FTW87FA203

NTSB accident investigation · Aerospatiale AS-355F-1 · Ship Shoal 214c · August 19, 1987

Accident · Serious injuriesField investigationFinal report
Date
August 19, 1987, 11:35 local (16:35 UTC)
Place
Ship Shoal 214c
Injuries
2 serious, 2 uninjured
Damage
Substantial damage
Phase of flight
Initial climb
Aircraft
N359EAerospatiale AS-355F-1
Weather
Visual (VMC) · Day
Status
Completed · report June 16, 1989
Report
Approved by Office Director
FAA report
19870819046869A
Case key
22270

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/malfunctionTakeoff - initial climb
Lubricating system,oil cooler - vibrationCause
Maintenance,balancing - not correctedCompany maintenance personnelFactor
Information unavailableManufacturerFactor
Rotor drive system,tail rotor drive shaft - vibrationCause
Rotor drive system,tail rotor drive shaft - fatigueCause
Rotor drive system,tail rotor drive shaft - separationCause
Loss of control - in flightTakeoff - initial climb
Emergency procedure - not possible
Acft/equip,inadequate control locationManufacturerFactor
Inadequate certification/approval,aircraftFaa(organization)Factor
DitchingLanding - flare/touchdown
Landing gear,float assembly - failure,partialFactor

Analysis

Acft experienced a tail rotor drive shaft failure during t/o from an offshore platform. Acft spun left and completed 6 to 7 revolutions prior to water contact as the single plt could not reach the throttles to reduce pwr to idle. Acft landed hard and the rt float deployed on touchdown while the left float did not and the acft rolled left. Occupants swam to rig from which t/o had been initiated. Investigation revealed that the forward shaft (no. 1 segment) had failed in the area of the aft splines near the main gearbox oil cooling fan connection. Failure was attributed to fatigue due to fretting caused by abnormal vibration levels induced by the oil cooling fan blades. Analysis indicated that fan blades would become contaminated with deposits of grease, oil, and soot causing vibration to increase from .6 ips to 4.0 ips. No previous requirement to clean the fan blades existed and the vibration would not have been detectable by the plt or pax.

Aircraft

Registration
N359E
Reported as
Aerospatiale AS-355F-1
Category
Helicopter
Serial number
5138
Airframe hours
3,102
Engine
Allison 250-C20F, 420 horsepower, turbo shaft
Damage
Substantial damage
Flight
Executive/Corporate · Part 91
Registered owner
Transcontinental Gas Pipeline
Airworthiness certificate
Standard, Normal
Last inspection
Continuous airworthiness · July 21, 1987 · 59 hours before
Destination
Ship Shoal 246, GM
Airport
Ship Shoal 214c

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
30
Certificates
Commercial, Airline transport
Airplane ratings
Single-engine land
Instrument ratings
Airplane, Helicopter
Medical
Class 2, Valid Medical--no waivers/lim.
Seat
Right
Flight hours
5,514 total · 2,810 in this make and model · 4,815 as pilot in command · 130 in the last 90 days · 3 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
325° at 5 knots
Visibility
5 statute miles
Lowest ceiling
None
Temperature
90 °F
Altimeter
30.00 inHg

FAA reports on this event · 1

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