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Testimony: Icing

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    Wonder Not Why ATC Sleeps-It’s 2 a.m.

    There is a lot of buzz going on right now with so many air traffic controllers caught sleeping on the job. Everyone is lowering the boom on these individuals, and perhaps it is rightly so. And yet it seems to me that it is not a complete coincidence that suddenly in 2011, multiple air traffic controllers are caught sleeping on the job. Has this never happened before? Has no one ever noted it?

    This is in addition to an increase in controller errors. However, the increase in controller errors is (supposedly) a statistical glitch–not more errors actually but more reportage due to a new non-punative reporting system.

    It makes me wonder what has led to the circumstance of lone air traffic controllers manning all-night shifts. Has this been going on for decades? Or is this a recent development of economic cutbacks and our changing fuel economy, and our highly qualified personnel may be fighting to keep a position even on the swing shift, as job alternatives dwindle.

    Why is there an evening shift at all when the airlines have been combining flights and canceling flights, and rearranging flights and consolidating fights for economy’s sake? If the fact that an airport with minimal evening traffic chooses to have a lone overnight ATC shift, the act is practically a lagniappe. And if that is the case, then how sad it is that an act of extended service has turned to bite those offering the service.

    We do not put a lifeguard on the beach during the night when there are no swimmers, when swimming in dark waters is foolish. And yet, if we did place a lifeguard on that beach, we would not expect him to sleep. But would we expect him to stare out at the waters all night with no concession to human biorhythm? Is that not somewhat cruel? By the way, FAA’s rules forbid a controller from doing anything not directly related to air traffic control.

    When I hear the head of the FAA Air Traffic Organization Hank Krakowski has stepped down, it leads me to suspect that there is some scheduling pattern or policy that is directly attributable to him, something he did to disrupt the culture of air traffic control, that may be behind the significant coincidence of six (or more) sleeping ATControllers. I do not know if his stepping down is typical bureaucratic scapegoating, if he is doing the honorable thing because he’s in charge and the buck stops with him, or if he is truly responsible for some policy change that has led to the sleeping ATC.

    There are solutions, but they won’t be solutions today’s citizen of “instant everything” will like. There will be either the hiring more than just two controllers to turn night to day; or there will be (eventually) curtailing night flights and a loss of 24 hour conveniences.

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  • DOT: Airworthiness Directives; Airbus Model A330-300, A340-200, A340-300

    [Federal Register: March 26, 2009 (Volume 74, Number 57)]
    [Proposed Rules]
    [Page 13148-13152]
    From the Federal Register Online via GPO Access [wais.access.gpo.gov]
    [DOCID:fr26mr09-30]

    ———————————————————————–

    DEPARTMENT OF TRANSPORTATION

    Federal Aviation Administration

    14 CFR Part 39

    [Docket No. FAA-2009-0264; Directorate Identifier 2008-NM-174-AD]
    RIN 2120-AA64

    Airworthiness Directives; Airbus Model A330-300, A340-200, and
    A340-300 Series Airplanes

    AGENCY: Federal Aviation Administration (FAA), DOT.

    ACTION: Notice of proposed rulemaking (NPRM).

    ———————————————————————–

    SUMMARY: We propose to adopt a new airworthiness directive (AD) for the
    products listed above. This proposed AD results from mandatory
    continuing airworthiness information (MCAI)

    [[Page 13149]]

    originated by an aviation authority of another country to identify and
    correct an unsafe condition on an aviation product. The MCAI describes
    the unsafe condition as:

    One Long Range operator experienced a failure of one spoiler
    servo-control, associated with surface deflection in flight and
    hydraulic leak. On ground, this servo-control Part Number (P/N)
    MZ4306000-02X was found with the maintenance cover broken.
    Investigations showed that the rupture of the maintenance cover was
    due to pressure pulse fatigue.
    * * * The rupture of the maintenance cover in flight may result
    in the deflection of the associated spoiler surface up to the null-
    hinge position (loss of the hydraulic locking). It may also result
    in the loss of the associated hydraulic system (external leakage).
    In the worst case, the three hydraulic systems may be affected,
    which constitutes an unsafe condition.

    * * * * *
    Loss of the three hydraulic systems could result in reduced
    controllability of the airplane. The proposed AD would require actions
    that are intended to address the unsafe condition described in the
    MCAI.

