What was found
DURING HEAVY MAINTENANCE, CRACK INDICATION FOUND (BY ROTOTEST INSPECTION) IN OPEN FASTENER HOLE LOCATED ON FRAME 35 (FUSELAGE SIDE SHELL) AFT POSITION BELOW STRG 30 R H SIDE, CRACK DIRECTION: 07 OCLOCK, D1-D2= 0.165 INCH APPROX, AD RELAT ED TASK CARD NO. A320-53-1372-01; (RESOLVED ON W/O: 1457737 TASKCARD: NR-00054 ) REF AEROMAN NR 2026-299153 WO 2026 196/1 ACCOMPLISHED REPAIR ON HOLE H2, LOCATED ON FRAME 35 (FUSELAGE SIDE SHELL) AFT POSITION BELOW STRG 30 RH SIDE, ACCORDANCE WITH AEROMAN EA 53-0042-26 PART 0 (COVER AND PART 1, PART 2, PART 3) AND RDAF 81803369/003/2026 ISSUED A, EC NO: A26-505-01. THIS REPAIR IS CATEGORY B, FOR ANGLE FITTING,AFT SKIN AND FRAME FLANGE LAYERS, INSPECTION THRESHOLD AT 67,700FC/135,400FH(WHICHEVER OCCUS FIRST), INSPECTION INTERVAL:TBD, INSPECTION METHOD:TBD, FWD SKIN LAYER: INSPECTION THRESHOLD:13,100FC/26 ,200FH (WHICHEVER OCCURS FIRST), INSPECTION INSTERVAL:6,500FC/13,000FH (WHICHEVER OCCURS FIRST), INSPECTION METHOD:DVI OF FUSELAGE SKIN AT FR35 AND 10CM FWD AT LEVEL OF STRINGER 30, INTERNAL SIDE IAW NTM 51-90-00