# SDR REXA2026062600979

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: June 9, 2026
- Submitted: June 26, 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): [5751 · Ailerons](https://openairdocs.org/jasc/5751)
- Part: Bushing
- Part number: 69057515411
- Condition: Damaged
- Location: Zone 500 Aileron
- 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/REXA2026062600979

## Discrepancy

UPON REMOVAL OF THE LT WING SIDE AILERON BUSHINGS, IT WAS FOUND THAT THE LUG -C- (HINGE NR 2 INBD) WAS PREVIOUSLY O/S & CURRENTLY MEASURES (0.8965").   COMPLIED WITH STEPS NR 1 & 2 OF IAW REO 690-57-51-541, REV -.  ENSURED NO PREVIOUS BLENDING ON WING SIDE AILERON LUG -C-. ENSURED WING SIDE AILERON LUG -C- HAS A FINAL INTERNAL DIAMETER THAT MEASURES (0.8965"). C/W ET ON WING SIDE AILERON OVERSIZED BORE -C- IAW REO 690-57-51-541, REV -.  NO INDICATIONS NOTED.  COMPLIED WITH STEPS 4 & 6(A) OF REO 690-57-51-541 REV-.   ALODINED THE BORE (A044).  FABRICATED ONE O/S AILERON BUSHING, LPI  PERFORMED IAW STEP 6(B) OF REO 690-57-51-541 REV. -.  NO INDICATIONS NOTED APPLIED CAD PLATE TO FABRICATED BUSHING IAW REO 690-57-51-541 REV-.  COMPLIED WITH STEPS 5, 7, 8 & 9 OF REO 690-57-51-541 REV -.  INSTALLED O/S AILERON BUSHING USING NITROGEN.  REAMED BUSHING. IAW REO 690-57-51-541.

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