FTW89FA013

NTSB accident investigation · Aerospatiale AS-355F-1 · W. Cameron 617 · November 4, 1988

Accident · FatalField investigationFinal report
Date
November 4, 1988, 06:51 local (12:51 UTC)
Place
W. Cameron 617
Injuries
4 fatal, 2 serious
Damage
Destroyed
Phase of flight
Initial climb
Aircraft
N355EHAerospatiale AS-355F-1
Weather
Visual (VMC) · Day
Status
Completed · report June 25, 1990
Report
Approved by Office Director
Safety recommendations
Yes
FAA report
19881104049389A
Case key
22751

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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Probable cause

The loss of control of the aircraft which occurred when the tail rotor drive shaft experienced a fatigue induced material failure and tail rotor thrust was lost. Evidence indicated that the shaft was under designed for the loads that were encountered during normal operations.

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/malfunctionTakeoff - initial climb
Rotor drive system,tail rotor drive shaft - separationCause
Acft/equip,inadequate designManufacturerCause
Rotor drive system,tail rotor drive shaft - fatigueCause
Loss of control - in flightTakeoff - initial climb
In flight collision with terrain/waterDescent - uncontrolled

Analysis

Acft was departing an elevated helideck on an offshore production platform when it experienced a complete loss of tail rotor thrust and acft control due to a failure of the tail rotor drive shaft. The failure occurred as the plt initiated his takeoff with the acft having just cleared the deck and recovery was not possible. Investigation revealed that the drive shaft had failed as a result of fatigue cracking in an area of fretting where the shaft was bonded and bolted to its coupling. This and previous failures in the same area indicated that the shaft was under designed for the application and normal operating stresses. Shaft was subsequently re-designed and the fleet retrofitted.

Aircraft

Registration
N355EH
Reported as
Aerospatiale AS-355F-1
Category
Helicopter
Serial number
5137
Airframe hours
8,747
Engine
Allison 250-C20F, 425 horsepower, turbo shaft
Damage
Destroyed
Flight
Part 135
Registered owner
Era Helicopters
Airworthiness certificate
Standard, Normal; Standard, Utility
Last inspection
AAIP · November 3, 1988
Departed
NONE · W. Cameron 617, GM
Flight plan
Company VFR
Airport
WC61 · W. Cameron 617

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
43
Certificate
Airline transport
Instrument ratings
Helicopter
Medical
Class 1, Valid Medical--w/ waivers/lim
Seat
Right
Toxicology
Performed
Flight hours
8,819 total · 1,081 in this make and model · 8,162 as pilot in command · 270 in the last 90 days · 81 in the last 30 days · 6 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
180° at 25 knots, gusting 35
Visibility
10 statute miles
Lowest ceiling
1,500 ft broken
Altimeter
29.00 inHg
Observed at
C556, 15 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.