# SDR QXEA2010072100427

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: July 20, 2010
- Submitted: July 21, 2010
- Operation: Air carrier
- Aircraft: [N612QX](https://openairdocs.org/aircraft/N612QX), registered now
- Make and model: Cndair CL6002C10
- Aircraft serial: 10042
- Aircraft time: 22,531 hours, 16,588 cycles
- System (JASC): [5530 · Vertical Stabilizer](https://openairdocs.org/jasc/5530)
- Part: Drag Angle
- Condition: Cracked
- Location: Vertical Stab
- Stage of operation: IN
- How discovered: 9
- Nature of condition: O
- Precautionary procedure: K
- FAA source: FAA Service Difficulty Reporting System (https://sdrs.faa.gov/)
- Page: https://openairdocs.org/sdr/QXEA2010072100427

## Discrepancy

RT V-STAB TO FUSELAGE ATTACHMENT DRAG ANGLE IS POSSIBLY CRACKED. APPROX STA 1240 HFEC INSPECTED SUSPECTED CRACK IAW NDTM PART 6, 53-00-000-250-A01.  CRACK INDICATION NOTED, APPROX 1.2" LONG.  REMOVED FASTENERS AND CUT OUT DAMAGE ON ATTACHMENT DRAG ANGLE IAW REO 670-55-31-018.  HFEC INSPECTED AT CUT OUT FOR CRACK IAW NDTM PART 1, 51-20-006, NO CRACK NOTED.  FABRICATED FILLER ANGLE AND ANGLE DOUBLER IAW REO 670-55-31-018. FAY SEALED FILLER AND DOUBLER AND INSTALLED NEW DOUBLER IAW REO 670-55-31-018.

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