# SDR CA130508008

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: May 5, 2013
- Submitted: September 14, 2015
- Operation: General aviation
- Make and model: Dhav DHC8102
- Aircraft time: 54,711 hours
- Engine: Pwa PW120A
- Propeller: Hamstd 14SF7
- System (JASC): [2797 · Flight Control System Wiring](https://openairdocs.org/jasc/2797)
- Part: Connector
- Condition: Failed
- Location: Te Flaps
- Stage of operation: CL
- How discovered: O
- Nature of condition: N
- Precautionary procedure: A
- FAA source: FAA Service Difficulty Reporting System (https://sdrs.faa.gov/)
- Page: https://openairdocs.org/sdr/CA130508008

## Discrepancy

(CAN) DURING CLIMB, FLIGHT CREW RECEIVED A, FLAP POWER, CAUTION MESSAGE AFTER SELECTING FLAP, FROM  5.  FLIGHT CREW TRIED TO MOVE THE FLAPS BACK TO 5 DEGREES WITH NO SUCCESS, FLAPS REMAINED AT 3. THE AIRCRAFT RETURNED AND LANDED WITHOUT FURTHER INCIDENT.  MAINTENANCE TRAVELED TO THE ACFT LOCATION, MOVED FLAPS TO 5 DEGREES AND INSPECTED THE FLAP PRIMARY/SECONDARY DRIVES SYSTEM.  THE ACFT WAS FERRIED TO A MAINTENANCE BASE WHERE ISOLATION SOLENOID VALVE ELECTRICAL CONNECTOR 2752-P3 WAS FOUND AT FAULT.  THE CONNECTOR WAS REPLACED AND THE SYS TESTED SERVICEABLE.

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