99-29739. Airworthiness Directives; AlliedSignal, Instrument Landing System Navigation Receivers, as Installed in, but Not Limited to, Airbus Model A300 Series Airplanes and Boeing Model 747-100, -100B, -100B SUD, - 200B, -200F, -200C, -300, 747SR, ...  

  • [Federal Register Volume 64, Number 223 (Friday, November 19, 1999)]
    [Rules and Regulations]
    [Pages 63174-63176]
    From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
    [FR Doc No: 99-29739]
    
    
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    DEPARTMENT OF TRANSPORTATION
    
    Federal Aviation Administration
    
    14 CFR Part 39
    
    [Docket No. 99-NM-257-AD; Amendment 39-11420; AD 99-23-24]
    RIN 2120-AA64
    
    
    Airworthiness Directives; AlliedSignal, Instrument Landing System 
    Navigation Receivers, as Installed in, but Not Limited to, Airbus Model 
    A300 Series Airplanes and Boeing Model 747-100, -100B, -100B SUD, -
    200B, -200F, -200C, -300, 747SR, and 747SP Series Airplanes
    
    AGENCY: Federal Aviation Administration, DOT.
    
    ACTION: Final rule; request for comments.
    
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    SUMMARY: This amendment adopts a new airworthiness directive (AD), 
    applicable to certain instrument landing system (ILS) navigation 
    receivers manufactured by AlliedSignal. This action requires 
    replacement of certain resistors in the ILS navigation receiver with 
    higher ohm resistors and replacement of the nameplate on the receiver 
    with a new nameplate. This amendment is prompted by reports of ILS 
    navigation receivers incorrectly indicating signals from the glideslope 
    ground station during final approach. The actions specified in this AD 
    are intended to ensure the ILS receiver provides the flight crew with 
    accurate glideslope data. Inaccurate glideslope data could result in an 
    approach off the glideslope, and, consequently, a landing short of the 
    runway or a runway overrun.
    
    DATES: Effective December 6, 1999.
        The incorporation by reference of certain publications listed in 
    the regulations is approved by the Director of the Federal Register as 
    of December 6, 1999.
        Comments for inclusion in the Rules Docket must be received on or 
    before January 18, 2000.
    
    ADDRESSES: Submit comments in triplicate to the Federal Aviation 
    Administration (FAA), Transport Airplane Directorate, ANM-114, 
    Attention: Rules Docket No. 99-NM-257-AD, 1601 Lind Avenue, SW., 
    Renton, Washington 98055-4056.
        The service information referenced in this AD may be obtained from 
    AlliedSignal Aerospace, Technical Publications, Dept. 65-70, P.O. Box 
    52170, Phoenix, Arizona 85072-2170. This information may be examined at 
    the FAA, Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton, 
    Washington; or at the Office of the Federal Register, 800 North Capitol 
    Street, NW., suite 700, Washington, DC.
    
    FOR FURTHER INFORMATION CONTACT: Jay G. Yi, Aerospace Engineer, Systems 
    and Equipment Branch, ANM-130S, FAA, Transport Airplane Directorate, 
    Seattle Aircraft Certification Office, 1601 Lind Avenue, SW., Renton, 
    Washington 98055-4056; telephone (425) 227-1013; fax (425) 227-1181.
    
    SUPPLEMENTARY INFORMATION: The FAA has received reports indicating 
    that, during final approach, instrument landing system (ILS) navigation 
    receivers installed on certain Airbus Model A300 series airplanes have 
    indicated a valid signal from the glideslope ground station, though the 
    ground station was not operating. An absent glideslope signal is 
    normally indicated by the glideslope instrument warning flag on the 
    radio direction magnetic indicator. In these events, the glideslope 
    instrument warning flag moved out of view, indicating to the flight 
    crew that a valid signal had been received from the glideslope ground 
    station. Investigation revealed that the ILS navigation receiver was 
    incorrectly responding to a low-voltage signal from the glideslope 
    ground station to the ILS enable input. The manufacturer of the 
    receiver has determined that certain resistors within the receiver are 
    improperly sized to ensure a correct response to all possible voltage 
    signals. This condition, if not corrected, could result in the ILS 
    navigation receiver providing inaccurate data to the flight crew by 
    falsely indicating a valid signal from the glideslope ground station. 
    The glideslope is the vertical flight path that an airplane is to 
    follow when making an ILS landing. Inaccurate data from the ILS 
    navigation receiver could lead to the airplane making an approach off 
    the glideslope, which could result in a landing short of the runway or 
    a runway overrun.
        The affected ILS navigation receiver is installed on, but not 
    limited to, Airbus Model A300 series airplanes and Boeing Model 747-
    100, -100B, -100B SUD, -200B, -200F, -200C, -300, 747SR, and 747SP 
    series airplanes.
    
