wreckage of the Helicopter |
The helicopter crash in the Oworonshoki
area of Lagos on August 12, 2015 was due to an uncontained engine
failure that lasted 12
seconds, the preliminary report from the Accident
Investigation Bureau has revealed.
The AIB specifically stated that field
examination suggested that the aircraft’s number two engine suffered an
uncontained failure, adding that the flight crew could not declare
emergency before the crash occurred.
It, however, stated that the crew were
certified and qualified to conduct the flight in accordance with
applicable Nigerian Civil Aviation Regulations, adding that the captain
and co-pilot had 1,077.45 and 570 hours flight time on the aircraft
type, respectively.
On August 12, the SikorskyS-76C+ chopper,
with registration 5N-BGD, a domestic chartered flight operated by
Bristow Helicopters Limited Nigeria, crashed into the lagoon at
Oworonshoki area of Lagos.
The
two flight crew members and four of the 10 passengers onboard lost
their lives. The helicopter was destroyed and there was no fire. The
flight departed from an offshore oil rig, SEDCO Express, and was heading
to the Murtala Muhammed Airport, Lagos.
The accident occurred when the helicopter was on the inbound flight of a round trip that originated from Lagos.
In its conclusion in the preliminary
report, which was obtained by our correspondent on Monday, the AIB said,
“The crew did not declare an emergency. According to FDR data, the
upset lasted for 12 seconds. There were 12 souls on board, including two
crew members at the time of the accident.
“There was no evidence of fire outbreak
before and after the crash. The life rafts on the helicopter were
observed deflated and floating in the lagoon but were not deployed. The
wreckage of the helicopter was confined in a small area around the crash
site in the lagoon.
“The surviving passengers reported that
the flight was normal until the helicopter suddenly spiraled, descended
and impacted the waters of the underlying lagoon. Field examination
suggested that No 2 engine suffered an uncontained failure.”
The AIB noted that the combined Solid State Voice/Flight Data Recorder only contained information of the flight data.
It said that the preliminary flight
recorder data indicated that at 1000ft and 120Kts, the helicopter
experienced sudden pitch up, and left roll with varying attitude of yaw,
roll and pitch for 12 seconds until it impacted the water at about
1531hrs.
The AIB stated that the main wreckage was
submerged in the lagoon, adding that the two raft inflation bottles
under the crew seats were still fully charged.
The bureau noted that the helicopter was
manufactured in 2003, with total airframe hours of 10,258:0913, and it
was maintained in accordance with approved maintenance schedules.
It added, “No records of any deferred
defects in the tech log. The control pushrod tube separated from control
rod end with the bearing and the Jamnut. The Jamnut was loose and was
not seating against the control rod. The flight departed from the SEDCO
Express Rig and was uneventful until about five minutes to landing.
“The flight preceding the accident
aircraft was without incident. There was good communication between the
helicopter and the tower before the accident.”
The rescue was promptly carried out by fishermen operating their boats around the crash site.”
The bureau, in the preliminary report,
outlined some interim safety actions undertaken by Sikorsky and the
Federal Aviation Administration of the United States.
It also recommended that the Nigerian
Civil Aviation Authority should immediately carry out appropriate
oversight action on all Sikorsky S-76 series helicopters flying in the
country.
This, according to the AIB, is to ensure
the implementation of the Emergency Airworthiness Directives and Alert
Service Bulletin issued by the FAA and Sikorsky Aircraft Corporation.
Source: Punch Newspaper.
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