97-13267. Rotorcraft, Transport Airplane, and Normal and Utility Airplane Seating Systems  

  • [Federal Register Volume 62, Number 98 (Wednesday, May 21, 1997)]
    [Notices]
    [Pages 27832-27833]
    From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
    [FR Doc No: 97-13267]
    
    
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    DEPARTMENT OF TRANSPORTATION
    
    Federal Aviation Administration
    
    
    Rotorcraft, Transport Airplane, and Normal and Utility Airplane 
    Seating Systems
    
    AGENCY: Federal Aviation Administration.
    
    ACTION: Notice of availability for public comment.
    
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    SUMMARY: This notice announces the availability of and requests 
    comments on a proposed revision to the Technical Standard Order 
    pertaining to aircraft seating systems. The proposed TSO prescribes the 
    minimum performance standards that aircraft seating systems must meet 
    to be identified with the marking ``TSO-C127a.''
    
    DATES: Comments must identify the TSO file number and be received on or 
    before August 29, 1997.
    
    ADDRESSES: Send all comments on the proposed Technical Standard Order 
    to: Technical Programs and Continued Airworthiness Branch, AIR-120, 
    Aircraft Engineering Division, Aircraft Certification Service--File No. 
    TSO-C127a, Federal Aviation Administration, 800 Independence Avenue, 
    SW., Washington, DC 20591. Or deliver comments to: Federal Aviation 
    Administration, Room 815, 800 Independence Avenue, SW., Washington, DC 
    20591.
    
    FOR FURTHER INFORMATION CONTACT:
    Ms. Bobbie J. Smith, Technical Programs and Continued Airworthiness 
    Branch, AIR-120, Aircraft Engineering Division, Aircraft Certification 
    Service, Federal Aviation Administration, 800 Independence Avenue, SW., 
    Washington, DC 20591, Telephone (202) 267-9546.
    
    Comments Invited
    
        Interested persons are invited to comment on the proposed revision 
    to TSO-C127 listed in this notice by submitting such written data, 
    views, or arguments as they desire to the above specified address. 
    Comments received on the proposed technical standard order may be 
    examined, before and after the comment closing date, in Room 815, FAA 
    Headquarters Building (FOB-10A), 800 Independence Avenue, SW., 
    Washington, DC 20591, weekdays except Federal holidays, between 8:30 
    a.m. and 4:30 p.m. All communications received on or before the closing 
    date for comments specified above will be considered by the Director of 
    the Aircraft Certification Service before issuing the final TSO.
    
    Background
    
        The FAA held two public meetings on 16-g dynamic testing seat 
    compliance in March and November 1995. In consideration of comments 
    received at these meetings regarding the difficulties associated with 
    demonstrating compliance with the requirements of TSO-C127, the FAA 
    decided that a revision to TSO-C127 would be
    
    [[Page 27833]]
    
    beneficial in eliminating some of the stated constraints and speed up 
    TSO approvals.
        TSO articles are considered ``stand alone'' items with broad 
    application and are intended to be design and production approvals 
    independent of installation. The existing TSO provided performance 
    standards for aircraft seating systems and incorporated a number of 
    installation requirements related to head impacts and emergency 
    evacuation. The proposed revision to TSO-C127, which references Society 
    of Automotive Engineers (SAE) Aerospace Standard (AS) 8049, includes 
    the following: deletes the pass/fail criteria for permanent structural 
    deformation, head injury criteria (HIC), and femur loads; expands the 
    belt angle between applicability to general aviation by including 
    additional requirements for compliance with 14 CFR Sec. 23.562; 
    includes a general design requirement specifying that seat the belt and 
    the seat pan (horizontal), be 45-55 degrees; requires additional 
    marking to include the seating system, safety belt and seat cushion 
    part numbers, and minimum seat pitch; permits optional marking to allow 
    aircraft-specific installation limitations; and requires additional 
    data requirements for the manufacturer to report HIC, head strike path, 
    permanent deformations, and femur loads results to the installer/user.
    
    How To Obtain Copies
    
        A copy of the proposed TSO-C127a may be obtained by contacting 
    ``For Further Information Contact.''
        Copies of SAE Aerospace Standard (AS) 8049, ``Performance Standards 
    for Seats in Civil Rotocraft and Transport Airplanes,'' dated July 
    1990, may be purchased from the Society of Automotive Engineers, Inc., 
    Department 331, 400 Commonwealth Drive, Warrendale, PA 15096-0001.
    
        Issued in Washington, DC, on May 16, 1997.
    John K. McGrath,
    Manager, Aircraft Engineering Division, Aircraft Certification Service.
    [FR Doc. 97-13267 Filed 5-20-97; 8:45 am]
    BILLING CODE 4910-13-M
    
    
    

Document Information

Published:
05/21/1997
Department:
Federal Aviation Administration
Entry Type:
Notice
Action:
Notice of availability for public comment.
Document Number:
97-13267
Dates:
Comments must identify the TSO file number and be received on or before August 29, 1997.
Pages:
27832-27833 (2 pages)
PDF File:
97-13267.pdf