What was found
REF F/C N/R 9720302 AND EA 5510-01843 R/H STAB INSPAR LOWER SKIN CRACKED AT STA 101.9 ABOUT 21" FROM FRONT SPAR R/H HORIZONTAL STAB LOWER INSPAR SKIN AT STA 101.90 HAS BEEN REP AIRED IAW ECRA 5511-01089 AN SRM 55-10-01 REP 11 INSP THRESHOLD AT 56000 TOTAL FLT CYCS FOLLOWED BY REPEAT INSPS AT EACH SUBSEQUENT 9000 CYCS PER STEP 5.A TABLE 204 ACCOMPLISH A PERMANENT REPAIR ON OR BEFORE 29 2022 PLANNING TO CONTACT ENGINEERING AFTER 29 NOV 2021 BUT BEFORE 29 DEC 2021 FOR THE PERMANENT REPAIR TOMC APPROVED DIP REF EC/RA 5511-01089 PART 1 STEP 3, ACCOMPLISH A PERMANENT REPAIR ON OR BEFORE 29 JAN 2022.PLANNING TO CONTACT ENGINEERING AFTER 29 NOV 2021 BUT BEFORE 29 DEC 2021 FOR THE PERMANENT REPAIR.? NOTE TO PLANNING: THIS ECRA IS BEING EVALUATED FOR DAMAGE TOLERANCE UNDER 14CFR 26.43(D) AND WILL LIKELY BE MADE PERMANENT WITH REPEAT INSPECTIONS. TOMC-APPROVAL FROM SC1ELBYC COMMENT REVIEWED AND APPROVED. QC REVIEW QC REVIEW INSPECTIONS CREATED BY AUTODIP PENDING AIRCRAFT RECORDS AUDIT & UPDATE.