# SDR DALA2026071304083

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: July 9, 2026
- Submitted: July 13, 2026
- Operation: Air carrier
- Aircraft: [N352NW](https://openairdocs.org/aircraft/N352NW), registered now
- Make and model: Airbus A320-212
- Registry model: [Airbus A320-212](https://openairdocs.org/model/airbus-industrie-a320-212) (OpenAirDocs)
- Aircraft serial: 778
- Aircraft time: 81,941 hours, 39,111 cycles
- System (JASC): [5330 · Fuselage Main, Plate/Skin](https://openairdocs.org/jasc/5330)
- Part: Skin
- Condition: Nicked
- 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/DALA2026071304083

## Discrepancy

FWD FUSELAGE FR13+65MM AND 400MM ABOVE OF LEFT SIDE STRG SKIN PANEL WITH NICK.  PERFORMED PERMANENT FUSELAGE SKIN REPAIR AT FWD FUSELAGE FROM FR 12 +238MM TO FR 13 +155MM, BETWEEN Z-520 AND Z-742 L/H SIDE I.A.W A320 SRM 53-11-11-300-041 PARAG 1 AND PARAG 2A FIGURE 001. NOTE: THIS REPAIR IS CATEGORY B REPAIR AND MUST BE INSPECTED I/ A/W TASK A320 SRM 53-11-11-205-037 PARAG 2 TABLE 001, INSPECTION THRESHOLD FROM TIME OF REPAIR EMBODIMENT: 60000 FC / 120000 FH (WHICHEVER VALUE FC / FH OCCURS FIRST) SUBSEQUENT INSPECTION AT INTERVALS OF: TBD, INSPECTION METHOD: TBD, TBD IN CASE OF AIRCRAFT LIFE EXTENSION MORE THAN 60000 FC / 120000 FH (WICHEVER OCCURS FIRST), A320 SRM REV 158.00 DATED 01-JUN-26. (LP: 1690852, AIRCRAFT WAS GROUNDED)

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