FTW87FA156

NTSB accident investigation · Aerospatiale AS-355-F1 · Venice, LA · July 4, 1987

Accident · FatalField investigationFinal report
Date
July 4, 1987, 14:45 local (19:45 UTC)
Place
Venice, LA
Injuries
1 fatal
Damage
Destroyed
Phase of flight
Enroute
Aircraft
N5796MAerospatiale AS-355-F1
Weather
Visual (VMC) · Day
Status
Completed · report May 16, 1989
Report
Approved by Office Director
FAA report
19870704032409A
Case key
22256

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

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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 - normal
Rotor system,rotor vibration absorber - not securedCause
Rotor system,rotor vibration absorber - looseCause
Maintenance,installation - improperCompany maintenance personnelCause
Maintenance,inspection - inadequateCompany maintenance personnelCause
Loss of control - in flightCruise - normal
Rotor system,rotor vibration absorber - separationCause
Aircraft control - not possible
In flight collision with terrain/waterDescent - uncontrolled
Terrain condition - water

Analysis

One of the mechanics who performed maintenance on the aircraft main rotor head stated that he was not sure that he installed the retaining bolts which secured the vibration absorber assembly to the aircraft. Metallurgical analysis of the assembly indicated that the retaining bolts were not installed at impact. Examination of the wreckage suggests that the vibration absorber assembly separated from the aircraft and contacted the main rotor system resulting in loss of aircraft control and subsequent contact with the terrain (water). Witnesses observed the helicopter come apart in flight after hearing a loud 'boom'.

Aircraft

Registration
N5796M
Reported as
Aerospatiale AS-355-F1
Category
Helicopter
Serial number
5162
Airframe hours
4,460
Engine
Allison 250-C20F, 420 horsepower, turbo shaft
Damage
Destroyed
Flight
Part 135
Operator
Petroleum Helicopters,Inc.
Registered owner
Petroleum Helicopters Inc.
Airworthiness certificate
Standard, Normal
Last inspection
AAIP · July 3, 1987 · 4 hours before
Departed
7R1 · Venice, LA
Destination
Gulf Of Mexico
Flight plan
Company VFR

Flight crew

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
40
Certificate
Commercial
Airplane ratings
Single-engine land
Instrument ratings
Helicopter
Medical
Class 2, Valid Medical--no waivers/lim.
Seat
Right
Toxicology
Performed
Flight hours
5,739 total · 543 in this make and model · 4,819 as pilot in command · 202 in the last 90 days · 9 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
180° at 12 knots
Visibility
10 statute miles
Lowest ceiling
1,700 ft broken
Temperature
91 °F, dew point 75 °F
Altimeter
30.00 inHg
Observed at
7R1, 17 nm away

FAA reports on this event · 1

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