NTSB INVESTIGATING TURBULENCE EVENT OVER MISSOURI

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    NTSB RELEASES PHOTOS OF AIRCRAFT ACCIDENT IN ALASKA

    The National Transportation Safety Board has released three
    photographs of the aircraft accident site near Aleknagik,
    Alaska that took the lives of 5 of the 9 persons aboard.

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    NTSB Holding Family Assistance Symposium

    NTSB Holding Family Assistance Symposium
    Panel discussions during the March 28-29 event will help the transportation industry, the media, and investigative agencies learn how families are helped after accidents around the world.

    The National Transportation Safety Board will hold a two-day conference March 28-29 for family members, transportation accident investigation agencies, transportation industry representatives, government agencies, and the media to discuss family assistance after transportation accidents in an international context. The event coincides with the 15th anniversary of the Aviation Disaster Family Assistance Act and the 10th anniversary of ICAO Circular 285 and will give those who attend the chance to learn firsthand from those involved worldwide in family assistance, according to NTSB.

    Day one features four panel discussions and will be webcast. Day two includes training by the NTSB Transportation Disaster Assistance staff, who will give an overview of the NTSB model for family assistance operations.

    The tentative agenda shows the panel discussions will be:

    Family Members: Perspectives from those affected by accidents, a discussion of their needs, and how those needs are met through family assistance programs.
    Transportation industry, vendors, and non-governmental organizations: Responsibilities of the industry, their vendors, and non-governmental organizations.

    Government transportation accident investigation agencies: How investigative agencies provide information about accident investigations and their role in family assistance.

    Media: How the media report on family members following accidents and how family assistance has affected such reporting.

    The event will take place at the NTSB Conference Center, 429 L’Enfant Plaza SW, Washington, DC 20594. Registration is free and is being conducted separately for each day. Visit this page to register and for links to transportation family assistance resources.

    Tentative Agenda

    Perspectives from Family Members, Industry, Government, and Media

    Welcome and Introductions: The Honorable Deborah A.P. Hersman
    Commemoration of the 15th Anniversary of the Aviation Disaster Family Assistance Act
    Four high-level panel discussions designed to share best practices and lessons learned in the provision of family assistance in transportation accidents internationally.
    Family Members: Perspectives from those impacted by accidents, a discussion of their needs, and ways in which those needs are met through family assistance programs.
    Transportation industry, vendors, and non-governmental organizations: Perspectives on the responsibilities of the industry, their vendors, and non-governmental organizations in providing assistance.
    Government transportation accident investigation agencies: How investigative agencies provide information about the accident investigation and their role in family assistance.
    Media: How the media reports on family members following accidents and how family assistance has impacted such reporting.
    March 29, 2011

    The NTSB Family Assistance Model: An Introduction

    NTSB family assistance legislation overview; information flow and timelines; family assistance operations; conducting effective family briefings; personal effects best practices; victim identification concerns; site visits, memorials, anniversaries.

    SEE AGENDA

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    NTSB Release: Maintenance Causes 2008 Crash

    FOR IMMEDIATE RELEASE
    April 6, 2010
    SB-10-10

    POOR MAINTENANCE STARTED ACCIDENT CHAIN THAT RESULTED IN HIGH-SPEED RUNWAY EXCURSION THAT KILLED FOUR IN 2008, NTSB DETERMINES

    Washington, DC – A chartered business jet crashed at a South Carolina airport 18 months ago because of the operator’s inadequate maintenance of the airplane’s tires and the decision by the captain to attempt a high-speed rejected takeoff, which went against standard operating procedures and training, the NTSB determined today.

    On September 19, 2008, at 11:53 p.m. EDT, a Bombardier Learjet Model 60 (N999LJ) operated by Global Exec Aviation and destined for Van Nuys, California, overran runway 11 during a rejected takeoff at Columbia Metropolitan Airport. After the airplane left the departure end of runway 11, it struck airport lights, crashed through a perimeter fence, crossed a roadway and came to rest on a berm. The captain, the first officer, and two passengers were killed; two other passengers were seriously injured.

    The investigation revealed that prior to the accident the aircraft was operated while the main landing gear tires were severely underinflated because of Global Exec Aviation’s inadequate maintenance. The underinflation compromised the integrity of the tires, which led to the failure of all four of the airplane’s main landing gear tires during the takeoff roll.

