Service difficulty report · Bolt · Bell 205A1

Difficulty date
May 22, 2008
Submitted
November 3, 2008
Operation
General aviation
Make and model
Bell 205A1
Aircraft time
16,602 hours
Engine
Lyc T5317BLYC
Part
Bolt
Part number
AN17420
Condition
Broken
Location
Stab Bar Damper
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

(CAN) WHILE PERFORMING ADI, AME DISCOVERED THAT A STAB BAR DAMPER TUBE ASSY P/N: 204-010-925-009 AND A DAMPER LEVER P/N: 212-010-301-001 WERE MISSING. IT APPEARS THAT THE TUBE ASSY UPPER BOLT P/N: AN174-20 BROKE OFF FIRST AND WAS THE CONTRIBUTING FACTOR OF THE DAMAGE. THE REMAINS OF SUBJECT BOLT (NUT WASHER AND SHANK WILL BE SENT FOR INVESTIGATION/ANALYSIS FOR POSSIBLE METAL FATIGUE AND/OR CORROSION. (REMAINS OF SUBJECT BOLT WERE STILL IN STAB BAR FRAME, INBOARD SIDE) STAB BAR DAMPER P/N: 204-010-937-009 WILL BE REPLACED AS A PRECAUTIONARY MEASURE AND SENT FOR INSVESTIGATION AS WELL FOR A POSSIBLE INTERNAL FAILURE/SEIZURE WHICH MIGHT HAVE CONTRIBUTED TO SUBJECT BOLT FAILURE. STAB BAR DAMPER TUBE RIGGING FOR POSSIBLE BOTTOMING HAS NOT BEEN EVALUATED AT THIS TIME BUT WILL BE C/O DURING REPAIRS. (TC NR 20080523002)

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