N390MA

Substantial
None

Aerospatiale AS350B S/N: 1549

Accident Details

Date
Monday, December 9, 1996
NTSB Number
FTW97LA058
Location
EAST CAMERON 71
Event ID
20001208X07157
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

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.

Aircraft Information

Registration
N390MA
Make
AEROSPATIALE
Serial Number
1549
Engine Type
Turbo-shaft
Year Built
2003
Model / ICAO
AS350B AS50
Aircraft Type
Rotorcraft
No. of Engines
1

Registered Owner (Historical)

Name
AVANTI AIRCORP INC
Address
3500 DUPONT HWY
Status
Deregistered
City
DOVER
State / Zip Code
DE 19901
Country
United States

Analysis

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.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# FTW97LA058