    Shortly after the first tire failed, which occurred about 1.5 seconds after the airplane passed the maximum speed at which the takeoff attempt could be safely aborted, the first officer indicated that the takeoff should be continued but the captain decided to reject the takeoff and deployed the airplane’s thrust reversers. Pilots are trained to avoid attempting to reject a takeoff at high-speed unless the pilot concludes that the airplane is unable to fly; the investigation found no evidence that the accident airplane was uncontrollable or unable to become airborne.

    The tire failure during the takeoff roll damaged a sensor, which caused the airplane’s thrust reversers to return to the stowed position. While the captain was trying to stop the airplane by commanding reverse thrust, forward thrust was being provided at near-takeoff power because the thrust reversers were stowed. The Safety Board determined that the inadvertent forward thrust contributed to the severity of the accident.

    The Safety Board also found that neither the Federal Aviation Administration nor Learjet adequately reviewed the Airplane’s design after a similar uncommanded forward thrust accident that occurred during landing in Alabama in 2001. While the modifications put into place after the Alabama accident provided additional protection against uncommanded forward thrust upon landing, no such protection was provided for a rejected takeoff.

    “This accident chain started with something as basic as inadequate tire inflation and ended in tragedy,” said NTSB Chairman Deborah A.P. Hersman. “This entirely avoidable crash should reinforce to everyone in the aviation community that there are no small maintenance items because every time a plane takes off, lives are on the line.”

    The safety recommendations that the NTSB made to the Federal Aviation Administration as a result of this investigation are: provide pilots and maintenance personnel with information on the hazards associated with tire underinflation, including the required intervals for tire pressure checks, and allow pilots to perform pressure checks in air taxi operations to ensure that tires remain safely inflated at all times; require tire pressure monitoring systems for all transport category airplanes; identify and correct deficiencies in both Learjet’s thrust reverser system safety analysis and the FAA’s design certification process to ensure that hazards encountered in all phases of flight are mitigated; require that simulator training for pilots who conduct turbojet operations include opportunities to practice responding to events other than engine failures near takeoff speeds; require that pilots who fly air taxi turbojet operations have a minimum level of pilot operating experience in an airplane type before acting as pilot-in- command in that type; and require that airplane tire testing criteria reflect the loads that may be imposed on tires both during normal operating conditions and after the loss of one tire.

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    NTSB Safety Recommendation A-10-119

    National Transportation Safety Board
    Washington, DC 20594
    August 6, 2010

    NTSB Safety Recommendation A-10-119 and -120
    and Reiteration of NTSB Safety Recommendation A-04-63

    The National Transportation Safety Board recommends that the European Aviation Safety Agency:

    Modify European Aviation Safety Agency Certification Specifications for Large Aeroplanes CS-25 to ensure safe handling qualities in the yaw axis throughout the flight envelope, including limits for rudder pedal sensitivity. (A-10-119)

    After the yaw axis certification standard recommended in Safety Recommendation A-10-119 has been established, review the designs of existing airplanes to determine if they meet the standard. For existing airplane designs that do not meet the standard, the European Aviation Safety Agency (EASA) should determine if the airplanes would be adequately protected from the adverse effects of a potential aircraft-pilot coupling (APC) after rudder inputs at all airspeeds. If adequate protection does not exist, EASA should require modifications, as necessary, to provide the airplanes with increased protection from the adverse effects of a potential APC after rudder inputs at high airspeeds. (A-10-
    120)

    In addition, the National Transportation Safety Board reiterates the following recommendation to the European Aviation Safety Agency:

    Review the options for modifying the Airbus A300-600 and the Airbus A310 to provide increased protection from potentially hazardous rudder pedal inputs at high airspeeds and, on the basis of this review, require modifications to the A300-600 and A310 to provide increased protection from potentially hazardous rudder pedal inputs at high airspeeds. (A-04-63

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  • NTSB Safety Recommendations

    The National Transportation Safety Board makes the following
    recommendations to the Federal Aviation Administration:
    Work with the military, manufacturers, and National
    Aeronautics and Space Administration to complete the
    development of a technology capable of informing pilots
    about the continuing operational status of an engine. (A-10-
    62)

    Once the development of the engine technology has been
    completed, as asked for in Safety Recommendation A-10-62,
    require the implementation of the technology on transport-
    category airplane engines equipped with full-authority
    digital engine controls. (A-10-63)

    Modify the 14 Code of Federal Regulations 33.76(c) small and
    medium flocking bird certification test standard to require
    that the test be conducted using the lowest expected fan
    speed, instead of 100-percent fan speed, for the minimum
    climb rate. (A-10-64)