    DATES: We must receive comments on this proposed AD by April 27, 2009.

    ADDRESSES: You may send comments by any of the following methods:
    Federal eRulemaking Portal: Go to http://
    www.regulations.gov. Follow the instructions for submitting comments.
    Fax: (202) 493-2251.
    Mail: U.S. Department of Transportation, Docket
    Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New
    Jersey Avenue, SE., Washington, DC 20590.
    Hand Delivery: U.S. Department of Transportation, Docket
    Operations, M-30, West Building Ground Floor, Room W12-40, 1200 New
    Jersey Avenue, SE., Washington, DC, between 9 a.m. and 5 p.m., Monday
    through Friday, except Federal holidays.
    For service information identified in this proposed AD, contact
    Airbus SAS–Airworthiness Office–EAL, 1 Rond Point Maurice Bellonte,
    31707 Blagnac Cedex, France; telephone +33 5 61 93 36 96; fax +33 5 61
    93 45 80, e-mail airworthiness.A330-A340@airbus.com; Internet http://
    www.airbus.com. You may review copies of the referenced service
    information at the FAA, Transport Airplane Directorate, 1601 Lind
    Avenue, SW., Renton, Washington. For information on the availability of
    this material at the FAA, call 425-227-1221 or 425-227-1152.

    Examining the AD Docket

    You may examine the AD docket on the Internet at http://
    www.regulations.gov; or in person at the Docket Operations office
    between 9 a.m. and 5 p.m., Monday through Friday, except Federal
    holidays. The AD docket contains this proposed AD, the regulatory
    evaluation, any comments received, and other information. The street
    address for the Docket Operations office (telephone (800) 647-5527) is
    in the ADDRESSES section. Comments will be available in the AD docket
    shortly after receipt.

    FOR FURTHER INFORMATION CONTACT: Vladimir Ulyanov, Aerospace Engineer,
    International Branch, ANM-116, Transport Airplane Directorate, FAA,
    1601 Lind Avenue, SW., Renton, Washington 98057-3356; telephone (425)
    227-1138; fax (425) 227-1149.

    SUPPLEMENTARY INFORMATION:

    Comments Invited

    We invite you to send any written relevant data, views, or
    arguments about this proposed AD. Send your comments to an address
    listed under the ADDRESSES section. Include “Docket No. FAA-2009-0264;
    Directorate Identifier 2008-NM-174-AD” at the beginning of your
    comments. We specifically invite comments on the overall regulatory,
    economic, environmental, and energy aspects of this proposed AD. We
    will consider all comments received by the closing date and may amend
    this proposed AD based on those comments.
    We will post all comments we receive, without change, to http://
    www.regulations.gov, including any personal information you provide. We
    will also post a report summarizing each substantive verbal contact we
    receive about this proposed AD.

    Discussion

    The European Aviation Safety Agency (EASA), which is the Technical
    Agent for the Member States of the European Community, has issued EASA
    Airworthiness Directive 2008-0160, dated August 22, 2008 (referred to
    after this as “the MCAI”), to correct an unsafe condition for the
    specified products. The MCAI states:

    One Long Range operator experienced a failure of one spoiler
    servo-control, associated with surface deflection in flight and
    hydraulic leak. On ground, this servo-control Part Number (P/N)
    MZ4306000-02X was found with the maintenance cover broken.
    Investigations showed that the rupture of the maintenance cover was
    due to pressure pulse fatigue.
    The maintenance cover allows switching the servo-control from
    “Operational” to “Maintenance” modes. The same cover is
    installed on all standard MZ spoiler servo-controls except on P/N
    MZ4339390-12 and MZ4306000-12, which have a reinforced maintenance
    cover. The rupture of the maintenance cover in flight may result in
    the deflection of the associated spoiler surface up to the null-
    hinge position (loss of the hydraulic locking). It may also result
    in the loss of the associated hydraulic system (external leakage).
    In the worst case, the three hydraulic systems may be affected,
    which constitutes an unsafe condition.
    For the reasons described above, this EASA AD requires the
    identification and the modification of all standard MZ spoiler
    servo-controls with initial maintenance cover (P/N MZ4339390-01X, –
    02X, -10X for position 1 and P/N MZ4306000-01X, 02X, -10X for
    positions 2 to 6) into standard MZ servo-controls with reinforced
    maintenance cover (P/N MZ4339390-12 for position 1 and P/N
    MZ4306000-12 for positions 2 to 6).

