# SDR DALA2025042203164

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: April 17, 2025
- Submitted: April 22, 2025
- Operation: Air carrier
- Aircraft: [N138DU](https://openairdocs.org/aircraft/N138DU), 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: 50057
- Aircraft time: 7,593 hours, 3,510 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/DALA2025042203164

## Discrepancy

FUSELAGE SKIN HAS CORROSION AROUND THE FWD CARGO DOOR LOWER SCUFF PLATE ATTACH FASTENERS HOLES 13OL, 14OL, 15OL, 19OL, 21OL. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 067-0001:5331-01297- 01C/001 00256 COMPLIED WITH ER/A PRI 625595-14 REV. 0, REV. 1, AND FINAL ER/A 625595-14 REV. ORIGINAL. SECTION 1 TIME LIMITED REPAIR. ORIGINAL THICKNESS IS 0.125, MATERIAL REMOVED IS BETWEEN 0.018 AND 0.001, MATERIAL REMAINING IS BETWEEN 0.107 AND 0.124 AND REF. ER/A 625660-14 REV. ORIGINAL AND NR# 149 FOR SILL REPLACEMENT. ALL REPETITIVE INSPECTION TO BE ACCOMPLISHED ON LOG 0908288. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 067-0001:5331-01297-01C/001 00256 COM PLIED WITH PRI 625595-14 REV A, REV. 0, REV. 1, AND FINAL ER/A 625595-14 REV A. SECTION 1 TIME LIMITED REPAIR. ORIGINAL THINKNESS IS 0.125, MATERIAL REMOVED I S BETWEEN 0.018 AND 0.001, MATERIAL REMAINING IS BETWEEN 0.107 AND 0.124 AND RE F. ER/A 625660-14 REV. ORIGINAL AND NR# 149 FOR SILL REPLACEMENT. ALL REPETITIVE. (LP# 0918303)

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