What was found
COMPRESSION TEST REVEALED 58/80 FOR NR 2 CYLINDER. USED LEAK DETECTOR LIQUID TO DETECT CRACK ADJACENT TO EXHAUST PORT BETWEEN 16TH AND 17TH FIN. CRACK EXTENDS FROM EXHAUST VALVE TO SPARK PLUG HOLE.
- Difficulty date
- December 8, 1998
- Submitted
- March 26, 2000
- Operation
- General aviation
- Aircraft
- N6585A
- Make and model
- Cessna 210N
- Aircraft serial
- 21063554
- Engine
- Cont IO520L
- System (JASC)
- 8530 · Reciprocating Engine Cylinder Section
- Part
- Cylinder
- Part number
- CN635448EC
- Condition
- Cracked
- Location
- Engine
- 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.