# SDR ASOA200801587

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: December 1, 2008
- Submitted: December 5, 2008
- Operation: Air carrier
- Aircraft: [N716EV](https://openairdocs.org/aircraft/N716EV), registered now
- Make and model: Cndair CL6002C10
- Aircraft serial: 10084
- Aircraft time: 15,320 hours, 10,304 cycles
- System (JASC): [5534 · Vertical Stabilizer Miscellaneous Structure](https://openairdocs.org/jasc/5534)
- Part: Drag Angle
- Condition: Cracked
- Location: Vertical Stab
- 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/ASOA200801587

## Discrepancy

LT VERTICAL FWD DRAG ANGLE APPEARS CRACKED.  PERFORMED EDDY CURRENT INSPECTION OF LEFT FORWARD VERTICAL STAB TO FUSELAGE DRAG ANGLE IAW CRJ 700 NDTM 51-20-006.  DRAG ANGLE CONFIRMED CRACKED AND MARKED.  LT DRAG ANGLE REPAIRED PER REO 670-55-31-018.  REMOVED PAINT IAW CRJ SRM 51-12-00, VERIFIED CORROSION TO BE OUT OF LIMITS IAW CRJ 200 SRM 53-00-00 FIG 102.  REPAIR OR REPLACEMENT REQUIRED.  REMOVED FLOOR LANDING PLATE, LOCATED AND DRILLED NEW PLATE FS 559+112 - 621 IAW CRJ 200 SRM 51-42-06.  CUT NEW FLOOR LANDING PLATE IAW BOMBARDIER REO 601R-53-61-593A STEPS 1 AND 2.

---
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.