    Loss of the three hydraulic systems could result in reduced
    controllability of the airplane. You may obtain further information by
    examining the MCAI in the AD docket.

    Relevant Service Information

    Airbus has issued the service information described in the
    following table. The actions described in this service information are
    intended to correct the unsafe condition identified in the MCAI.

    Service Information
    ————————————————————————
    Service Bulletin Revision level Date
    ————————————————————————
    Airbus Mandatory Service 01……………. July 25, 2008.
    Bulletin A330-27A3154.
    Airbus Service Bulletin A330-27- 02……………. March 2, 2007.
    3110.
    Airbus Mandatory Service 01……………. July 25, 2008.
    Bulletin A340-27A4154.
    Airbus Service Bulletin A340-27- 01……………. March 2, 2007.
    4115.
    ————————————————————————

    [[Page 13150]]

    FAA’s Determination and Requirements of This Proposed AD

    This product has been approved by the aviation authority of another
    country, and is approved for operation in the United States. Pursuant
    to our bilateral agreement with the State of Design Authority, we have
    been notified of the unsafe condition described in the MCAI and service
    information referenced above. We are proposing this AD because we
    evaluated all pertinent information and determined an unsafe condition
    exists and is likely to exist or develop on other products of the same
    type design.

    Differences Between This AD and the MCAI or Service Information

    We have reviewed the MCAI and related service information and, in
    general, agree with their substance. But we might have found it
    necessary to use different words from those in the MCAI to ensure the
    AD is clear for U.S. operators and is enforceable. In making these
    changes, we do not intend to differ substantively from the information
    provided in the MCAI and related service information.
    We might also have proposed different actions in this AD from those
    in the MCAI in order to follow FAA policies. Any such differences are
    highlighted in a NOTE within the proposed AD.

    Costs of Compliance

    Based on the service information, we estimate that this proposed AD
    would affect 16 products of U.S. registry. We also estimate that it
    would take between 1 work-hour per product to comply with the basic
    requirements of this proposed AD. The average labor rate is $80 per
    work-hour. Based on these figures, we estimate the cost of the proposed
    AD on U.S. operators to be $1,280, or $80 per product.

    Authority for This Rulemaking

    Title 49 of the United States Code specifies the FAA’s authority to
    issue rules on aviation safety. Subtitle I, section 106, describes the
    authority of the FAA Administrator. “Subtitle VII: Aviation
    Programs,” describes in more detail the scope of the Agency’s
    authority.
    We are issuing this rulemaking under the authority described in
    “Subtitle VII, Part A, Subpart III, Section 44701: General
    requirements.” Under that section, Congress charges the FAA with
    promoting safe flight of civil aircraft in air commerce by prescribing
    regulations for practices, methods, and procedures the Administrator
    finds necessary for safety in air commerce. This regulation is within
    the scope of that authority because it addresses an unsafe condition
    that is likely to exist or develop on products identified in this
    rulemaking action.

    Regulatory Findings

    We determined that this proposed AD would not have federalism
    implications under Executive Order 13132. This proposed AD would not
    have a substantial direct effect on the States, on the relationship
    between the national Government and the States, or on the distribution
    of power and responsibilities among the various levels of government.
    For the reasons discussed above, I certify this proposed
    regulation:
    1. Is not a “significant regulatory action” under Executive Order
    12866;
    2. Is not a “significant rule” under the DOT Regulatory Policies
    and Procedures (44 FR 11034, February 26, 1979); and
    3. Will not have a significant economic impact, positive or
    negative, on a substantial number of small entities under the criteria
    of the Regulatory Flexibility Act.
    We prepared a regulatory evaluation of the estimated costs to
    comply with this proposed AD and placed it in the AD docket.

    List of Subjects in 14 CFR Part 39

    Air transportation, Aircraft, Aviation safety, Incorporation by
    reference, Safety.

    The Proposed Amendment

    Accordingly, under the authority delegated to me by the
    Administrator, the FAA proposes to amend 14 CFR part 39 as follows:

    PART 39–AIRWORTHINESS DIRECTIVES

    1. The authority citation for part 39 continues to read as follows:

    Authority: 49 U.S.C. 106(g), 40113, 44701.

