# SDR ASOA200901240

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: November 5, 2009
- Submitted: November 12, 2009
- Operation: Air carrier
- Aircraft: [N752EV](https://openairdocs.org/aircraft/N752EV), registered now
- Make and model: Cndair CL6002C10
- Aircraft serial: 10166
- Aircraft time: 12,610 hours, 8,629 cycles
- System (JASC): [5534 · Vertical Stabilizer Miscellaneous Structure](https://openairdocs.org/jasc/5534)
- Part: Drag Angle
- Part number: AV67021186003
- Condition: Cracked
- Location: Vertical Stab
- Stage of operation: IN
- How discovered: E
- Nature of condition: O
- Precautionary procedure: K
- FAA source: FAA Service Difficulty Reporting System (https://sdrs.faa.gov/)
- Page: https://openairdocs.org/sdr/ASOA200901240

## Discrepancy

LT SIDE VERTICLE STAB TO FUSELAGE ATTACHMENT AFT DRAG ANGLE CRACKED FWD SIDE AT 67.5 REAR SPAR DATUM.  REMOVED CRACKED LT SIDE AFT DRAG ANGLE IAW SRM 51-42-21, 51-42-22, AND 51-42-13.  DRILLED UP AND COUNTERSANK NEW LT AFT DRAG ANGLE AS  SRM 51-40-11.  OK TO INSTALL -003.  INSTALLED NEW -003 ANGLE IAW SRM 51-42-22, 51-42-21, 51-42-13.

---
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.