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NTSB Report

December 9, 1996 · Aerospatiale AS350B · N390MA

East Cameron 71

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
December 9, 1996
Injury Outcomes
No injuries (2 uninjured)
Location
East Cameron 71
Aircraft
Aerospatiale AS350B
Tail Number
N390MA
Injuries
None
Aircraft Damage
Substantial
NTSB Number
FTW97LA058

The pilot hovered the helicopter about 3 feet above the helipad of an offshore platform, and initiated a pedal turn to keep the tailrotor clear of the stairwell and to align the helicopter into the wind for the landing. During the turn, the tailrotor struck a guard on the operator bucket of a crane, and one tail rotor blade separated from the helicopter. The helicopter rotated (uncontrolled) through 90 degrees of heading change, as the pilot rolled off the throttle and performed an autorotation onto the platform helipad. Winds were from the south at 10 gusting 18 knots.

NTSB Probable Cause

failure of the pilot to maintain clearance from an object (crane/bucket). The gusty wind condition and proximity of the crane/bucket were related factors.

Full Narrative

On December 9, 1996, at 1458 central standard time, an Aerospatiale AS350B, N390MA, registered to and operated by Metro Aviation, Inc., under Title 14 CFR Part 135, struck a crane while hovering at an offshore platform at the East Cameron 71 in the Gulf of Mexico. The commercial pilot and the sole passenger were not injured and the helicopter sustained substantial damage. Visual meteorological conditions prevailed for the flight and a company VFR flight plan was filed. The flight originated from West Cameron 238, Gulf of Mexico, at 1442. During telephone interviews and on the Pilot/Operator Report, the pilot and company personnel reported the following information to the investigator-in-charge. The helicopter approached the platform at an airspeed of 120 knots on a 190 to 200 degree heading. Winds were from the south at 10 knots gusting to 18 knots. The pilot hovered the helicopter about 3 feet above the helipad and initiated a pedal turn to keep the tailrotor clear of the stairwell and to align the helicopter into the wind for the landing. During the turn, the tailrotor struck a guard on the operator bucket of the crane and one tail rotor blade separated from the helicopter. The helicopter rotated uncontrolled through 90 degrees of heading change as the pilot rolled off the throttle and performed an autorotation onto the platform's helipad. The helicopter was examined by the pilot and other company personnel. Company personnel reported damage to the tailrotor blades, gearbox, and at the gearbox to tailboom attachment points.

Flight

Event TypeAccident
Event Time20:58 UTC
Nearest Airport0nm
Runway0
Flight Plan FiledCvfr
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftAerospatiale AS350B
Tail NumberN390MA
Aircraft CategoryHeli
DamageSubstantial
Operating RulePart 135
Engines1
Engine TypeTurboshaft
Engine DetailsTurbomeca · ARRIEL 1B1 · Turboshaft · 641
Seats6

People & Injuries

Injury SummaryNo injuries (2 uninjured)
Fatal0
Serious0
Minor0
Uninjured2
Total2
Crew 1Age 41 · Second Class

Conditions

ConditionsVMC
LightDaylight
Wind135° @ 10 kt, gusting 18 kt
Visibility15 sm
CeilingNone
Temperature / Dew Point64 F / 0 C
Altimeter0
Weather SourcePILO

Appendix: Source Data