# SDR CA000719018

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: May 25, 2000
- Submitted: July 24, 2000
- Operation: General aviation
- Make and model: Bnorm BN2A26
- Aircraft time: 18,458 hours
- Engine: Lyc O540E4C5
- System (JASC): [5541 · Rudder, Spar/Rib](https://openairdocs.org/jasc/5541)
- Part: Beam
- Part number: NB4513544
- Condition: Cracked
- Location: Rudder Beam
- Component: Rudder Beam, Bnorm
- Stage of operation: IN
- How discovered: V
- Nature of condition: O
- Precautionary procedure: O
- FAA source: FAA Service Difficulty Reporting System (https://sdrs.faa.gov/)
- Page: https://openairdocs.org/sdr/CA000719018

## Discrepancy

(CAN) FLUORESCENT LP EXAMINATION WAS CONDUCTED ON THE AIRCRAFT PILOT, COPILOT LT, RT RUDDER PEDAL TORQUE ARM RADIUS.  RESULTS:  COPILOT RUDDER SET REVEALED REJECTABLE CRACK INDICATIONS AS MARKED.  IN SERVICE BULLETIN (PRECAUTIONARY EXAMINATION) THERE WERE NO REJECTABLE INDICATION IN ACCORDANCE WITH CODE ON THE PILOT SET.

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