# SDR SWIA2026040277002

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: April 2, 2026
- Submitted: September 1, 2026
- Operation: Air carrier
- Aircraft: [N477CA](https://openairdocs.org/aircraft/N477CA), registered now
- Make and model: Cndair CL6002B19
- Aircraft serial: 7670
- Aircraft time: 39,206 hours, 38,058 cycles
- System (JASC): [5330 · Fuselage Main, Plate/Skin](https://openairdocs.org/jasc/5330)
- Part: Skin
- Condition: Gouged
- 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/SWIA2026040277002

## Discrepancy

MULTIPLE DAMAGES TO FUSELAGE SKIN BETWEEN BS 513 - 544, S6R & 10R. DUE TO FALLING DEBRIS IN HANGER.SPOT1: GOUGE/DENT MEASURING 1.1" LENGTH, 1.1" WIDTH, 0.052" DEPTH. SPOT 2: GOUGE MEASURING 0.700" IN LENGTH, 0.060" WIDTH, 0.007" DEPTH. SPOT 3: GOUGE MEASURING 0.600 LENGTH, 0.200" WIDTH, 0.010" DEPTH.  SPOT 4: GOUGE/ DENT MEASURING 1.1" LENGTH, 1.0" WIDTH, 0.045" DEPTH. SPOT 5: GOUGE MEASURING 0.900" LENGTH, 0.060" WIDTH, 0.005" DEPTH. SPOT 6: GOUGE/DENT MEASURING 1.0" LENGTH, 0.070" WIDTH, 0.009" DEPTH.PLOT, MAP, AND EVALUATE DAMAGE IF WITHIN ACCEPTABLE LIMITS OR REWORKED, ELIMINATE EVIDENCE USING STANDARD ACFT PRACTICES.PERFORMED MAJOR REPAIR ON MULTIPLE DAMAGES TO FUSELAGE SKIN BETWEEN BS 513.- 544 AND S6R AND S10R. DUE TO FALLING DEBRIS IN HANGER IAW REO 601R-51-00-309 REV. -B DATED 2026-05-20  AND REO 601R-53-00-944 REV-.

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