    During the bird-ingestion rulemaking database (BRDB) working
    group’s reevaluation of the current engine bird-ingestion
    certification regulations, specifically reevaluate the 14
    Code of Federal Regulations (CFR) 33.76(d) large flocking
    bird certification test standards to determine whether they
    should 1) apply to engines with an inlet area of less than
    3,875 square inches and 2) include a requirement for engine
    core ingestion. If the BRDB working group’s reevaluation
    determines that such requirements are needed, incorporate
    them into 14 CFR 33.76(d) and require that newly
    certificated engines be designed and tested to these
    requirements. (A-10-65)

    Require manufacturers of turbine-powered aircraft to develop
    a checklist and procedure for a dual-engine failure
    occurring at a low altitude. (A-10-66)

    Once the development of the checklist and procedure for a
    dual-engine failure occurring at a low altitude has been
    completed, as asked for in Safety Recommendation A-10-66,
    require 14 Code of Federal Regulations Part 121, Part 135,
    and Part 91 Subpart K operators of turbine-powered aircraft
    to implement the checklist and procedure. (A-10-67)

    Develop and validate comprehensive guidelines for emergency
    and abnormal checklist design and development. The
    guidelines should consider the order of critical items in
    the checklist (for example, starting the auxiliary power
    unit), the use of opt outs or gates to minimize the risk of
    flight crewmembers becoming stuck in an inappropriate
    checklist or portion of a checklist, the length of the
    checklist, the level of detail in the checklist, the time
    needed to complete the checklist, and the mental workload of
    the flight crew. (A-10-68)

    Require 14 Code of Federal Regulations Part 121, Part 135,
    and Part 91 Subpart K operators to include a dual-engine
    failure scenario occurring at a low altitude in initial and
    recurrent ground and simulator training designed to improve
    pilots? critical-thinking, task-shedding, decision-making,
    and workload-management skills. (A-10-69)

    Require 14 Code of Federal Regulations Part 121, Part 135,
    and Part 91 Subpart K operators to provide training and
    guidance to pilots that inform them about the visual
    illusions that can occur when landing on water and that
    include approach and touchdown techniques to use during a
    ditching, with and without engine power. (A-10-70)

    Work with the aviation industry to determine whether
    recommended practices and procedures need to be developed
    for pilots regarding forced landings without power both on
    water and land. (A-10-71)

    Require applicants for aircraft certification to demonstrate
    that their ditching parameters can be attained without
    engine power by pilots without the use of exceptional skill
    or strength. (A-10-72)

    Require Airbus operators to amend the ditching portion of
    the Engine Dual Failure checklist and any other applicable
    checklists to include a step to select the ground proximity
    warning system and terrain alerts to OFF during the final
    descent. (A-10-73)

    Require Airbus operators to expand the angle-of-attack-
    protection envelope limitations ground-school training to
    inform pilots about alpha-protection mode features while in
    normal law that can affect the pitch response of the
    airplane. (A-10-74)

    Require all 14 Code of Federal Regulations Part 139-
    certificated airports to conduct wildlife hazard assessments
    (WHA) to proactively assess the likelihood of wildlife
    strikes, and, if the WHA indicates the need for a wildlife
    hazard management plan (WHMP), require the airport to
    implement a WHMP into its airport certification manual. (A-
    10-75)

    Work with the U.S. Department of Agriculture to develop and
    implement innovative technologies that can be installed on
    aircraft that would reduce the likelihood of a bird strike.
    (A-10-76)
    Require Airbus to redesign the frame 65 vertical beam on
    A318, A319, A320, and A321 series airplanes to lessen the
    likelihood that it will intrude into the cabin during a
    ditching or gear-up landing and Airbus operators to
    incorporate these changes on their airplanes. (A-10-77)

    Conduct research to determine the most beneficial passenger
    brace position in airplanes with nonbreakover seats
    installed. If the research deems it necessary, issue new
    guidance material on passenger brace positions. (A-10-78)

    Require, on all new and in-service transport-category
    airplanes, that cabin safety equipment be stowed in
    locations that ensure that life rafts and/or slide/rafts
    remain accessible and that sufficient capacity is available
    for all occupants after a ditching. (A-10-79)

    Require quick-release girts and handholds on all evacuation
    slides and ramp/slide combinations. (A-10-80)

    Require 14 Code of Federal Regulations Part 121, Part 135,
    and Part 91 Subpart K operators to provide information about
    life lines, if the airplane is equipped with them, to
    passengers to ensure that the life lines can be quickly and
    effectively retrieved and used. (A-10-81)

