Service difficulty report · Rod Cap · Beech 58

Difficulty date
April 5, 2001
Submitted
April 5, 2001
Operation
General aviation
Aircraft
N827TS
Make and model
Beech 58
Aircraft serial
TH836
Engine
Cont IO520C
Part
Rod Cap
Part number
646778
Condition
Failed
Location
Cylinder 2
Part time
2,206 hours
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

DURING CRUISE FLT RT ENG NR 2 CYL PISTON CONN ROD BROKE LOOSE FROM CRANKSHAFT, PENETRATED UPPER CRANKCASE. NR2 CYL SEP FROM ENGINE, RESTED IN COWLING. THE FORCE OF CONNECTING ROD COMING THROUGH THE CASE BROKE LEFT MAGNETO OFF ITS BASE AND PUNCHED A HOLE IN THE UPPER COWL. PILOT SECURED ENGINE AND FLEW TO A MAINTENANCE BASE. UPON REMOVING PIECES AND LAYING THEM OUT ON TABLE IT WAS NOTICED ONE OF THE CONNECTING ROD CAP BOLTS DID NOT HAVE THE REMAINS OF A COTTER PIN IN EITHER OF THE SAFETING HOLES. BOLT HEAD HAD BEEN BROKEN OFF(SUSPECTED FROM THE HAMMERING WHEN THE NUT WAS LOOSE). IT WAS ALSO NOTED THAT THREADS OF SAME BOLT, NOT AS DAMAGED AS BOLT ON OTHER SIDE , INDICATING IT UNSCREWED ITSELF.

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