    Sec. 39.13 [Amended]

    2. The FAA amends Sec. 39.13 by adding the following new AD:

    Airbus: Docket No. FAA-2009-0264; Directorate Identifier 2008-NM-
    174-AD.

    Comments Due Date

    (a) We must receive comments by April 27, 2009.

    Affected ADs

    (b) None.

    Applicability

    (c) This AD applies to Airbus Model A330-300, A340-200, and
    A340-300 series airplanes; certificated in any category, except
    those identified in paragraph (c)(1) and (c)(2) of this AD.
    (1) Airbus Model A330-301, -302, -303, -321, -322, -323, -341, –
    342, and -343 airplanes, manufacturer serial numbers (MSNs) up to
    and including MSN 588, except those on which Airbus Service Bulletin
    A330-27-3110 has been embodied in service.
    (2) Airbus Model A340-211, -212, -213, -311, -312, and -313
    airplanes, MSNs up to and including MSN 598, except those on which
    Airbus Service Bulletin A340-27-4115 has been embodied in service.

    Subject

    (d) Air Transport Association (ATA) of America Code 27: Flight
    controls.

    Reason

    (e) The mandatory continuing airworthiness information (MCAI)
    states:
    One Long Range operator experienced a failure of one spoiler
    servo-control, associated with surface deflection in flight and
    hydraulic leak. On ground, this servo-control Part Number (P/N)
    MZ4306000-02X was found with the maintenance cover broken.
    Investigations showed that the rupture of the maintenance cover was
    due to pressure pulse fatigue.
    The maintenance cover allows switching the servo-control from
    “Operational” to “Maintenance” modes. The same cover is
    installed on all standard MZ spoiler servo-controls except on P/N
    MZ4339390-12 and MZ4306000-12, which have a reinforced maintenance
    cover. The rupture of the maintenance cover in flight may result in
    the deflection of the associated spoiler surface up to the null-
    hinge position (loss of the hydraulic locking). It may also result
    in the loss of the associated hydraulic system (external leakage).
    In the worst case, the three hydraulic systems may be affected,
    which constitutes an unsafe condition.
    For the reasons described above, this EASA AD requires the
    identification and the modification of all standard MZ spoiler
    servo-controls with initial maintenance cover (P/N MZ4339390-01X, –
    02X, -10X for position 1 and P/N MZ4306000-01X, 02X, -10X for
    positions 2 to 6) into standard MZ servo-controls with reinforced
    maintenance cover (P/N MZ4339390-12 for position 1 and P/N
    MZ4306000-12 for positions 2 to 6).
    Loss of the three hydraulic systems could result in reduced
    controllability of the airplane.

    Actions and Compliance

    (f) Unless already done, do the following actions.
    (1) For airplanes that have accumulated more than 8,500 total
    flight cycles since first flight as of the effective date of this
    AD: Do the actions required by paragraphs (f)(1)(i) and (f)(1)(ii)
    of this AD, as applicable.
    (i) Within 3 months after the effective date of this AD:
    Identify the part number of spoiler servo-controls installed on the
    airplane at all positions in order to determine the number of
    affected hydraulic circuits in accordance with the Accomplishment
    Instructions of Airbus Mandatory Service Bulletin A330-27A3154,
    Revision 01; or Airbus Mandatory Service Bulletin A340-27A4154,
    Revision 01; both dated July 25, 2008, as applicable. If there is no
    spoiler servo-control installed with a part number

    [[Page 13151]]

    identified in Table 1 of this AD, no further action is required by
    this paragraph.
    (ii) If there is any spoiler servo-control installed with a part
    number identified in Table 1 of this AD, do all applicable actions
    required by paragraph (f)(2), (f)(3), or (f)(4) of this AD.

    Table 1–Spoiler Servo-Control Part Numbers
    ————————————————————————
    Position 1 Positions 2 through 6
    ————————————————————————
    MZ4339390-01X……………………….. MZ4306000-01X.
    MZ4339390-02X……………………….. MZ4306000-02X.
    MZ4339390-10X……………………….. MZ4306000-10X.
    ————————————————————————

