Service difficulty report · Bolt · Bolkms BO105LSA3

Difficulty date
April 13, 2006
Submitted
May 18, 2006
Operation
Air carrier
Aircraft
N202LF
Make and model
Bolkms BO105LSA3
Aircraft serial
2014
Engine
Allsn 250C28
Part
Bolt
Part number
LN90828X18
Condition
Sheared
Location
Intermediate Gb
Part time
3,988 hours
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

DURING COURSE OF AN ACCIDENT INVESTIGATION, IT WAS NOTED THAT BOLTS THAT CONNECT TAIL ROTOR DRIVE SHAFT TO INPUT THOMAS COUPLING OF INTERMEDIATE GEARBOX WERE SHEARED. SHEARING TOOK PLACE JUST BELOW GRIP LENGTH AREA OF BOLT . SHEARED BOLTS WERE STILL IN FLANGE OF GEAR BOX THOMAS COUPLING. THREADED PORTIONS OF BOLTS WERE RECOVERED WITH NUTS INSTALLED IN WRECKAGE ALONG WITH OTHER HARDWARE. IT WAS NOTED THAT THE BOLT HOLES IN FLANGE ON TAIL ROTOR DRIVE SHAFT WERE ELONGATED. THIS INDICATES AN UNDER TORQUE CONDITION WHICH IF GONE UNNOTICED COULD LIKELY LEAD TO THE SHEARING OF THE BOLTS. THIS RESULTS IN LOSS OF THE TAIL ROTOR CONTROL AND AN ACCIDENT. (K)