# SDR ASOA200900088

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: January 19, 2009
- Submitted: January 23, 2009
- Operation: Air carrier
- Aircraft: [N717EV](https://openairdocs.org/aircraft/N717EV), registered now
- Make and model: Cndair CL6002C10
- Aircraft serial: 10088
- Aircraft time: 15,421 hours, 10,325 cycles
- System (JASC): [5553 · Vertical Stabilizer, Attach Fittings](https://openairdocs.org/jasc/5553)
- Part: Drag Angle
- Condition: Cracked
- Location: Fuselage
- 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/ASOA200900088

## Discrepancy

RT DRAG ANGLE (VERTICAL - FUSELAGE) APPEARS CRACKED.   PERFORMED REPAIR TO CRACKED LT DRAG ANGLE (VERTICAL FUSELAGE) AS PER REO 670-55-31-018 STEPS 1-5.  PERFORMED EDDY CURRENT INSPECTION DRAG ANGLE IAW NDTM 51-20-006.  ANGLE IS CONFIRMED CRACKED AND MARKED.  CUT OUT DAMAGED AREA.  COMPLIED WITH NDT OF CUTLINE PER STEP 3 OF REO 670-53-31-018.  FABRICATED DOUBLER AND FILLER FOR LT DRAG ANGLE REPAIR IAW REO 670-55-31-018.  INSTALLED ALL REPAIR PARTS AND FASTENERS EXCEPT 2 EA FASTENERS ON FWD EDGE OF BOTTOM LEG OF DRAG ANGLE.

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