What was found
BALL END OF CAM SEGMENT IS UNDERSIZED ON THE 0.311 INCH DIAMETER. POSSIBLE CAUSE: APPEARS TO BE CAUSED BY MOVEMENT INSIDE YAW DAMPER SLIDE. (X)
- Difficulty date
- March 10, 2000
- Submitted
- May 1, 2000
- Operation
- Air carrier
- Make and model
- Boeing 737*
- System (JASC)
- 2720 · Rudder Control System
- Part
- Cam
- Part number
- 69356071
- Condition
- Worn
- Location
- Yaw Damper
- Part time
- 35,591 hours
- Component
- Rudder Pcu · Boeing
- Component part number
- 65C370539
- Stage of operation
- IN
- How discovered
- V
- Nature of condition
- O
- Precautionary procedure
- K
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.