What was found
R/H FUSELAGE STA 259.5 STR 20R LEADING EDGE OF SKIN DOUBLER REPAIR IS BENT/ CONTOUR IS DEFORMED. 43 AND BS 277, S-18R AND S-23R IN ACCORDANCE WITH PART 2 OF ECRA CYCLES. NOTE TO PLANNING: THIS ECRA IS BEING EVAL. FOR DAMAGE TO INSPECTION CRITERIA WILL BE INCLUDED IN PART 2 AT THE CONCLUSION 5331-03028 ON OR BEFORE THE AIRCRAFT REACHING 50,000 TOTAL FLT LERANCE WHICH WILL REQUIRE REPEAT/SUPPLEMENTAL INSPECTIONS. THE PERFORMED INTERIM REPAIR PER ECRA 5331-03028. INTIATED DTA DIP T O PERFORM AN INSPECTION OF THE FUSELAGE SKIN REPAIR BETWEEN BS 2 PLACED ON DIP TO PERFORM AN INSPECTION OF THE FUSELAGE SKIN TOMC-APPROVAL FROM SC1ELBYC COMMENT REPAIR BETWEEN BS 243 AND BS 277, S-18R AND S-23R IN ACCORDANCE WITH PART 2 OF EC/RA 5331-03028 ON OR BEFORE THE AIRCRAFT REACHING 50,000 TOTAL FLIGHT CYCLES IAW ECRA 5331-03028 VERIFIED CKD OK RECORDS UPDATE RECORDS UPDATE QC QC REVIEW T/A: ON OR BEFORE 50,000 TAFC...LN/U253409 REF PLN/ENG LP 4694023