Aviation Crash Map

San Joaquin OH-58A+ N177SJ

10 August 2005 · Lancaster, California, United States · Fatal

Summary

On 10 August 2005 at about 13:00 local time, a San Joaquin OH-58A+ registered N177SJ was involved in an accident near Lancaster, California, United States. One person was on board and one died. The aircraft was substantially damaged. The NTSB has published a probable cause for this accident; it is quoted in full below.

The record

Date
at 13:00
Classification
Accident
Location
Lancaster, California, United States
Coordinates
34.7078, -118.0325
Aircraft
San Joaquin OH-58A+
Registration
N177SJ
Category
Helicopter
Engines
1
Operator
Not recorded
Operating rule
Part 137: Agricultural
Purpose of flight
Aerial Application
Phase of flight
Not recorded
Route
Lancaster → Lancaster
Aircraft damage
Substantial
Weather
VMC
Light
Dawn
NTSB number
LAX05FA264

People

1 person died.

On board Died Serious Minor Uninjured
1 1 0 0 0

Probable cause

The pinion to turbine shaft coupling failed in fatigue due to a misaligned turbine shaft, which resulted in a loss of engine power.

Quoted verbatim from the NTSB record. This site does not paraphrase or interpret it.

Read the full NTSB narrative

Following a loss of engine power, the helicopter impacted the ground during the application of chemicals to an agricultural field. Post accident examination of the engine showed that the power turbine to pinion gear coupling had fractured. Metallurgical examination of the affected components showed that the coupling failed in fatigue, which effectively separated the engine from the main rotor gearbox. The fatigue was the result of a misaligned power turbine outer shaft, where the axis of the turbine shaft was angled slightly relative to the coupling and pinion axes. The turbine section had been removed from another engine due to metal contamination. The turbine section was repaired and subsequently installed on the accident helicopter on August 11, 2004, where it operated for 770.3 hours prior to the accident. Weight and balance calculations showed that the helicopter was in excess of its certificated maximum gross weight by 174 pounds.

Quoted verbatim from the NTSB record.

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