# SDR CA010112016

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: October 27, 2000
- Submitted: January 19, 2001
- Operation: General aviation
- Make and model: Dhav DHC8*
- Engine: Pwa PW120
- Propeller: Hamstd 14SF7
- System (JASC): [2761 · Drag Control Actuator](https://openairdocs.org/jasc/2761)
- Part: Actuator
- Part number: A44700007
- Condition: Cracked
- Location: Spoiler
- Part time: 22,017 hours, 29,820 cycles
- Component: Drag Control Act
- Stage of operation: IN
- How discovered: V
- Nature of condition: K
- Precautionary procedure: K
- FAA source: FAA Service Difficulty Reporting System (https://sdrs.faa.gov/)
- Page: https://openairdocs.org/sdr/CA010112016

## Discrepancy

(CAN) A REPORTED HYDRAULIC LEAK WAS FOUND TO BE CAUSED BY A CRACKED ROLL SPOILER BODY. UNIT REPLACED WITH NEW ACTUATOR AND AIRCRAFT RETURNED TO SERVICE.

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