What was found
(CAN) IN CRUISE, NR1 HYD SYSTEM WAS LOOSING FLUID UP TO 10% FOLLOWING TOUCH DOWN. R/H I/B FLIGHT SPOILER PCU WAS LEAKING BETWEEN TORQUE MOTOR AND VALVE BODY
- Difficulty date
- November 12, 1999
- Submitted
- January 19, 2001
- Operation
- General aviation
- Make and model
- Cndair CL6002B19
- System (JASC)
- 2760 · Drag Control System
- Part
- Pcu
- Part number
- 270007
- Condition
- Leaking
- Location
- Rt Spoiler
- Component
- Stabilizer Actua
- Stage of operation
- CR
- How discovered
- O
- Nature of condition
- J, K
- Precautionary procedure
- O
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.