What was found
COMRPESSION TEST REVEALED NR 1 CYLINDER 30/80, NR 5 CYLINDER 52/80, AND NR 6 CYLINDER 42/80. UPON APPLICATION OF LEAK DETECTOR LIQUID, CRACKS WERE FOUND IN ALL THREE CYLINDER HEADS.
- Difficulty date
- December 8, 1998
- Submitted
- March 26, 2000
- Operation
- General aviation
- Aircraft
- N761PS
- Make and model
- Cessna 210M
- Aircraft serial
- 21062415
- Engine
- Cont IO520L
- System (JASC)
- 8530 · Reciprocating Engine Cylinder Section
- Part
- Cylinder
- Part number
- TM639272E
- Condition
- Cracked
- Location
- Nr 1, 5, 6
- 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.