    Require that aircraft operated by 14 Code of Federal
    Regulations Part 121, Part 135, and Part 91 Subpart K
    operators be equipped with flotation seat cushions and life
    vests for each occupant on all flights, regardless of the
    route. (A-10-82)

    Require 14 Code of Federal Regulations Part 121, Part 135,
    and Part 91 Subpart K operators to brief passengers on all
    flotation equipment installed on an airplane, including a
    full demonstration of correct life vest retrieval and
    donning procedures, before all flights, regardless of route.
    (A-10-83)

    Require modifications to life vest stowage compartments or
    stowage compartment locations to improve the ability of
    passengers to retrieve life vests for all occupants. (A-10-
    84)

    Revise the life vest performance standards contained in
    Technical Standard Order-C13f to ensure that they result in
    a life vest that passengers can quickly and correctly don.
    (A-10-85)

    Conduct research on, and require 14 Code of Federal
    Regulations Part 121, Part 135, and Part 91 Subpart K
    operators to implement, creative and effective methods of
    overcoming passengers? inattention and providing them with
    safety information. (A-10-86)

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    NTSB ISSUES UPDATE ON JACKSON HOLE B-757 RUNWAY OVERRUN INCIDENT

    NTSB Advisory
    National Transportation Safety Board
    Washington, DC 20594
    December 31, 2010

    In its continuing investigation of the runway overrun of a jetliner in Jackson Hole, Wyo., the National Transportation Safety Board has developed the following factual information:

    At about 11:38 am MT on Wednesday, December 29, American Airlines flight 2253, a B-757-200 (N668AA) inbound from Chicago O’Hare International Airport, ran off the end of runway 19 in snowy conditions while landing at Jackson Hole Airport. No injuries were reported among the 181 passengers and crew on board.

    The aircraft came to rest in hard packed snow about 350 feet beyond the runway overrun area. An initial inspection did not reveal any structural damage to the aircraft. Shortly after the aircraft came to a stop, in accordance with American Airlines’ procedures, the pilots pulled the circuit breaker to the cockpit voice recorder (CVR) to preserve all of the recorded information for investigators.

    The CVR and DFDR (digital flight data recorder) arrived at the Safety Board’s recorder laboratory on Thursday evening, Dec. 30, where investigators were standing by to download the contents of both recorders. The CVR provided a two-hour recording of excellent quality audio; the voices of each of the pilots on the flight deck were clearly audible. The DFDR provided 1200 recorded parameters of flight data and captured the entire incident.

    The crew, who were interviewed on Thursday evening, indicated that they saw the runway prior to reaching the minimum descent altitude before touchdown. Both crewmembers characterized the flight and approach to landing as uneventful prior to the runway overrun. The first officer was the flying pilot.

    The accident docket, which will contain additional factual information, is expected to be opened in 60-90 days. It will be available on the docket section of the NTSB website at http://go.usa.gov/rjR

    PROTOCALS FOR TRANSPORTING AIRCRAFT RECORDERS IN INCIDENT INVESTIGATIONS

    The Safety Board has long-established protocols for the handling and transportation of CVRs and DFDRs that contain recorded information from a commercial aviation incident, which by definition is one where no serious injuries or substantial damage to the aircraft or other property has occurred.

    In such incident investigations, the Safety Board frequently asks the airline involved to transport the recorders on their own aircraft as such an arrangement often provides the most expeditious means of conveying the devices to Safety Board labs in Washington. The airline is instructed to transport the recorders without delay and without accessing the information contained within them by any means. This practice has worked efficiently and without complication for more than 40 years.

    During this incident investigation, the Safety Board learned that the recorders were flown to Tulsa, Okla., where American Airlines technicians downloaded information from the DFDR; the CVR was not accessed by American.

    “Although a thorough examination by our investigators determined that no information from the DFDR was missing or altered in any way, the breach of protocol by American Airlines personnel violates the Safety Board’s standards of conduct for any organization granted party status in an NTSB investigation,” said NTSB Chairman Deborah A.P. Hersman. “Because maintaining and enforcing strict investigative protocols and procedures is vital to the integrity of our investigative processes, we have revoked the party status of American Airlines and excused them from further participation in this incident investigation.”

    American Airlines has assured the Safety Board that a full review of proper procedures and internal controls would be undertaken to ensure that such an occurrence is not repeated.

    Despite their removal from party standing, the NTSB will provide American Airlines with any and all information needed to ensure a timely response to operational safety deficiencies identified in the course of the investigation.

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