FTW83FA238

NTSB accident investigation · Aerospatiale AS-350D · Venice, LA · May 18, 1983

Accident · FatalField investigationFinal report
Date
May 18, 1983, 10:56 local (15:56 UTC)
Place
Venice, LA
Injuries
1 fatal
Damage
Destroyed
Phase of flight
Enroute
Aircraft
N36062Aerospatiale AS-350D
Weather
Visual (VMC) · Day
Status
Completed
Report
Approved by Office Director
FAA report
19830518019909A
Case key
20724

From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.

On this page

Sequence of events

NTSB’s coding before 2008: each occurrence and phase of flight, and the causes and factors under it. The codes are defined in NTSB’s coding manual.

Airframe/component/system failure/malfunctionCruise
Turboshaft engine,reduction gear box - fatigueCause
Inadequate quality controlManufacturerCause
Fuselage - vibration
Forced landingLanding
Autorotation - initiatedPilot in command
In flight collision with terrain/waterLanding
Rotor rpm - not maintainedPilot in command

Analysis

The acft crashed into a swamp with low rotor RPM after a failure of the accessory gearbox power output gear. The pilot radioed an emergency call saying he was experiencing severe vibrations and was landing. A few seconds later, he radioed that he was crashing. Rescue acft found the helicopter on its right side partially in water. There was evidence that thefailed gear box resulted in low rotor speed which was not recovered due to lack of altitude at the time of failure. An investigation revealed that the power turbine output (pto) gear, pn 4-081-044-15, failed from low stress, high cycle fatigue. The fatigue originated at a point were rehardening burns caused by grinding were present. This grinding was accomplished during manufacturing of the gear after it had been carburized. The procedure should have been accomplished prior to carburization when the material surface was much softer & less susceptible to grinding burns.

Aircraft

Registration
N36062
Reported as
Aerospatiale AS-350D
Category
Helicopter
Serial number
1237
Airframe hours
2,987
Engine
Lycoming LTS-101-600A2, turbo shaft
Damage
Destroyed
Flight
Ferry · Part 91
Registered owner
Petroleum Helicopters, Inc.
Airworthiness certificate
Standard, Normal
Departed
West Delta, GM
Destination
7R1 · Venice, LA
Flight plan
Company VFR

Matched to the registry by N-number and the event date; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

Flight crew

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
48
Certificate
Commercial
Airplane ratings
Single-engine land
Instrument ratings
Airplane
Medical
Class 2, Valid Medical--w/ waivers/lim
Seat
Right
Toxicology
Performed
Flight hours
6,340 total · 1,469 in this make and model · 4,649 as pilot in command · 130 in the last 90 days · 4 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
140° at 10 knots
Visibility
10 statute miles
Lowest ceiling
9,000 ft overcast
Temperature
79 °F, dew point 72 °F
Altimeter
30.00 inHg
Observed at
NEW

FAA reports on this event · 1

The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.