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NTSB Reports on July 15 Flight, Turbulence, Injury

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    NTSB Report Blames Clear Air Turbulence for United Airline Flight Injuries

    The National Transportation Safety Board (NTSB) has released the preliminary investigation report on the February 17 incident of United Airlines Flight 1676, flying from Denver-to-Billings, which suddenly started to jolt, injuring many passengers.

    According to the report, the airplane was in cruise flying mode at an altitude of 34,000 feet, when it ran into extreme clear air turbulence and resulted in several injuries. The report further elaborates that among 114 passengers and flight crew, 2 were seriously injured while 9 were hospitalized with minor injuries.

    The Boeing 737-700 was also damaged and was taken to United maintenance facility in Houston.

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    NTSB Sends Investigators to Paraguay

    February 4, 2013
    WASHINGTON – The National Transportation Safety Board is sending investigators to assist in the investigation of a Robinson R44 II helicopter that crashed about 80 miles north of Asuncion, Paraguay. Initial reports indicate that the pilot and two passengers were fatally injured.
    The investigation is being led by the Paraguay Civil Aviation Authority (CIPAA). The NTSB has designated senior investigator Paul Cox as the U. S. accredited representative to the CIPAA’s investigation and he will be accompanied by representatives from NTSB, the FAA, Robinson Helicopters, and Lycoming Engines. The U.S. team is expected to arrive Wednesday morning. Further information regarding the investigation will be released by the CIPAA.

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    Preliminary Report Issued in Piper Crash

    According to one report, the piper that crashed on Jan 12 near Paris Texas killed Passengers Michael Dale Bradley, 44, and Michael Endo, 51, and pilot Rob Thompson, 49. After takeoff, the plane lost its rudder and crashed in “foggy and drizzly” conditions between 8:54 and 9:00 a.m., a minute after talking to ATC in Fort Worth.

    Witnesses heard the engine backfire several times, and saw black smoke coming from the field where the plane crashed near Glory Texas.

    The horizontal stabilizer/rudder separated from the airframe and the report recorded that it was was found “approximately 30 feet behind the main wreckage.”

    The report was issued on Jan 22.

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    UK Participating in Sita Air Accident, Nepal

    What: Sita Air Dornier 228-202 en route from Kathmandu-Tribhuvan Airport to Lukla
    Where: 500 Meters from airport
    When: Sept 28, 2012
    Who: 19 fatalities
    Update: Because seven British subjects were killed aboard the Sita Air crash on September 28, the UK Air Accidents Investigation Branch will be joining the accident investigation.

    The British fatalities were named as:

    1. Raymond Eagle, 58, from Macclesfield, Cheshire
    2. Timothy Oakes, 57, from Winwick, near Warrington
    3. Stephen Holding, 60, from Stoke-on-Trent
    4. Vincent Kelly, 50, from Lostock, Bolton
    5. Darren Kelly (brother) 45 from Isle of Whithorn Southern Galloway
    6. Benjamin Ogden, 27, from London
    7. Christopher Davey, 51, from Northampton

    Nepalese authorities have a three month report deadline.

    EVEREST Plane Crash 19 Killed

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  • UPDATE ON BOEING 787 ENGINE FAILURE IN SOUTH CAROLINA


    August 8, 2012
    WASHINGTON – The National Transportation Safety Board continues its investigation of the July 28, 2012 contained engine failure that occurred on a Boeing 787 Dreamliner during a pre-delivery taxi test in Charleston, South Carolina. A contained engine failure is a specific engine design feature in which components might separate inside the engine but either remain within the engine’s cases or exit the engine through the tail pipe. This design feature generally does not pose immediate safety risks.

    Last week, the NTSB sent an investigator to the scene to gather information on the incident and subsequently launched a full investigation into the cause of the failure, led by NTSB Investigator-in-Charge, Mr. David Helson.

    On August 1, 2012, a team of experts from the NTSB, FAA, Boeing and GE Aviation specializing in engine systems and metallurgy traveled to a GE facility in Cincinnati, OH to disassemble and examine the failed GEnx engine. GE is the manufacturer of the GEnx engine. The parties to the investigation have been extremely cooperative in assisting NTSB personnel in its review and assessment.

    As a result of the investigative work to date, the NTSB has determined that a fan mid-shaft on the failed GEnx engine fractured at the forward end of the shaft, rear of the threads where the retaining nut is installed. The fan mid-shaft is undergoing several detailed examinations including dimensional and metallurgical inspections.

    The GEnx engine is a newly designed aircraft engine. It is a “dual shaft” engine, meaning that one shaft connects the compressor spool at one end to the high pressure turbine spool at the other end. A longer “fan shaft” connects the fan and booster in the front of the engine to the low pressure turbine in the back.

    The cockpit voice recorder and flight data recorder, which is a combined unit on the 787 Dreamliner, was transported to the agency’s Recorders Laboratory in Washington, DC for processing and readout. Both recordings captured the event and analysis is ongoing.

    Moving forward, investigators will continue the detailed examination of the engine and metallurgical analysis of its components. The investigators have also begun reviewing the engine manufacturing and assembly records.

    This investigation is ongoing. The information released today is factual in nature and does not include any analysis. Additional factual information may be released as it is developed.

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    NTSB Safety Recommendation A-12-7


    The National Transportation Safety Board makes the following recommendation to the Federal Aviation Administration:

    Require repetitive inspection of Engine Components, Inc. cylinder assemblies produced between May 2003 and October 2009 (serial numbers 7709 through 52884) installed on Teledyne Continental Motors model 520 and 550 engines and removal of these cylinder assemblies once they reach the engine manufacturer’s recommended normal time (hours) in service between overhauls. (A-12-7)

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