# SDR DALA2024123112107

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: December 27, 2024
- Submitted: December 31, 2024
- 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): [5730 · Wing, Plate/Skin](https://openairdocs.org/jasc/5730)
- Part: Skin
- Condition: Cracked
- Location: Zone 600
- 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/DALA2024123112107

## Discrepancy

RIGHT WING, #5 SLAT TRACK CUT OUT HAS A CRACK AT UPPER OUTBOARD CORNER. VERIFIED BY HFEC AT .236 INCHES LONG. MARKED/PHOTO. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0679:5741-2001-LH/020 00163 REPAIRED PER ER/A 602228-14TR REV A SECTION I. NR 00163. R/H TRACK 5. CRACK LENGTH .236". TRIM OUT LENGTH .600" SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0679:5741-2001-LH/020 00163 REPAIRED PER ER/A 602228-14TR REV A SECT ION I. NR 00163. R/H TRACK 5. CRACK LENGTH .236". TRIM OUT LENGTH .600". (LP# 0730710)

---
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.