SDR 95ZZZX2666

Service difficulty report · Cylinder

Difficulty date
February 16, 1995
Submitted
March 26, 2000
Operation
General aviation
Engine
Cont TSIO520BE
Part
Cylinder
Condition
Cracked
Location
Stud Hole
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.

What was found

ROCKER ARM RETAINING STUD HELICOIL IMPROPERLY INSTALLED AND THE CYLINDER WAS CRACKED OUT OF SAME HOLE.