96-15555. Airworthiness Directives; PTC Seating Products Division, B/E Aerospace, Model 950 Series Passenger Seats Equipped With Footrest Assembly  

  • [Federal Register Volume 61, Number 122 (Monday, June 24, 1996)]
    [Rules and Regulations]
    [Pages 32317-32318]
    From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
    [FR Doc No: 96-15555]
    
    
    
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    DEPARTMENT OF TRANSPORTATION
    
    Federal Aviation Administration
    
    14 CFR Part 39
    
    [Docket No. 95-ANE-25; Amendment 39-9651; AD 96-12-09]
    RIN 2120-AA64
    
    
    Airworthiness Directives; PTC Seating Products Division, B/E 
    Aerospace, Model 950 Series Passenger Seats Equipped With Footrest 
    Assembly
    
    AGENCY: Federal Aviation Administration, DOT.
    
    ACTION: Final rule.
    
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    SUMMARY: This amendment adopts a new airworthiness directive (AD), 
    applicable to PTC Seating Products Division, B/E Aerospace (PTC), 
    formally known as PTC Aerospace, Model 950 series passenger seats with 
    footrest assembly. This amendment will require the removal of the 
    footrest assembly arms and the installation of a conversion kit on each 
    PTC Model 950 series passenger seat equipped with footrest assembly. 
    This amendment is prompted by two incidents of finger injuries that 
    occurred during attempts to either extend or retract the footrest 
    system on PTC Model 950 series passenger seats equipped with footrest 
    assembly. The actions specified by this AD are intended to prevent 
    injury to hands during the operation of a PTC Model 950 series 
    passenger seat equipped with footrest assembly.
    
    DATES: Effective July 29, 1996.
        The incorporation by reference of certain publications listed in 
    the regulations is approved by the Director of the Federal Register 
    July 29, 1996.
    
    ADDRESSES: The service information referenced in this AD may be 
    obtained from B/E Aerospace, PTC Seating Products Division, 607 Bantam 
    Road, Litchfield, CT 06759. This information may be examined at the 
    FAA, New England Region, Office of the Assistant Chief Counsel, 12 New 
    England Executive Park, Burlington, MA; or at the Office of the Federal 
    Register, 800 North Capitol Street, NW, suite 700, Washington, DC.
    
    FOR FURTHER INFORMATION CONTACT: Richard Noll, Aerospace Engineer, 
    Boston Aircraft Certification Office, FAA, Engine and Propeller 
    Directorate, 12 New England Executive Park, Burlington, MA 01803-5299; 
    telephone (617) 238-7160, fax (617) 238-7199.
    
    SUPPLEMENTARY INFORMATION: A proposal to amend part 39 of the Federal 
    Aviation Regulations (14 CFR part 39) to include an airworthiness 
    directive (AD) that is applicable to PTC Model 950 series passenger 
    seats equipped with footrest assembly was published in the Federal 
    Register on October 2, 1995 (60 FR 51375). That action proposed to 
    require the removal of the footrest assembly arms and the installation 
    of a conversion kit on each PTC Model 950 series passenger seat 
    equipped with footrest assembly.
        Interested persons have been afforded an opportunity to participate 
    in the making of this amendment. Due consideration has been given to 
    the comments received.
        One commenter states that the compliance time of 9 months should 
    only apply to the footrest on first class Model 950 seats, stating that 
    the potential problem with the linkage only occurs on the first class 
    Model 950 seats when the footrest is in a horizontal position. The 
    commenter further states, that the compliance time should be increased 
    to 18 months on the executive class Model 950 seats, since the footrest 
    has a physical stop that limits the travel of the linkage and thus the 
    footrest to approximately 45 degrees.
        The FAA disagrees. The FAA has examined the various seats equipped 
    with footrest and finds that the potential for injury to the hands 
    exists on all of these seat models. The FAA considers the modification 
    to be repetitive and not complex, therefore, does not need to be done 
    during scheduled maintenance. An increase of the compliance time to 18 
    months is not needed.
        There are approximately 5800 seats equipped with footrest assembly 
    of the affected design in the worldwide fleet. The FAA estimates that 
    5000 seats
    
    [[Page 32318]]
    
    equipped with footrest assembly installed on aircraft of U.S. registry 
    would be affected by this AD, that it would take approximately \3/4\ 
    work hours per seat to accomplish the required actions, and that the 
    average labor rate is $60 per work hour. Required parts will cost 
    approximately $30 per seat. Based on these figures, the total cost 
    impact of the AD on U.S. operators is estimated to be $225,000.
        The regulations adopted herein will not have substantial direct 
    effects 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. Therefore, in 
    accordance with Executive Order 12612, it is determined that this final 
    rule does not have sufficient federalism implications to warrant the 
    preparation of a Federalism Assessment.
        For the reasons discussed above, I certify that this action (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. A final evaluation has been prepared for this action 
    and is contained at the location provided under the caption ADDRESSES.
    
