Service difficulty report · Rod · Cessna 337

Difficulty date
August 13, 2007
Submitted
April 4, 2009
Operation
General aviation
Aircraft
N2167X
Make and model
Cessna 337
Aircraft serial
0067
Aircraft time
3,183 hours
Engine
Cont IO360CB
Engine time
634 hours, 30 cycles
Part
Rod
Condition
Obstructed
Location
Nr 4 Cylinder
Stage of operation
CR
How discovered
O
Nature of condition
Y, B, T
Precautionary procedure
E, B, A

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

What was found

TOTAL & SUDDEN ENGINE FAILURE DUE TO NR 4 CYLINDER CONNECTING ROD NUT COMING IN CONTACT WITH BOTTOM OF CYLINDER BARREL. BOTTOM OF BARREL EXTENTS 1 INCH .400 INTO CASE & THERE IS ONLY .010 -.020 INCH CLEARANCES BETWEEN BOTTOM OF CYLINDER BARREL & CONNECTING ROD NUT WHEN CYLINDER COMES UP TO TOP DEAD CENTER. CONNECTING ROD NUTS, ORIGINAL STYLE WERE CASTLE NUT WITH COTTER PIN. CLEARANCE WAS SO MINIMAL PIECES COTTER PIN BROKE OFF & FOUND IN ENGINE SCREENS. MFG CHANGED TO A 12 POINT CONNECTING ROD NUT WITH NO COTTER PIN WHICH OFFERS MORE CLEARANCE & SOLVED PROBLEM OF BROKEN COTTER PIN, BUT NEVER MADE MANDATORY. ENGINE BUILDERS STILL SELLING & INSTALLING CASTLE NUTS WITH COTTER PINS IN THESE ENGINES. THERE ARE STILL SERVICE INFORMATION LETTER SIL93-15 & CRITICAL SERVICE BULLETIN CSB96-13 ABOUT INSTALLING COTTER PIN. MFG PUBLISHED CRANKCASE HALF SERVICEABLE LIFE LIMIT FOR THIS ENGINE IS 4.554 INCH, & DECK TO DECK CASE WIDTH 9.108 INCH. CRANKCASE SERVICED MILLED THIS CASE TO SERVICE LIFE LIMITS BY REMOVING ONLY .003 INCH FROM ONE SIDE OF CASE & .005 FROM OTHER SIDE. WHEN FAILURE REPORTED HAVE APPROVAL TO REMOVE .025 OF AN INCH. THIS IS ANOTHER PROBLEM BECAUSE IF THAT AMOUNT WAS EVER MILL IT WOULD MEAN CERTAIN FAILURE OF THE ENGINE AND CASE PENETRATION. THERE IS NO WAY TO SEE THIS LACK OF CLEARANCE WHILE BUILDING UP THE ENGINE IN THE NORMAL STEPS AND PROCEDURES SPELLED OUT IN THE OVERHAUL MANUAL, BUT IF FOR INSPECTION PURPOSES ONE HALF OF THE CASE IS ASSEMBLED. WITH THE CRANKSHAFT BEARING, A CYLINDER, PISTON AND CONNECTION ROD YOU CAN SEE HOW CLOSE THESE PARTS COME TO EACH OTHER BY ROTATING THE CRANKSHAFT IN ONE SIDE OF THE CASE HALF. FIT TEST. A SIMPLE SOLUTION WOULD BE TO REMOVE .050 TO .100 INCH FROM THE BOTTOM OF EACH BARREL TO ALLOW ROOM FOR EXPANSION OF THESE CRITICAL ROTATING PARTS.

More about the Cessna 337