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.
According to Punch Newspaper 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.
In its conclusion in the preliminary report, which
was obtained by Punch 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.
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