    List of Subjects in 14 CFR Part 39
    
        Air transportation, Aircraft, Aviation safety, Incorporation by 
    reference, Safety.
    
    Adoption of the Amendment
    
        Accordingly, pursuant to the authority delegated to me by the 
    Administrator, the Federal Aviation Administration amends part 39 of 
    the Federal Aviation Regulations (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. Section 39.13 is amended by adding the following new 
    airworthiness directive: 4
    96-12-09 PTC Seating Products Division, B/E Aerospace:Amendment 39-
    9651. Docket No. 95-ANE-25.
    
        Applicability: PTC Seating Products Division, B/E Aerospace 
    (PTC) Model 950 series passenger seat equipped with footrest 
    assembly.
    
        Note: This AD applies to each seat identified in the preceding 
    applicability provision, regardless of whether it has been modified, 
    altered, or repaired in the area subject to the requirements of this 
    AD. For seats equipped with footrest assembly that have been 
    modified, altered, or repaired so that the performance of the 
    requirements of this AD is affected, the owner/operator must use the 
    authority provided in paragraph (b) to request approval from the 
    FAA. This approval may address either no action, if the current 
    configuration eliminates the unsafe condition, or different actions 
    necessary to address the unsafe condition described in this AD. Such 
    a request should include an assessment of the effect of the changed 
    configuration on the unsafe condition addressed by this AD. In no 
    case does the presence of any modification, alteration, or repair 
    remove any seat from the applicability of this AD.
    
        Compliance: Required as indicated, unless accomplished 
    previously. To prevent injury to hands during operation of the PTC 
    Model 950 series passenger seats equipped with footrest assembly, 
    accomplish the following:
        (a) Within nine calendar months after the effective date of this 
    AD,
        (1) Remove seat footrest assembly arms, P/N 98440-1 or -2, in 
    accordance with the Accomplishment Instructions of PTC Aerospace 
    Service Bulletin (SB) 25-1192, Revision A, dated March 16, 1992.
        (2) Install conversion kit, P/N 122966-1, in accordance with 
    Section 2, Accomplishment Instructions of PTC Seating Products 
    Division, B/E Aerospace SB 25-1330, dated July 27, 1994.
        (b) An alternative method of compliance or adjustment of the 
    compliance time that provides an acceptable level of safety may be 
    used if approved by the Manager, Boston Aircraft Certification 
    Office. The request should be forwarded through an appropriate FAA 
    Principal Maintenance Inspector, who may add comments and then send 
    it to the Manager, Boston Aircraft Certification Office.
    
        Note: Information concerning the existence of approved 
    alternative methods of compliance with this airworthiness directive, 
    if any, may be obtained from the Boston Aircraft Certification 
    Office.
    
        (c) The removal of seat footrest assembly arms and replacement 
    of the conversion kit shall be done in accordance with PTC Aerospace 
    Service Bulletin (SB) 25-1192, Revision A, dated March 16, 1992, 
    pages 1-5, and PTC Seating Products Division, B/E Aerospace SB 25-
    1330, dated July 27, 1994, pages 1-12. This incorporation by 
    reference was approved by the Director of the Federal Register in 
    accordance with 5 U.S.C. 552(a) and 1 CFR part 51. Copies may be 
    obtained from B/E Aerospace, PTC Seating Products Division, 607 
    Bantam Road, Litchfield, CT 06759. Copies may be inspected at the 
    FAA, New England Region, Office of the Assistant Chief Counsel, 12 
    New England Executive Park, Burlington, MA; or at the Office of the 
    Federal Register, 800 North Capital Street, NW., suite 700, 
    Washington, DC.
        (d) This amendment becomes effective July 29, 1996.
    
        Issued in Burlington, Massachusetts on June 4, 1996.
    James C. Jones,
    Acting Manager, Engine and Propeller Directorate, Aircraft 
    Certification Service.
    [FR Doc. 96-15555 Filed 6-21-96; 8:45 am]
    BILLING CODE 4910-13-U
    
    

Document Information

Effective Date:
7/29/1996
Published:
06/24/1996
Department:
Federal Aviation Administration
Entry Type:
Rule
Action:
Final rule.
Document Number:
96-15555
Dates:
Effective July 29, 1996.
Pages:
32317-32318 (2 pages)
Docket Numbers:
Docket No. 95-ANE-25, Amendment 39-9651, AD 96-12-09
RINs:
2120-AA64: Airworthiness Directives
RIN Links:
https://www.federalregister.gov/regulations/2120-AA64/airworthiness-directives
PDF File:
96-15555.pdf
CFR: (1)
14 CFR 39.13