Service difficulty report · Cylinder · Beech 35C33

Difficulty date
December 8, 2008
Submitted
December 22, 2008
Operation
General aviation
Aircraft
N653P
Make and model
Beech 35C33
Aircraft serial
CD991
Engine
Cont IO470K
Propeller
Mcauly 2A36C23
Part
Cylinder
Part number
539491
Condition
Cracked
Location
Engine
Part time
295 hours
Stage of operation
IN
How discovered
V
Nature of condition
K
Precautionary procedure
K

As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.

What was found

ANNUAL INSP REVEALED A LARGE QUANITY OF VERY BLACK OIL RUNNING DOWN THE ENGINE MOUNT LEG AND AIRFRAME STRUCTURE. FURTHER INVESTIGATION FOUND THE LEAK TO ORIGINATE AT THE HEAD TO BARREL CONNECTIONS OF CYLINDERS NR 1, AND NR 3. COMPRESSION CHECK USING AN INPUT PRESSURE OF 80 PSI AND LEAK DETECTING SOLUTION SHOWED AIR TO BE LEAKING FROM THE CYLINDER HEAD TO BARREL CONNECTION. CYLINDERS WERE REMOVED AND INSPECTED BUT IT COULD NOT BE CONFIRMED IF CRACK EXISTED OR IF LEAK WAS THROUGH THE THREADS. THE LOW TIME ON NEW MFG CYLINDERS INDICATES THAT THE PROBLEM COULD BE IN THE MFG PROCESS. NOTE: ENGINE WAS REBUILT / ZERO TIMED USING NEW CYLINCERS ON 5/20/2001. (K)

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