Service difficulty report · Support · Bell 206B3

Difficulty date
November 3, 2011
Submitted
September 14, 2015
Operation
General aviation
Make and model
Bell 206B3
Aircraft time
10,725 hours
Engine
Allsn 250C*
Part
Support
Condition
Cracked
Location
T/R Gearbox
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) DURING FIELD INSPECTION OF AFT TAIL ROTOR GEAR BOX SUPPORT, THE LT BOLT ATTACH HOLE THROUGH CASTING WAS FOUND TO BE CRACKED. DURING REPAIR OF DAMAGED PART, 3 RIVETS IN LOCAL AREA WERE FOUND TO BE SHEARED, AND SEVERED. AFTER ASSESSING THE DAMAGED AREA, IT WAS FOUND THAT THE SHEARED RIVETS WERE NOT DIRECTLY RELATED TO THE CRACKED BOLT HOLE IN CASTING. AT THIS TIME WE SUSPECT THE REASON AS TO WHY THE RIVETS WERE SHEARED/SEVERED IS DUE TO PRE-LOADING CONDITION DURING A PRIOR ASSY.

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