# SDR REXA2026062900987

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: June 9, 2026
- Submitted: June 29, 2026
- Operation: Air carrier
- Aircraft: [N153PQ](https://openairdocs.org/aircraft/N153PQ), registered now
- Make and model: Cndair CL6002D24
- Aircraft serial: 15153
- Aircraft time: 41,398 hours, 31,131 cycles
- System (JASC): [5342 · Fuselage, Stabilizer Attach Fittings](https://openairdocs.org/jasc/5342)
- Part: Drag Angle
- Part number: AV67021186003
- Condition: Cracked
- 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/REXA2026062900987

## Discrepancy

THERE IS A POSSIBLE CRACK IN THE RIGHT-HAND VERTICAL STABILIZER DRAG ANGLE.  STRIPPED PAINT FROM FWD DRAG ANGLE IAW CRJ900 SRM 51-26-01-001-001-A01. FOUND FWD DRAG ANGLE TO BE VISUALLY CRACKED 2.35"L,  REMOVED FASTENERS FOR ACCESS FOR REPAIR IAW SRM 51-42-06-001-001-A01 & SRM 51-42-21-001-001-A01.  CUT AWAY DAMAGE AND REMOVED ALL BURRS AND SHARP EDGES ON RT FWD DRAG ANGLE IAW SRM 55-31-00-201-001-A01, STEPS 5B(1), AND 5B(2).  PERFORMED HFEC OF RT VSTAB DRAG ANGLE CUTLINE & UNDERLYING STRUCTURE IAW SRM 55-31-00-201-001-A01 STEP 5B(3). NO INDICATIONS NOTED AT THIS TIME. COMPLIED WITH STEPS 5B(4), 5B(7) & 5B(8) OF SRM 55-31-00-201-001-A01.  COMPLIED WITH STEPS 5B (5,6, AND 11) OF SRM 55-31-00-201-001-A01. COMPLIED

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