What was found
GOUGES ARE ON THE 0.170 INCH DIAMETER OF THE SEGMENT. APPEARS TO BE CAUSED BY RUBBING ON SLEEVE OF YAW DAMPER LAP ASSEMBLY.
- Difficulty date
- November 4, 1998
- Submitted
- March 26, 2000
- Operation
- General aviation
- Filed by
- IU6R626N
Aero Controls, LLC - System (JASC)
- 5540 · Rudder Structure
- Part
- Cam Segment
- Part number
- 69356071
- Condition
- Gouged
- Location
- Rudder
- Component
- Boeing · 6935649
- Stage of operation
- IN
- Nature of condition
- O
- Precautionary procedure
- K
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.