# SDR YENA2026070900558

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: July 5, 2026
- Submitted: July 10, 2026
- Operation: Air carrier
- Aircraft: [N568JB](https://openairdocs.org/aircraft/N568JB), registered now
- Make and model: Airbus A320-232
- Registry model: [Airbus A320-232](https://openairdocs.org/model/airbus-a320-232) (OpenAirDocs)
- Aircraft serial: 02063
- Aircraft time: 84,031 hours, 30,499 cycles
- System (JASC): [5330 · Fuselage Main, Plate/Skin](https://openairdocs.org/jasc/5330)
- Part: Skin
- Condition: Cracked
- Location: Zone 100
- Stage of operation: IN
- How discovered: V
- Nature of condition: O
- Precautionary procedure: K
- FAA source: FAA Service Difficulty Reporting System (https://sdrs.faa.gov/)
- Page: https://openairdocs.org/sdr/YENA2026070900558

## Discrepancy

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

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