    (2) If three affected hydraulic circuits are identified during
    the inspection required by paragraph (f)(1) of this AD, do the
    actions required by paragraphs (f)(2)(i), (f)(2)(ii), and
    (f)(2)(iii) of this AD, at the time specified.
    (i) Before the accumulation of 10,400 total flight cycles since
    first flight, or within 3 months after accomplishing the
    requirements of paragraph (f)(1)(i) of this AD, whichever occurs
    later: Modify the affected spoiler servo-controls on one hydraulic
    circuit in accordance with the Accomplishment Instructions of Airbus
    Service Bulletin A330-27-3110, Revision 02; or Airbus Service
    Bulletin A340-27-4115, Revision 01; both dated March 2, 2007, as
    applicable.
    (ii) Before the accumulation of 10,800 total flight cycles since
    first flight, or within 6 months after accomplishing the
    requirements in paragraph (f)(1)(i) of this AD, whichever occurs
    later: Modify the affected spoiler servo-controls on the second
    hydraulic circuit in accordance with the Accomplishment Instructions
    of Airbus Service Bulletin A330-27-3110, Revision 02; or Airbus
    Service Bulletin A340-27-4115, Revision 01; both dated March 2,
    2007, as applicable.
    (iii) Within 18 months after the effective date of this AD:
    Modify the remaining affected spoiler servo-controls in accordance
    with the Accomplishment Instructions of Airbus Service Bulletin
    A330-27-3110, Revision 02; or Airbus Service Bulletin A340-27-4115,
    Revision 01; both dated March 2, 2007, as applicable.
    (3) If two affected hydraulic circuits are identified during the
    inspection required by paragraph (f)(1) of this AD, do the actions
    required by paragraphs (f)(3)(i) and (f)(3)(ii) of this AD, at the
    time specified:
    (i) Before the accumulation of 10,800 total flight cycles since
    first flight, or within 6 months after accomplishing the
    requirements in paragraph (f)(1)(i) of this AD, whichever occurs
    later: Modify the affected spoiler servo-controls on one hydraulic
    circuit in accordance with the Accomplishment Instructions of Airbus
    Service Bulletin A330-27-3110, Revision 02; or Airbus Service
    Bulletin A340-27-4115, Revision 01; both dated March 2, 2007, as
    applicable.
    (ii) Within 18 months after the effective date of this AD:
    Modify the remaining affected spoiler servo-controls in accordance
    with the Accomplishment Instructions of Airbus Service Bulletin
    A330-27-3110, Revision 02; or Airbus Service Bulletin A340-27-4115,
    Revision 01; both dated March 2, 2007, as applicable.
    (4) If one affected hydraulic circuit is identified during the
    inspection required by paragraph (f)(1) of this AD: Within 18 months
    after the effective date of this AD, modify the affected spoiler
    servo-controls in accordance with the Accomplishment Instructions of
    Airbus Service Bulletin A330-27-3110, Revision 02; or Airbus Service
    Bulletin A340-27-4115, Revision 01; both dated March 2, 2007, as
    applicable.
    (5) For airplanes that have accumulated less than or equal to
    8,500 total flight cycles since first flight as of the effective
    date of this AD: Do the actions required by paragraphs (f)(5)(i) and
    (f)(5)(ii) of this AD, as applicable.
    (i) Within 9 months after the effective date of this AD: Do the
    actions specified in paragraph (f)(1)(i) of this AD. If there is no
    spoiler servo-control installed with a part number identified in
    Table 1 of this AD, no further action is required by this paragraph.
    (ii) If there is any spoiler servo-control installed with a part
    number identified in Table 1 of this AD: Within 18 months after the
    effective date of this AD, modify all the affected spoiler servo-
    controls in accordance with the Accomplishment Instructions of
    Airbus Service Bulletin A330-27-3110, Revision 02; or Airbus Service
    Bulletin A340-27-4115, Revision 01; both dated March 2, 2007, as
    applicable.
    (6) As of the effective date of this AD, no person may install
    any spoiler servo-control with a part number identified in Table 1
    of this AD on any aircraft as a replacement part, unless the part
    has been modified in accordance with the Accomplishment Instructions
    of Airbus Service Bulletin A330-27-3110, Revision 02; or Airbus
    Service Bulletin A340-27-4115, Revision 01; both dated March 2,
    2007, as applicable.
    (7) Actions accomplished before the effective date of this AD in
    accordance with the service bulletins specified in Table 2 of this
    AD are considered acceptable for compliance with the corresponding
    requirements of this AD.

