Service difficulty report · Thru Bolt · Cessna U206F

Difficulty date
September 8, 2015
Submitted
September 14, 2015
Operation
Air carrier
Aircraft
N8419Q
Make and model
Cessna U206F
Aircraft serial
U20603279
Aircraft time
11,764 hours
Engine
Cont IO550F
Engine time
3,234 hours
Part
Thru Bolt
Part number
AEC641931981
Condition
Broken
Location
Engine
Part time
1,026 hours
Component
Engine · Cont · IO550F1B
Component part number
IO550F1B
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

WHILE PERFORMING A ROUTINE OIL & FILTER CHANGE, MECHANIC SAW LARGE AMOUNTS OF LEAKED OIL & A CRANKCASE THROUGH BOLT NUT IN THE COWLING. FURTHER INVESTIGATION REVEALED THAT THE LOWER FWD THROUGH BOLT HAD BROKEN AT THE NR 6 CYLINDER. UPON REMOVING THE REMAINS OF THE THROUGH BOLT, IT WAS FOUND TO BE QUITE RUSTED AT THE NR 6 CYLINDER END & RUST PITTING WAS OBSERVED WHERE THE CRACK HAD STARTED. THE UPPER THROUGH BOLT SHOWED NO SIGNS OF SIMILAR CORROSION. ACCORDING TO THE LOGBOOKS, BOTH THROUGH BOLTS HAD BEEN REPLACED WITH NEW PARTS AT THE LAST OVERHAUL 8 YEARS AGO. BOTH THROUGH BOLTS WERE REPLACED WITH NEW PARTS & THE ACFT WAS RETURNED TO SERVICE.

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