Service difficulty report · Helicoil · Cessna P210N

Difficulty date
June 27, 2000
Submitted
April 19, 2001
Operation
Air carrier
Aircraft
N6612W
Make and model
Cessna P210N
Aircraft serial
P21000805
Engine
Cont TSIO520AF
Part
Helicoil
Condition
Dislodged
Location
Nr 1 Cylinder
Component
Nr 1 Cylinder · Teledynecntl
Component part number
65496
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

PILOT REPORTED THAT AN ENGINE FAILURE OCCURRED DURING FLIGHT WITH UNEVENTFUL LANDING. PILOT INFORMED TECHS THT THE TOP SPARK PLUG HAD BECOME REMOVED FROM THE NR 1 CYLINDER. UPON ARRIVAL TO THE AIRCRAFT, FOUND TOP COWLINGS REMOVED AND THE NR 1 TOP SPARK PLUG LAYING ADJACENT TO THE CORRESPONDING CYLINDER, SPARK PLUG BOSS. THE NR 1, TOP SPARK PLUG BOSS HELICOIL WAS STILL INSTALLED IN THE CYLINDER. REPLACED THE EFFECTED HELICOIL WITH NEW AND SECURED HELICOIL IN PLACE, USING CARE NOT TO CONTAMINATE THE CYLINDER. NOTED THE CYLINDER BOSS THREADS HAD TO BE TAPPED OR CLEANED TO ACCEPT THE NEW HELICOIL. CYLINDER BOSS APPEARED TO NOT BE FULLY TAPPED AND BOSS THREADS MAY HAVE BEEN TAPERED.

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