# SDR DALA2025032602233

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: March 21, 2025
- Submitted: March 26, 2025
- Operation: Air carrier
- Aircraft: [N123DQ](https://openairdocs.org/aircraft/N123DQ), registered now
- Make and model: Airbus BD-500-1A10
- Registry model: [Airbus BD-500-1A10](https://openairdocs.org/model/airbus-canada-ltd-ptnrsp-bd-500-1a10) (OpenAirDocs)
- Aircraft serial: 50042
- Aircraft time: 14,156 hours, 6,458 cycles
- System (JASC): [5330 · Fuselage Main, Plate/Skin](https://openairdocs.org/jasc/5330)
- Part: Skin
- Condition: Corroded
- 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/DALA2025032602233

## Discrepancy

FUSELAGE SKIN AT AFT SERVICE DOOR AREA COVERED BY THE LOWER SILL SCUFF PLATE HAS CORROSION AROUND ATTACH FASTENER HOLES 2OL, 4OL , 5OL, 6OL, 8OL, 9OL,10OL, 11OL, 12OL, 13OL . SUMMARY SEE NR FOR ADDITIONAL INFORMATION 022-0001:5331-01297- 02B/001 00260 REPAIRED PER PRI 624617-14 REV 0, PRI 624617-14 REV 1, PRI 624617-14 REV 2, PRI 624617-14 REV 3 AND FINAL ER/A 624617-14 REV ORIGINAL SECTION I. (LP# 0870561)

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