What was found
(A3NB-53-4-6179) AFT CRG COMPT: STR41 LH BETWEEN FR63 AND FR64 H AS CORROSION EVIDENCE DOT 61-056. 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 60000 FABRICATED REPAIR PARTS: STRINGER DAN50B-11 BATCH 0003841248 AND IAW SRM 53-00-13-300-001 FIG 001 SHEETS 02,03,04,05 & 06. THIS / FH 120000 WHICHEVER ACHIEVED FIRST, SUBSEQUENT INSPECTIONS 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 VTMAE EMP V934344. BLENDED CORRISION ON STR41L @ FR63 AND 64 IAW SRM 51-74-00. ORG MATERIAL 0.110 AFTER REWORK 0.089 L=11.5" W=0.8" D=0.021 OUT OF LIMITS IAW SRM 53-41-13-283-002 FIG 001 SHT 01. CUT OUT DAMAGE OK TO DIP REPAIR OF CORROSION AT STR 41 LH BETWEEN FR63 AND FR64 TOMC-APPROVAL FROM SC1ELBYC COMMENT REF SRMS 53-41-13-283-002 AND 53-00-13-300-001. REF SRI 53-00-13-205-001, MUST ACCOMPLISH RECHECK WITHIN 60000 FLIGHT CYCLES-120000 FLIGHT HOURS FROM REPAIR EMBODIMENT WHICHEVER OCCURS FIRST. AT TIME OF 1ST INSPECTION, RECHECK SRI AND APPLY APPLICABLE RECHECK LIMITS. INSPECTIONS CREATED BY AUTODIP PENDING AIRCRAFT RECORDS AUDIT & UPDATE. QC REVIEWED QC REVIEWED