# SDR DALA2025011000226

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: January 7, 2025
- Submitted: January 10, 2025
- Operation: Air carrier
- Aircraft: [N104DU](https://openairdocs.org/aircraft/N104DU), 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: 50023
- Aircraft time: 15,111 hours, 7,026 cycles
- System (JASC): [5330 · Fuselage Main, Plate/Skin](https://openairdocs.org/jasc/5330)
- Part: Skin
- Condition: Corroded
- Location: Zone 200
- 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/DALA2025011000226

## Discrepancy

WHILE ACCOMPLISHING AFT LEFT PASSENGER DOOR CORROSION INSPECTION PER AMDS 5331-01297-02A, FOUND CORROSION AT/AROUND HOLES 12OL. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 047-0001:5331-01297- 02A/002 00247 REPAIRED PER ER/A 622582-14 PRI REV 0, REV 1, AND ER/A 622582-14 ORIGINAL, ORIGINAL THICKNESS .125 MIN MAX MATERIAL REMOVED .063, REMAINING THICKNESS .062. F SUMMARY SEE NR FOR ADDITIONAL INFORMATION 047-0001:5331-01297-02A/002 00247 REP AIRED PER ER/A 622582-14 PRI REV 0, REV 1, AND ER/A 622582-14 ORIGINAL, ORIGINAL THICKNESS .125 MIN MAX MATERIAL REMOVED .063, REMAINING THICKNESS .062. THE W IP STATING THERE WAS WORK ACCOMPLISHED ON REV 2 WAS AN ERROR, THE WORK WAS ACCOMPLISHED ON REV 1. (LP# 0748965)

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