# SDR VNAA202606300002

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: May 10, 2026
- Submitted: July 1, 2026
- Operation: Air carrier
- Aircraft: [N530EA](https://openairdocs.org/aircraft/N530EA), registered now
- Make and model: Cndair CL6002C10
- Aircraft serial: 10308
- Aircraft time: 34,311 hours, 26,835 cycles
- System (JASC): [5330 · Fuselage Main, Plate/Skin](https://openairdocs.org/jasc/5330)
- Part: Skin
- Part number: CC670331021
- Condition: Damaged
- 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/VNAA202606300002

## Discrepancy

FUSELAGE LIGHTNING STRIKE DAMAGE.  DAMAGE AROUND FASTENER CSK BY NEXT HEAVY MAINTENANCE VISIT (HMV), PERFORM PERMANENT REPAIR PER SRM 53-00-00-201-003-A03 SECTION 5.C.(4) - PERMANENT DISPOSITION TO FUSELAGE SKIN AROUND THE FASTENER COUNTERSINK FOR DAMAGE DEPTH MORE THAN 0.005 IN. (0.13 MM) // ENGINEERING COMMENTS: EVALUATE 53-00-00-201-003 FOR A PERMANENT REPAIR. IF OUT OF LIMITS REMOVE THE DAMAGE IAW SRM 51-12 AND PERFORM A CONDUCTIVITY TEST IAW SRM 51-11-20 SUBMIT A NEW RFTS WITH A DETAILED DAMAGE REPORT WITH CONDUCTIVITY TEST RESULTS DISPLAYED IN A GRID ALONG WITH AN MRT GRID.  LIGHTNING STRIKE DAMAGE ON FUSELAGE FASTENERS BTW FS 201 -  295 AND STRINGER 22L-23L WERE REPAIRED IAW SRM 53-00-00-201-003-A01.

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