# SDR DALA2024112511185

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: November 21, 2024
- Submitted: November 25, 2024
- Operation: Air carrier
- Aircraft: [N102DU](https://openairdocs.org/aircraft/N102DU), 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: 50021
- Aircraft time: 13,596 hours, 6,359 cycles
- System (JASC): [5320 · Fuselage Miscellaneous Structure](https://openairdocs.org/jasc/5320)
- Part: Scuff Plate
- 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/DALA2024112511185

## Discrepancy

AFT CARGO DOOR LOWER SCUFF PLATE FASTENER HOLE 3OL HAS CORROSION AT THE HOLE AND SURROUNDING SURFACE. (P)(M). SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 060-0001:5331-01297-02C/006 00240 COMPLIED WITH ER/A 621911-14 PRI REV 0, REV 1, AND ER/A 621911- 14 REV ORIGINAL. ORIGINAL THICKNESS: 0.125" .MAX REMOVED THICKNESS: 0.019" . MINIMUM REMAINING THICKNESS: 0.106". (LP# 0671626)

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.
