Service difficulty report · Shaft · Bell 206B

Difficulty date
June 21, 2007
Submitted
October 24, 2007
Operation
General aviation
Make and model
Bell 206B
Aircraft time
15,766 hours
Engine
Allsn 250C20
Part
Shaft
Part number
23037413
Condition
Cracked
Location
Engine
Part time
232 hours
Stage of operation
TX
How discovered
O
Nature of condition
K, B
Precautionary procedure
O

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

What was found

(CAN) POWER TURBINE ACTION DISMANTLED TO DETERMINE CAUSE OF OIL CONSUMPTION AND SMOKING. UPON TEARDOWN AND DETAIL INSPECTION IT WAS NOTED THAT THE PT OUTER SHAFT HAD A LARGE CRACK ORIGINATING AT ROOT OF 1 CURVIC COUPLINGS AND SPLITTING INTO 2 FURTHER DOWN SHAFT. CRACKING AND MATERIAL DAMAGE TO CURVIC RESULTED IN LOSS OF 1 OF CURVICS WHICH WAS NOT RECOVERED. FRETTING DAMAGE IS ALSO OBSERVED ON MATING CURVICS OF 3RD AND 4TH STAGE WHEELS. REPORTED OIL CONSUMPTION AND SMOKING ASSOCIATED WITH THIS TURBINE LIKELY RESULT OF OIL AND OIL MIST MOVING THROUGH TIGHT FIT OF PT INNER AND OUTER SHAFT. NORMAL TIGHT FIT BETWEEN THESE COMPONENTS WOULD HAVE BEEN AFFECTED BY CRACKING OF OUTER SHAFT RESULTING IN OIL FLOW ACROSS THIS AREA AND SUBSEQUENT LEAKAGE INTO TURBINE THROUGH CURVICS OR THE CRACK OF PT OUTER SHAFT ITSELF. HEAT TINTING SEEN ON THE NICKEL OF PT OUTER SHAFT IS LIKELY RESULT OF RESIDUE AND/OR HEAT FROM OIL BURNING AS IT LEAKED THROUGH CURVIC AREA.

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