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************************************************************
NTSB PRESS RELEASE ************************************************************ National
Transportation Safety Board Washington, DC
20594 FOR IMMEDIATE
RELEASE: November 24, 2010 SB-10-45 ************************************************************ NTSB CITES LACK
OF BIRD STRIKE RESISTANT WINDSHIELD REQUIREMENTS IN
FATAL CRASH OF HELICOPTER IN LOUISIANA ************************************************************ The National
Transportation Safety Board today released a final report on a
fatal crash involving a transport-category helicopter caused
by a bird strike. The Board said the lack of requirements
for bird strike-resistant windshields contributed to
the crash, and called on the FAA to develop such
requirements. On January 4,
2009, a dual-engine Sikorsky S-76C++ helicopter
(N748P), registered to and operated by PHI, Inc., crashed into
marshy terrain near Morgan City, Louisiana approximately 7
minutes after takeoff from Amelie, Louisiana, on a
charter flight to an oil rig in the Gulf of Mexico. Both
pilots and 6 of the 7 passengers were killed in the crash. The aircraft had
reached level cruise flight at 850 feet mean sea level
and 135 knots when the cockpit voice recorder recorded a loud
bang, followed by sounds consistent with rushing wind and
a power reduction on both engines. The aircraft crashed
several seconds later. Feathers and other bird debris were
collected from the canopy and windshield of the aircraft.
Laboratory analysis identified the remains as coming from a
female red-tailed hawk; the average weight of such a bird is
2.4 pounds. The investigation
revealed that the impact of the bird on the canopy just
above the windshield near the engine control quadrant likely
jarred the fire extinguisher T-handles out of their detents
and moved them aft, pushing both engine control levers
into or near the flight idle position, reducing fuel to
both engines. The pilots were probably disoriented from
the broken windshield and rushing air and were unable to
react in time to maintain control of the helicopter. The helicopter
was originally equipped with laminated glass windshields that complied
with European bird-strike resistance
standards. PHI replaced the windshields with lighter-weight,
aftermarket cast acrylic windshields that did not have any
bird-strike resistance standards. The NTSB
determined that the helicopter crashed because of the sudden loss
of power to both engines following the bird strike and the
subsequent disorientation of the crewmembers. Contributing to
the accident, the Board said, were the lack of FAA
regulations and guidance requiring helicopter windshields to be
resistant to bird strikes, the lack of protections that
would prevent the T-handles from inadvertently
dislodging out of their detents, and the lack of a master
warning light and audible system to alert the flight crew of a
low-rotor speed condition. Recommendations
were issued to the FAA dealing with, among other things, the
design of S-76C++ fire extinguisher T- handles and
engine control quadrants, and similar designs of other
helicopters, and of audible low-rotor alarm systems; certification
standards for helicopter windshields; and simultaneous
dual-engine power loss training for helicopter pilots. A copy of the
Board's report may be found on its website at http://ntsb.gov/ntsb/GenPDF.asp?id=CEN09MA117&rpt=fi. A copy of the recommendation
letter may be found at http://ntsb.gov/Recs/letters/2010/A-10-136-147.pdf. - 30 - NTSB Media
Contact: Ted Lopatkiewicz (202)
314-6100 lopatt@xxxxxxxx ************************************************************ This message is
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