What was found
PIN HOLE LEAK IN HOUSING AT CYLINDER 1 PORT. FATIGUE, OVERTIGHTENING OF FITTING OR IMPACT COULD HAVE CAUSED CRACK. FITTING REMOVED FROM PORT SHOWS SIGNS OF A HARD IMPACT.
- Difficulty date
- January 25, 1999
- Submitted
- March 26, 2000
- Operation
- General aviation
- Filed by
- IU6R626N
Aero Controls, LLC - System (JASC)
- 3222 · Nose/Tail Landing Gear Strut/Axle
- Part
- Body
- Part number
- S6026
- Condition
- Leaking
- Location
- Strut
- Component
- Sargent · S60252
- 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.