97-19358. Airborne Navigation Sensors Using the Global Positioning System (GPS) Augmented by the Wide Area Augmentation System (WAAS)  

  • [Federal Register Volume 62, Number 141 (Wednesday, July 23, 1997)]
    [Notices]
    [Pages 39575-39577]
    From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
    [FR Doc No: 97-19358]
    
    
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    DEPARTMENT OF TRANSPORTATION
    
    Federal Aviation Administration
    
    
    Airborne Navigation Sensors Using the Global Positioning System 
    (GPS) Augmented by the Wide Area Augmentation System (WAAS)
    
    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 Technical Standard Order pertaining to airborne 
    navigation sensors using GPS augmented by WAAS. The proposed TSO 
    prescribes the performance standards that manufacturer-specified 
    appliances must meet to be identified with the marking ``TSO-C145.''
    
    DATES: Comments must identify the TSO file number and be received on or 
    before October 30, 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-C145, Federal Aviation Administration, 800 Independence Avenue, SW, 
    Washington, DC 20591. Or deliver comments to: Federal Aviation
    
    [[Page 39576]]
    
    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 TSO 
    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
    
        At the request of the FAA, the RTCA, Incorporated Special 
    Committee, SC-159 convened to develop standards for the use of the 
    Global Positioning System. The recommendations of this committee 
    provide the basis for the January 16, 1996 publication of the Minimum 
    Operational Performance Standards for Global Positioning System/Wide 
    Area Augmentation System Airborne Equipment, RTCA/DO-229, which is the 
    foundation for the requirements set forth in this proposed Technical 
    Standard Order.
        The standards of proposed TSO-C145 apply to airborne GPS/WAAS 
    sensors that provide position information to a navigation management 
    unit. Using this position information, the navigation management unit 
    outputs deviation commands, referenced to a desired flight path, for 
    use by the pilot or autopilot to guide the aircraft. Proposed TSO-C145 
    does not address integration issues or the use of this position 
    information for any other applications.
    
    Marking
    
        To fulfill the requirements of 14 CFR 21.607(d), the manufacturer 
    would have to permanently and legibly mark at least one major component 
    of the article with the markings listed in that paragraph. In addition 
    to the requirements of 14 CFR 21.607, this TSO proposes requirements 
    for marking of separate components. Each separate component would have 
    to be permanently and legibly marked with the name of the manufacturer, 
    manufacturer's part number, and the TSO number.
        If the component includes software, the part number would have to 
    include the hardware and software identification; that part number 
    would have to uniquely identify the hardware and software design, 
    including the modification status. Separate part numbers would be 
    acceptable for hardware and software.
    
    Data Requirements
    
        The proposed TSO has the following technical data submittal 
    requirements to comply with 14 CFR 21.605(a)(2):
        1. Operating instructions and equipment limitations. The 
    limitations shall be sufficient to describe the operational capability 
    of the equipment.
        2. Installation procedures and limitations. The limitations shall 
    be sufficient to ensure that the article, when installed in accordance 
    with the installation procedures, continues to meet the requirements of 
    this TSO. The limitations shall also be sufficient to identify any 
    unique aspects of the installation. The limitations shall include at 
    least the following
        a. A note with the following statement:
        ``The conditions and tests required for TSO approval of this 
    article are minimum performance standards. It is the responsibility of 
    those desiring to install this article either on or within a specific 
    type or class of aircraft to determine that the article, when 
    installed, performs in accordance with the design specifications that 
    meet this TSO. The article may be installed only if further evaluation 
    by the applicant documents an acceptable installation and is approved 
    by the Administrator.''
        b. Adequate specification of the interface between the GPS/WAAS 
    sensor and other systems to ensure proper functioning of the integrated 
    system. This must include maximum tolerable currents and voltages into 
    the antenna port if the equipment is to be installed with a standard 
    antenna (TSO-C144).
        c. If the equipment has only been demonstrated to satisfy the 
    requirements of RTCA/DO-229 when used in conjunction with a particular 
    antenna, the use of that antenna (by part number) must be specified as 
    a limitation.
        (d) If the equipment is dependent on any inputs in order to satisfy 
    the requirements of RTCA/DO-229 (e.g., baro-aided FDE), those inputs 
    should be made a requirement on the installation (i.e., a limitation).
        e. When applicable, identification that the article is an 
    incomplete system or a multi-use system. This must describe the 
    functions that are intended to be provided by the article.
        3. Schematic drawings as applicable to the installation procedures.
        4. Wiring drawings as applicable to the installation procedures.
        5. Specifications.
        6. List of the components (by part number) that make up the 
    equipment system complying with the standards prescribed in this TSO.
        7. Instructions for periodic maintenance and calibration which are 
    necessary for continued airworthiness once the article is installed.
        8. An environmental qualifications form as described in RTCA/DO-
    160C for each component of the system.
        9. Manufacturer's TSO qualification test report.
        10. Nameplate drawing.
        11. A drawing list, enumerating all of the drawings and processes 
    that are necessary to define the article's design.
        12. If the article includes software: Plan for Software Aspects of 
    Certification (PSAC), Software Configuration Index, and Software 
    Accomplishment Summary.
    
        Note: The FAA recommends that the PSAC be submitted early in the 
    software development process. Early submittal will allow timely 
    resolution of issues such as partitioning and determination of 
    software levels.
    
        Note that there is also data that must be made available upon the 
    request of the ACO manager. They are listed in Paragraph 5 of proposed 
    TSO C-145.
    
    Data To Be Furnished With Manufactured Articles
    
        The proposed TSO would require the TSOA holder to provide the 
    article purchaser with certain data described in Paragraph 5 of 
    proposed TSO C-145.
    
    How To Obtain Copies
    
        A copy of the proposed TSO-C145 may be obtained via Internet 
    (http:/www.faa.gov/avr/air/100home.htm) or on request from the office 
    listed under FOR FURTHER INFORMATION CONTACT. Copies of RTCA Document 
    No. DO-229, ``Minimum Operational Performance Standards for Global 
    Positioning System/Wide Area Augmentation System Airborne Equipment'', 
    dated January 16, 1996, may be purchased from RTCA, Inc., 1140 
    Connecticut Avenue, NW., Suite 1020, Washington, DC 20036.
    
    
    [[Page 39577]]
    
    
        Issued in Washington, DC, on July 17, 1997.
    John K. McGrath,
    Manager, Aircraft Engineering Division, Aircraft Certification Service.
    [FR Doc. 97-19358 Filed 7-22-97; 8:45 am]
    BILLING CODE 9410-13-M
    
    
    

Document Information

Published:
07/23/1997
Department:
Federal Aviation Administration
Entry Type:
Notice
Action:
Notice of availability for public comment.
Document Number:
97-19358
Dates:
Comments must identify the TSO file number and be received on or before October 30, 1997.
Pages:
39575-39577 (3 pages)
PDF File:
97-19358.pdf