0.080 L=12", W=.8", D=0.030 OUT OF LIMITS IAW SRM 53-41-13-283-002 FIG 001 SHT 01. CUT OUT DAMAGE OK TO CARRY PER SRI 53-00-13-205-001, REQUIRES INSPECTION AT TOMC-APPROVAL FROM SC1ELBYC COMMENT 60000 TOTAL F/C''S OR 120000 TOTAL F/H''S, WHICH EVER OCCURS FIRST. TOMC APPROVED : QC REVIEWED. TOMC APPROVED : QC REVIEWED. INSPECTIONS CREATED BY AUTODIP PENDING AIRCRAFT RECORDS AUDIT & UPDATE.