What was found
(CAN) DURING INSPECTION WHILE BENDING THE TAB THAT SECURES THE ROCKER STUD NUT THE TAB CRACKED/BROKE.
- Difficulty date
- November 15, 1996
- Submitted
- March 26, 2000
- Operation
- General aviation
- Engine
- Cont IO360D
- System (JASC)
- 8530 · Reciprocating Engine Cylinder Section
- Part
- Lock Tab
- Part number
- SA501867
- Condition
- Cracked
- Location
- Rocker Stud Nut
- 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.