    Explanation of Relevant Service Information
    
        The FAA has reviewed and approved Bendix/King Service Bulletin RIA-
    32A-34-47, Revision 1, dated January 1992, which describes procedures 
    for replacement of three resistors in the ILS navigation receiver with 
    higher ohm resistors. The FAA also has reviewed and approved Bendix/
    King Service Bulletin RIA-32A-34-48, dated December 1991, which 
    describes procedures for replacement of the nameplate on the receiver 
    with a new nameplate (which, among other things, identifies a new part 
    number) once Bendix/King Service Bulletin RIA-32A-34-47 is 
    accomplished. Accomplishment of the actions specified in the service 
    bulletins is
    
    [[Page 63175]]
    
    intended to adequately address the identified unsafe condition.
    
    Explanation of Requirements of the Rule
    
        Since an unsafe condition has been identified that is likely to 
    exist or develop on other airplanes of the same type design, this AD is 
    being issued to ensure the ILS receiver provides the flight crew with 
    accurate glideslope data. Inaccurate glideslope data could result in an 
    approach off the glideslope, and, consequently, a landing short of the 
    runway or a runway overrun. This AD requires accomplishment of the 
    actions specified in the service bulletins described previously, except 
    as discussed below.
    
    Differences Between This AD and the Service Bulletin
    
        Operators should note that this AD requires replacement of certain 
    resistors in the ILS navigation receiver with higher ohm resistors and 
    replacement of the nameplate on the receiver with a new nameplate 
    within 6 months after the effective date of this AD. Bendix/King 
    Service Bulletin RIA-32A-34-47 recommends that replacement of the 
    resistors with higher ohm resistors should be accomplished, ``during 
    the next routine maintenance.'' In developing an appropriate compliance 
    time for this action, the FAA considered not only the degree of urgency 
    associated with addressing the subject unsafe condition, but the 
    availability of required parts. The FAA has determined that 6 months 
    represents an appropriate interval of time allowable wherein an ample 
    number of required parts will be available for modification of the U.S. 
    fleet within the compliance period. The FAA also finds that such a 
    compliance time will not adversely affect the safety of the affected 
    airplanes.
        Operators also should note that, although Bendix/King Service 
    Bulletin RIA-32A-34-48 states that the new part numbers are intended 
    for Airbus Model A300 series airplanes only, this AD requires new part 
    numbers for components installed on any airplane. The FAA has 
    determined that accurate recordkeeping for components on which the 
    replacement has been accomplished necessitates new part numbers.
    
    Cost Impact
    
        None of the airplanes affected by this action are on the U.S. 
    Register. All airplanes included in the applicability of this rule 
    currently are operated by non-U.S. operators under foreign registry; 
    therefore, they are not directly affected by this AD action. However, 
    the FAA considers that this rule is necessary to ensure that the unsafe 
    condition is addressed in the event that any of these subject airplanes 
    are imported and placed on the U.S. Register in the future.
        Should an affected airplane be imported and placed on the U.S. 
    Register in the future, it would require approximately 2 work hours to 
    accomplish the required replacement, at an average labor rate of $60 
    per work hour. Required parts would cost approximately $55 per 
    airplane. Based on these figures, the cost impact of this AD would be 
    $175 per airplane.
    
    Determination of Rule's Effective Date
    
        Since this AD action does not affect any airplane that is currently 
    on the U.S. register, it has no adverse economic impact and imposes no 
    additional burden on any person. Therefore, prior notice and public 
    procedures hereon are unnecessary and the amendment may be made 
    effective in less than 30 days after publication in the Federal 
    Register.
    
    Comments Invited
    
        Although this action is in the form of a final rule and was not 
    preceded by notice and opportunity for public comment, comments are 
    invited on this rule. Interested persons are invited to comment on this 
    rule by submitting such written data, views, or arguments as they may 
    desire. Communications shall identify the Rules Docket number and be 
    submitted in triplicate to the address specified under the caption 
    ADDRESSES. All communications received on or before the closing date 
    for comments will be considered, and this rule may be amended in light 
    of the comments received. Factual information that supports the 
    commenter's ideas and suggestions is extremely helpful in evaluating 
    the effectiveness of the AD action and determining whether additional 
    rulemaking action would be needed.
        Comments are specifically invited on the overall regulatory, 
    economic, environmental, and energy aspects of the rule that might 
    suggest a need to modify the rule. All comments submitted will be 
    available, both before and after the closing date for comments, in the 
    Rules Docket for examination by interested persons. A report that 
    summarizes each FAA-public contact concerned with the substance of this 
    AD will be filed in the Rules Docket.
        Commenters wishing the FAA to acknowledge receipt of their comments 
    submitted in response to this rule must submit a self-addressed, 
    stamped postcard on which the following statement is made: ``Comments 
    to Docket Number 99-NM-257-AD.'' The postcard will be date stamped and 
    returned to the commenter.
    
