Service difficulty report · Pushrod

Difficulty date
February 24, 2003
Submitted
February 24, 2003
Operation
General aviation
Engine
Cont IO520F
Engine time
3,587 hours
Part
Pushrod
Part number
538304P030
Condition
Worn
Location
Cylinder
Component
Cylinder · Cont
Component part number
653446A9
Stage of operation
IN
How discovered
V
Nature of condition
O
Precautionary procedure
K

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

What was found

UPON DISASSEMBLING THE ENGINE FOR OVERHAUL IT WAS DISCOVERED THAT THE NR 1 CYLINDER EXHAUST PUSHROD WAS SEVERLY WORN AT A POINT ABOUT 4 INCHES FROM THE ROCKER ARM END. THE WORN AREA WAS SMOOTH, CRESCENT SHAPED, ABOUT 1/2 INCH IN LENGTH, ALMOST PENETRATING THE ENTIRE WALL THICKNESS OF THE PUSHROD. INSPECTION OF THE PUSHROD HOUSING REVEALED A SMALL BUT SHARP DENT ABOUT 1/8 INCH DEEP CORRESPONDING TO AREA OF WEAR ON THE PUSHROD. IT WAS UNABLE TO DETERMINE HOW LONG THE DENT HAD BEEN THERE BUT IMMINENT FAILURE OF THE PUSHROD WAS VERY LIKELY.