Service difficulty report · Shaft · Piper PA34200T

Difficulty date
January 30, 2005
Submitted
January 31, 2005
Operation
General aviation
Aircraft
N123AP
Make and model
Piper PA34200T
Aircraft serial
347770015
Engine
Cont TSIO360E
Part
Shaft
Part number
SA631991REVC
Condition
Out Of Round
Location
Engine
Stage of operation
NR
How discovered
9
Nature of condition
O
Precautionary procedure
O

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

What was found

UPON INSTALLING A SHAFT INTO A ROCKER WITH INADEQUATE TOLERANCE LIMITS, NOTED BINDING IN 3 O`CLOCK POSITIONS. WITH PRUSSION BLUE FOUND SHAFT IS FORMED IN ELIPTICAL OR, MODIFIED TRIANGULAR SHAPE WITH REDUCED WEAR SURFACE AREA DUE TO INCONSISTANT DIA OF SHAFT. ALL 24 NEW SHAFTS DISPLAYED SAME MACHINING RESULTS. HIGHEST PRESSURE POINT WAS NARROWEST CONTACT POINT. GALLING OF THESE SHAFTS APPEARS TO BE CONSISTANT WITH REDUCED WEAR SURFACE & CROWNING OF SHAFT. WHILE OTHER FACTORS MAY BE ATTRIBUTED TO CAUSE OF PREMATURE SHAFT FAILURE, REDUCTUION IN SURFACE AREA IS CONSISTANT WITH ACCELERATED DECOMPOSITION OF BEARING SURFACE. AIRWEST AIRCRAFT ENGINES SUPPLIED PARTS. RETURNED PARTS.

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