    Table 2–Credit Service Information
    ————————————————————————
    Service Bulletin Revision level Date
    ————————————————————————
    Airbus Service Bulletin A330-27- Original………. November 28, 2003.
    3110.
    Airbus Service Bulletin A330-27- 01……………. March 26, 2004.
    3110.
    Airbus Service Bulletin A340-27- Original………. November 28, 2003.
    4115.
    ————————————————————————

    FAA AD Differences

    Note 1: This AD differs from the MCAI and/or service information
    as follows: No differences.

    Other FAA AD Provisions

    (g) The following provisions also apply to this AD:
    (1) Alternative Methods of Compliance (AMOCs): The Manager,
    International Branch, ANM-116, Transport Airplane Directorate, FAA,
    has the authority to approve AMOCs for this AD, if requested using
    the procedures found in 14 CFR 39.19. Send information to ATTN:
    Vladimir Ulyanov, Aerospace Engineer, International Branch, ANM-116,
    Transport Airplane Directorate, FAA, 1601 Lind Avenue, SW., Renton,
    Washington 98057-3356; telephone (425) 227-1138; fax (425) 227-1149.
    Before using any approved AMOC on any airplane to which the AMOC
    applies, notify your principal maintenance inspector (PMI) or
    principal avionics inspector (PAI), as appropriate, or lacking a
    principal inspector, your local Flight Standards District Office.
    (2) Airworthy Product: For any requirement in this AD to obtain
    corrective actions from a manufacturer or other source, use these
    actions if they are FAA-approved. Corrective actions are considered
    FAA-approved if they are approved by the State of Design Authority
    (or their delegated agent). You are required to assure the product
    is airworthy before it is returned to service.
    (3) Reporting Requirements: For any reporting requirement in
    this AD, under the provisions of the Paperwork Reduction Act, the
    Office of Management and Budget (OMB) has approved the information
    collection requirements and has assigned OMB Control Number 2120-
    0056.

    Related Information

    (h) Refer to European Aviation Safety Agency Airworthiness
    Directive 2008-0160, dated August 22, 2008, and the service
    bulletins specified in Table 3 of this AD, for related information.

    Table 3–Service Information
    —————————————————————————————————————-
    Revision
    Service Bulletin level Date
    —————————————————————————————————————-
    Airbus Mandatory Service Bulletin A330-27A3154. 01 July 25, 2008.

    [[Page 13152]]

    Airbus Service Bulletin A330-27-3110……….. 02 March 2, 2007.
    Airbus Mandatory Service Bulletin A340-27A4154. 01 July 25, 2008.
    Airbus Service Bulletin A340-27-4115……….. 01 March 2, 2007.
    —————————————————————————————————————-

    Issued in Renton, Washington, on March 18, 2009.
    Ali Bahrami,
    Manager, Transport Airplane Directorate, Aircraft Certification
    Service.
    [FR Doc. E9-6734 Filed 3-25-09; 8:45 am]

    BILLING CODE 4910-13-P

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  • |

    DR. EARL F. WEENER SWORN IN AS NTSB MEMBER

    National Transportation Safety Board
    Washington, DC 20594

    FOR IMMEDIATE RELEASE: June 30, 2010
    SB-10-25

    Earl F. Weener, Ph.D., took the oath of office today as a
    Member of the National Transportation Safety Board.

    Dr. Weener is a licensed pilot who has dedicated his entire
    career to the field of aviation safety. He most recently has
    been a consultant and fellow for the Flight Safety
    Foundation, where he worked to reduce accidents through
    coordinated industry programs.

    From 1984 to 1999, Dr. Weener held a series of positions
    with The Boeing Company, including three Chief Engineer
    positions, in Airworthiness, Reliability and
    Maintainability, and Safety; in System Engineering; and in
    Safety Technology Development. He also served four years as
    Boeing’s Manager of Government Affairs.

    He has served as a general aviation flight instructor and
    Part 135 pilot.

    Dr. Weener earned all three of his academic degrees in
    Aerospace Engineering at the University of Michigan – his
    bachelor’s, master’s and doctorate.

    Among his awards are a 1994 Laurel Award from Aviation Week
    and Space Technology magazine and, in 2005, the Honeywell
    Bendix Trophy for Aviation Safety.

    Dr. Weener’s term as a Member of the NTSB expires December
    31, 2015.

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  • |

    American Airlines Federal Credit Union Partners With PrimeVest Financial Services, Inc.