    Regulatory Impact
    
        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 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 it is contained in the Rules Docket. A copy of it may be obtained 
    from the Rules Docket 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:
    
    99-23-24 AlliedSignal: Amendment 39-11420. Docket 99-NM-257-AD.
    
        Applicability: RIA-32A instrument landing system (ILS) 
    navigation receivers having part numbers (P/N) 2070724-3201 and 
    3203; as installed in, but not limited to, Airbus Model A300 series 
    airplanes and Boeing Model 747-100, -100B, -100B SUD, -200B, -200F, 
    -200C, -300, 747SR, and 747SP series airplanes; certificated in any 
    category.
    
        Note 1: This AD applies to AlliedSignal RIA-32A ILS navigation 
    receivers having P/
    
    [[Page 63176]]
    
    N 2070724-3201 and -3203, as installed on any airplane, regardless 
    of whether the airplane has been modified, altered, or repaired in 
    the area subject to the requirements of this AD. For airplanes that 
    have been modified, altered, or repaired so that the performance of 
    the requirements of this AD is affected, the owner/operator must 
    request approval for an alternative method of compliance in 
    accordance with paragraph (c) of this AD. The request should include 
    an assessment of the effect of the modification, alteration, or 
    repair on the unsafe condition addressed by this AD; and, if the 
    unsafe condition has not been eliminated, the request should include 
    specific proposed actions to address it.
    
        Compliance: Required as indicated, unless accomplished 
    previously.
        To ensure the ILS receiver provides the flight crew with 
    accurate glideslope data, accomplish the following:
    
    Replacement
    
        (a) For ILS navigation receivers having serial numbers 1 through 
    2365 inclusive: Within 6 months after the effective date of this AD, 
    replace three resistors in the ILS navigation receiver with higher 
    ohm resistors in accordance with Bendix/King Service Bulletin RIA-
    32A-34-47, Revision 1, dated January 1992; and replace the nameplate 
    on the receiver with a new nameplate in accordance with Bendix/King 
    Service Bulletin RIA-32A-34-48, dated December 1991.
        (b) For ILS navigation receivers having serial numbers 2366 and 
    subsequent: Within 6 months after the effective date of this AD, 
    replace the nameplate on the receiver with a new nameplate in 
    accordance with Bendix/King Service Bulletin RIA-32A-34-48, dated 
    December 1991.
    
    Alternative Methods of Compliance
    
        (c) 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, Seattle Aircraft Certification 
    Office (ACO), FAA, Transport Airplane Directorate. Operators shall 
    submit their requests through an appropriate FAA Principal Avionics 
    Inspector, who may add comments and then send it to the Manager, 
    Seattle ACO.
    
        Note 2: Information concerning the existence of approved 
    alternative methods of compliance with this AD, if any, may be 
    obtained from the Seattle ACO.
    
    Special Flight Permits
    
        (d) Special flight permits may be issued in accordance with 
    sections 21.197 and 21.199 of the Federal Aviation Regulations (14 
    CFR 21.197 and 21.199) to operate the airplane to a location where 
    the requirements of this AD can be accomplished.
    
    Incorporation by Reference
    
        (e) The replacements shall be done in accordance with Bendix/
    King Service Bulletin RIA-32A-34-47, Revision 1, dated January 1992; 
    and Bendix/King Service Bulletin RIA-32A-34-48, dated December 1991. 
    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 AlliedSignal Aerospace, Technical 
    Publications, Dept. 65-70, P.O. Box 52170, Phoenix, Arizona 85072-
    2170. Copies may be inspected at the FAA, Transport Airplane 
    Directorate, 1601 Lind Avenue, SW., Renton, Washington; or at the 
    Office of the Federal Register, 800 North Capitol Street, NW., suite 
    700, Washington, DC.
        (f) This amendment becomes effective on December 6, 1999.
    
        Issued in Renton, Washington, on November 5, 1999.
    D.L. Riggin,
    Acting Manager, Transport Airplane Directorate, Aircraft Certification 
    Service.
    [FR Doc. 99-29739 Filed 11-18-99; 8:45 am]
    BILLING CODE 4910-13-P
    
    
    

Document Information

Effective Date:
12/6/1999
Published:
11/19/1999
Department:
Federal Aviation Administration
Entry Type:
Rule
Action:
Final rule; request for comments.
Document Number:
99-29739
Dates:
Effective December 6, 1999.
Pages:
63174-63176 (3 pages)
Docket Numbers:
Docket No. 99-NM-257-AD, Amendment 39-11420, AD 99-23-24
RINs:
2120-AA64: Airworthiness Directives
RIN Links:
https://www.federalregister.gov/regulations/2120-AA64/airworthiness-directives
PDF File:
99-29739.pdf
CFR: (1)
14 CFR 39.13