# SDR CA020326009

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: March 26, 2002
- Submitted: April 26, 2002
- Operation: General aviation
- Make and model: Cndair CL2151A10
- System (JASC): [2750 · Trailing Edge Flap Control System](https://openairdocs.org/jasc/2750)
- Part: Arm
- Part number: 21515065
- Condition: Cracked
- Location: Mass Balance
- 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/CA020326009

## Discrepancy

(CAN) SMALL CRACK FOUND IN RADIUS OF THE BASE OF THE MASS BALANCE ARM.

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