    FORT WORTH, Texas, Oct. 22 — American Airlines Federal Credit Union (AA Credit Union) is proud to announce its partnership with PrimeVest Financial Group, Inc. The services will be offered by the newly renamed Flagship Financial Group to better provide member-owners with comprehensive investment and insurance solutions for all their personal money management needs.

    PrimeVest is one of the nation’s leading broker-dealers exclusively serving clients at credit unions and banks.

    “With PrimeVest’s support, Flagship Financial Group advisors can offer a holistic approach to assisting members with their financial goals,” said Sherry Reams, Managing Director of Flagship Financial Group. “PrimeVest’s sound financial products complement AA Credit Union’s offerings.

    “The benefits of working with PrimeVest are plentiful,” Reams added. Member-owners will gain access to a large assortment of investment and insurance solutions that can be customized to fit their unique needs. Flagship Financial Group’s knowledgeable advisors will use the latest technology and resources to support the entire process making it easier to meet the varied needs of AA Credit Union members.

    Flagship Financial Group advisors will serve as PrimeVest-registered representatives at AA Credit Union. They can be reached at (800) 533-0035, Ext. 36699.

    Securities and insurance products offered by PrimeVest: are not FDIC/NCUSIF insured, may go down in value, are not financial institution guaranteed, are not deposits, and are not insured by any federal government agency.

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  • EASA publishes rules for harmonised pilot licensing

    The European Aviation Safety Agency (EASA) today published a proposal to the European Commission for a harmonised regulation on Flight Crew Licensing (Part-FCL) in the form of an ‘Opinion’. This new regulation will ensure that the same pilot licensing requirements and related high safety levels apply in all Member States.

    This ‘Opinion’ covers requirements for pilot licensing for aeroplanes, helicopters, airships, powered-lift aircraft, sailplanes and balloons. Measures to ensure a smooth transition to the new rules are also provided.

    As requested by the European Parliament in its Agenda for Sustainable General and Business Aviation, the newly developed Light Aircraft Pilot Licence, which is part of the new regulation, will facilitate the access to aviation for a broader public while maintaining a high level of safety.

    EASA’s proposal was initially open to public consultation from June 2008 to February 2009. Over 8,000 comments were received from a wide range of stakeholders and this feedback was taken into account and integrated in this ‘Opinion’.

    The new regulation on Flight Crew Licensing will be adopted by the European Commission and enter info force as Community law by April 2012.

    The ‘Opinion’ can be accessed by clicking here.

  • | |

    Comair Crash: Kentucky 2006-Findings

    Lexington: U.S. District Judge Karl Forester ruled that two pilots who took off on the wrong runway were negligent in the August 2006 Comair crash.

    A jury is deciding if punitive damages will apply.

    On August 27, 2006, about 0606:35 eastern daylight time, Comair flight 5191, a Bombardier CL-600-2B19, N431CA, crashed during takeoff from Blue Grass Airport, Lexington, Kentucky. The flight crew was instructed to take off from runway 22 but instead lined up the airplane on runway 26 and began the takeoff roll. The airplane ran off the end of the runway and impacted the airport perimeter fence, trees, and terrain. The captain, flight attendant, and 47 passengers were killed, and the first officer received serious injuries. The airplane was destroyed by impact forces and postcrash fire. The flight was operating under the provisions of 14 Code of Federal Regulations Part 121 and was en route to Hartsfield-Jackson Atlanta International Airport, Atlanta, Georgia. Night visual meteorological conditions prevailed.

    FINDINGS

    1) The captain and the first officer were properly certificated and qualified under Federal regulations. There was no evidence of any medical or behavioral conditions that might have adversely affected their performance during the accident flight. Before reporting for the accident flight, the flight crewmembers had rest periods that were longer than those required by Federal regulations and company policy.

    2) The accident airplane was properly certified, equipped, and maintained in accordance with Federal regulations. The recovered components showed no evidence of any structural, engine, or system failures.

    3) Weather was not a factor in this accident. No restrictions to visibility occurred during the airplane’s taxi to the runway and the attempted takeoff. The taxi and the attempted takeoff occurred about 1 hour before sunrise during night visual meteorological conditions and with no illumination from the moon.

    4) The captain and the first officer believed that the airplane was on runway 22 when they taxied onto runway 26 and initiated the takeoff roll.

