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Aviation safety reports, made easier to study

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March 2, 2009 · Bell 206 L4 · N410RL

Galliano, LA

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
March 2, 2009
Injury Outcomes
No injuries (1 uninjured)
Location
Galliano, LA
Aircraft
Bell 206 L4
Tail Number
N410RL
Operator
Rotorcraft Leasing
Injuries
None
Aircraft Damage
Substantial
NTSB Number
CEN09LA198

The commercial pilot was starting the single-engine helicopter's engine when he heard a loud bang and vibration. He immediately shut down the engine and exited the helicopter. Examination of the helicopter revealed that the tail rotor driveshaft 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 tail rotor drive shaft cover. The mechanic moved on to 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 0.2-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.

NTSB Probable Cause

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.

Full Narrative

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.

Flight

Event TypeAccident
Event Time06:20 CST
Nearest AirportSouth Lafourche Leonard Miller (1nm)
Flight Plan FiledUnknown
Flight Plan ActivatedUnknown
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftBell 206 L4
Tail NumberN410RL
Aircraft CategoryHeli
DamageSubstantial
OperatorRotorcraft Leasing
Operating RulePart 91
Engine TypeTurboshaft
Engine DetailsRolls Royce · 260c30 · Turboshaft · 850
Seats7

People & Injuries

Injury SummaryNo injuries (1 uninjured)
Fatal0
Serious0
Minor0
Uninjured1
Total1
Crew 1Age 32 · Second Class · None

Conditions

ConditionsVMC
LightDaylight
Wind7 kt
Visibility10 sm
CeilingNone
Temperature / Dew Point30 C / 30 C
Altimeter0
Observation Time11:00
Weather SourceWFAC

Appendix: Source Data