What was found
(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.
- 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
- 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
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.