    5) The flight crew recognized that something was wrong with the takeoff beyond the point from which the airplane could be stopped on the remaining available runway.

    6) Because the accident airplane had taxied onto and taken off from runway 26 without a clearance to do so, this accident was a runway incursion.

    7) Adequate cues existed on the airport surface and available resources were present in the cockpit to allow the flight crew to successfully navigate from the air carrier ramp to the runway 22 threshold.

    8) The flight crewmembers’ nonpertinent conversation during the taxi, which was not in compliance with Federal regulations and company policy, likely contributed to their loss of positional awareness.

    9) The flight crewmembers failed to recognize that they were initiating a takeoff on the wrong runway because they did not cross-check and confirm the airplane’s position on the runway before takeoff and they were likely influenced by confirmation bias.

    10) Even though the flight crewmembers made some errors during their preflight activities and the taxi to the runway, there was insufficient evidence to determine whether fatigue affected their performance.

    11) The flight crew’s noncompliance with standard operating procedures, including the captain’s abbreviated taxi briefing and both pilots’ nonpertinent conversation, most likely created an atmosphere in the cockpit that enabled the crew’s errors.

    12) The controller did not notice that the flight crew had stopped the airplane short of the wrong runway because he did not anticipate any problems with the airplane’s taxi to the correct runway and thus was paying more attention to his radar responsibilities than his tower responsibilities.

    13) The controller did not detect the flight crew’s attempt to take off on the wrong runway because, instead of monitoring the airplane’s departure, he performed a lower-priority administrative task that could have waited until he transferred responsibility for the airplane to the next air traffic control facility.

    14) The controller was most likely fatigued at the time of the accident, but the extent that fatigue affected his decision not to monitor the airplane’s departure could not be determined in part because his routine practices did not consistently include the monitoring of takeoffs.

    15) The Federal Aviation Administration’s operational policies and procedures at the time of the accident were deficient because they did not promote optimal controller monitoring of aircraft surface operations.

    16) The first officer’s survival was directly attributable to the prompt arrival of the first responders; their ability to extricate him from the cockpit wreckage; and his rapid transport to the hospital, where he received immediate treatment.

    17) The emergency response for this accident was timely and well coordinated.

    18) A standard procedure requiring 14 Code of Federal Regulations Part 91K, 121, and 135 pilots to confirm and cross-check that their airplane is positioned at the correct runway before crossing the hold short line and initiating a takeoff would help to improve the pilots’ positional awareness during surface operations.

    19) The implementation of cockpit moving map displays or cockpit runway alerting systems on air carrier aircraft would enhance flight safety by providing pilots with improved positional awareness during surface navigation.

    20) Enhanced taxiway centerline markings and surface painted holding position signs provide pilots with additional awareness about the runway and taxiway environment.

    21) This accident demonstrates that 14 Code of Federal Regulations 91.129(i) might result in mistakes that have catastrophic consequences because the regulation allows an airplane to cross a runway during taxi without a pilot request for a specific clearance to do so.

    22) If controllers were required to delay a takeoff clearance until confirming that an airplane has crossed all intersecting runways to a departure runway, the increased monitoring of the flight crew’s surface navigation would reduce the likelihood of wrong runway takeoff events.

    23) If controllers were to focus on monitoring tasks instead of administrative tasks when aircraft are in the controller’s area of operations, the additional monitoring would increase the probability of detecting flight crew errors.

    24) Even though the air traffic manager’s decision to staff midnight shifts at Blue Grass Airport with one controller was contrary to Federal Aviation Administration verbal guidance indicating that two controllers were needed, it cannot be determined if this decision contributed to the circumstances of this accident.

    25) Because of an ongoing construction project at Blue Grass Airport, the taxiway identifiers represented in the airport chart available to the flight crew were inaccurate, and the information contained in a local notice to airmen about the closure of taxiway A was not made available to the crew via automatic terminal information service broadcast or the flight release paperwork.

    26) The controller’s failure to ensure that the flight crew was aware of the altered taxiway A configuration was likely not a factor in the crew’s inability to navigate to the correct runway.

    27) Because the information in the local notice to airmen (NOTAM) about the altered taxiway A configuration was not needed for the pilots’ wayfinding task, the absence of the local NOTAM from the flight release paperwork was not a factor in this accident.

    28) The presence of the extended taxiway centerline to taxiway A north of runway 8/26 was not a factor in this accident.

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