What was found
ON PRELIMINARY FUNCTIONAL TEST, THE BODY WAS NOTED TO HAVE A PIN HOLE CRACK WITH 3,000 PSI APPLIED TO THE P1 PORT. THE CRACK IS ADJACENT TO THE C1 PORT.
- Difficulty date
- February 17, 1999
- Submitted
- March 26, 2000
- Operation
- General aviation
- Filed by
- IU6R626N
Aero Controls, LLC - System (JASC)
- 3252 · Shimmy Damper
- Part
- Valve
- Part number
- 59561015501
- Condition
- Cracked
- Location
- Shimmy Dampener
- Component
- Doug
- 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.