Service difficulty report · Bearing · Bell 205A1

Difficulty date
July 13, 2008
Submitted
November 3, 2008
Operation
General aviation
Make and model
Bell 205A1
Aircraft time
21,477 hours
Engine
Lyc T5313B
Part
Bearing
Condition
Damaged
Location
M/R Mast
Part time
6,478 hours
Component
Mast
Component part number
204040366021F
Stage of operation
HO
How discovered
O
Nature of condition
J
Precautionary procedure
A

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

What was found

(CAN) DURING HELI-PORTABLE SEISMIC DRILLING OPS, UPON DESCENT WITH AN EXTERNAL LOAD, THE MASTER CAUTION WARNING INDICATION ILLUMINATED. THE PIC CHECKED THE CAUTION PANEL TO FIND A TRANSMISSION OIL PRESSURE CAUTION LIGHT ILLUMINATED AND THE TRANSMISSION OIL PRESSURE GAUGE INDICATING ZERO PRESSURE. THE PIC DISCONTINUED ANY FURTHER OPS AND PROCEEDED TO LAND NORMALLY IN AN ADJACENT CUT BLOCK. A POST-SHUTDOWN INSPECTION BY THE AME REVEALED AN ABUNDANCE OF ALUMINUM METAL SHAVINGS IN THE OIL SYSTEM AND OIL FILTER. FURTHER DISASSEMBLY AND INSPECTION OF THE OIL SUMP SCREEN AND SUBSEQUENT REMOVAL OF THE OIL PUMP INDICATED EVEN MORE METAL SHAVINGS BUT THE ORIGIN OF THE MATERIAL COULD NOT DETERMINED. DURING THE FIELD REMOVAL OF THE TRANSMISSION, IT WAS DISCOVERED THAT THE LOWER BEARING RACE RETAINING NUT ON THE MAST ASSEMBLY HAD BROKEN FREE OF IS TORQUE AND LOCKING DEVICE. THE NUT BACKED OFF ALL THE WAY TO THE LAST THREAD CARVING A 1 INCH DEEP GROOVE INTO THE TRANSMISSION SUMP CASE.

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