N410RL

Substantial
None

BELL 206

Accident Details

Date
Monday, March 2, 2009
NTSB Number
CEN09LA198
Location
Galliano, LA
Event ID
20090310X83102
Coordinates
29.437778, -90.256668
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

The failure of the tail rotor driveshaft and coupling during engine start due to the mechanic's failure to properly reattach the tail rotor driveshaft and coupling during maintenance.

Aircraft Information

Registration
N410RL
Make
BELL
Engine Type
Turbo-shaft
Year Built
2005
Model / ICAO
206B06
Aircraft Type
Rotorcraft
No. of Engines
1

Registered Owner (Historical)

Name
TVPX AIRCRAFT SOLUTIONS INC TRUSTEE
Address
39 E EAGLE RIDGE DR STE 201
Status
Deregistered
City
NORTH SALT LAKE
State / Zip Code
UT 84054-2533
Country
United States

Analysis

On March 2, 2009, at 0720 central daylight time, a Bell 206L-3, N401RL, was damaged when the tail rotor drive shaft and coupling severed while the helicopter was sitting on the ramp with the engine running. The helicopter was operated by and registered to Rotorcraft Leasing Company, LLC, Broussard, Louisiana. The commercial pilot was not injured. Visual meteorological conditions prevailed and no flight plan was filed for the ferry flight conducted under 14 Code of Federal Regulations Part 91.

According to the operator, the pilot heard a loud bang and vibration shortly after starting the engine. He immediately shut down the engine, and exited the helicopter. Examination of the helicopter revealed that the tail rotor drive shaft and coupling had severed just forward of the gearbox, which resulted in substantial damage to the tail boom.

The helicopter had undergone recent maintenance to the tail rotor gearbox input seal which included the removal of the tail rotor drive shaft from the coupling. When the two components were reattached, the mechanic only hand tightened the bolts, figuring additional maintenance was still planned for the gearbox. He then installed the tailrotor drive shaft cover. The mechanic moved onto another project and did not make a logbook entry of the work that he had completed or that the bolts were only hand tightened. Another mechanic later performed additional maintenance to the gearbox, but the bolts were not checked since the maintenance manual did not require the removal of the tail rotor driveshaft cover. A .2-hour maintenance flight check was conducted and the helicopter was returned to service. The accident occurred on first engine start after it had been returned to service.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CEN09LA198