99-14537. Airworthiness Directives; AlliedSignal Inc. VN 411B Very High Frequency (VHF) Navigation Receivers  

  • [Federal Register Volume 64, Number 112 (Friday, June 11, 1999)]
    [Rules and Regulations]
    [Pages 31490-31491]
    From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
    [FR Doc No: 99-14537]
    
    
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    DEPARTMENT OF TRANSPORTATION
    
    Federal Aviation Administration
    
    14 CFR Part 39
    
    [Docket No. 95-CE-91-AD; Amendment 39-11190; AD 99-12-06]
    RIN 2120-AA64
    
    
    Airworthiness Directives; AlliedSignal Inc. VN 411B Very High 
    Frequency (VHF) Navigation Receivers
    
    AGENCY: Federal Aviation Administration, DOT.
    
    ACTION: Final rule.
    
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    SUMMARY: This amendment adopts a new airworthiness directive (AD) that 
    requires replacing certain AlliedSignal Inc. VN 411B VHF navigation 
    receivers installed on aircraft if the receivers do not have 
    Modification 21 incorporated. This AD is the result of a report of 
    navigation receiver interference during landing operations. The actions 
    specified by this AD are intended to prevent VHF navigation receiver 
    interference from frequency modulation (FM) radio station broadcasts, 
    which could cause distortion of the navigation audio and deflection of 
    the desired flight path of the airplane during landing operations with 
    possible loss of control of the airplane.
    
    DATES: Effective July 23, 1999.
        The incorporation by reference of certain publications listed in 
    the regulations is approved by the Director of the Federal Register as 
    of July 23, 1999.
    
    ADDRESSES: Service information that applies to this AD may be obtained 
    from AlliedSignal, Inc. 23500 W. 105th Street, Olathe, Kansas 66051-
    1950. This information may also be examined at the Federal Aviation 
    Administration (FAA), Central Region, Office of the Regional Counsel, 
    Attention: Rules Docket No. 95-CE-91-AD, Room 1558, 601 E. 12th Street, 
    Kansas City, Missouri 64106; or at the Office of the Federal Register, 
    800 North Capitol Street, NW, suite 700, Washington, DC.
    
    FOR FURTHER INFORMATION CONTACT: Mr. Roger Souter, Aerospace Engineer, 
    FAA, Wichita Aircraft Certification Office, 1801 Airport Road, Room 
    100, Wichita, Kansas 67209; telephone: (316) 946-4134, facsimile: (316) 
    946-4407.
    
    SUPPLEMENTARY INFORMATION:
    
    Events Leading to the Issuance of This AD
    
        A proposal to amend part 39 of the Federal Aviation Regulations (14 
    CFR part 39) to include an AD that would apply to certain AlliedSignal 
    Inc. VN 411B very high frequency (VHF) navigation receivers installed 
    in aircraft was published in the Federal Register as a supplement 
    notice of proposed rulemaking (NPRM) on December 22, 1998 (63 FR 
    70698). The supplemental NPRM proposed to require replacing any VHF 
    navigation receiver that does not have Modification 21 incorporated 
    with one where an AlliedSignal Bendix/King-owned service center has 
    incorporated Modification 21. Accomplishment of the proposed action as 
    specified in the supplemental NPRM would be in accordance with 
    AlliedSignal Bendix/King Service Bulletin VN 411B-21, dated November 
    1996.
        The NPRM was the result of a report of navigation receiver 
    interference during landing operations.
        Interested persons have been afforded an opportunity to participate 
    in the making of this amendment. No comments were received on the 
    proposed rule or the FAA's determination of the cost to the public.
    
    The FAA's Determination
    
        After careful review of all available information related to the 
    subject presented above, the FAA has determined that air safety and the 
    public interest require the adoption of the rule as proposed except for 
    minor editorial corrections. The FAA has determined that these minor 
    corrections will not change the meaning of the AD and will not add any 
    additional burden upon the public than was already proposed.
    
    Cost Impact
    
        The FAA estimates that 19 VHF navigation receivers in the U.S. 
    registry will be affected by this AD, that it will take approximately 2 
    workhours per receiver to accomplish this action, and that the average 
    labor rate is approximately $60 an hour. The manufacturer is not 
    charging the owner/operator for exchanging the navigation receiver unit 
    and is offering 2 workhours of labor warranty credit to accomplish this 
    action. Based on these figures, this AD imposes no cost impact on U.S. 
    operators. The FAA has no way of determining if any of the affected 
    airplanes have navigation receivers with Modification 21 incorporated.
    
    Compliance Time of This AD
    
        The condition specified by this AD is not caused by actual hours 
    time-in-service (TIS) of the aircraft where the affected VHF navigation 
    receivers are installed. The need for replacing the VHF navigation 
    receiver with one that incorporates hardware modifications has no 
    correlation to the number of times the equipment is utilized or the age 
    of the equipment. For this reason, the compliance time of this AD is 
    presented in calendar time instead of hours TIS.
    
    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
    
    [[Page 31491]]
    
    impact, positive or negative, on a substantial number of small entities 
    under the criteria of the Regulatory Flexibility Act. A copy of the 
    final evaluation prepared for this action is contained in the Rules 
    Docket. A copy of it may be obtained by contacting 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 a new airworthiness directive 
    (AD) to read as follows:
    
    99-12-06  AlliedSignal Inc.: Amendment 39-11190; Docket No. 95-CE-
    91-AD.
    
        Applicability: The following very high frequency (VHF) 
    navigation receivers that are installed on, but not limited to, 
    Learjet Model 31A, Fokker Model F27-50, and British Aerospace Model 
    ATP airplanes:
    
    --VN 411B, BPN 3614004-4101, all serial numbers, that are currently 
    at Modification Status 18, 19, or 20;
    --VN 411B, BPN/KPN 3614004-4101/066-1101-00, all serial numbers, 
    that are currently at Modification Status 18, 19, or 20;
    --VN 411B, P/N 066-1101-00, serial numbers up to and including 4229, 
    that are currently at Modification Status 18, 19, or 20; and
    --VN 411B, P/N 066-1101-31/40/50, serial numbers up to and including 
    10799, that are currently at Modification Status 19 or 20.
    
        Note 1: This AD applies to each airplane in which a VHF 
    navigation receiver identified in the preceding applicability 
    provision has been installed, regardless of whether it 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 (d) 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 in the body of this AD, unless 
    already accomplished.
        To prevent VHF navigation receiver interference from frequency 
    modulation (FM) radio station broadcast frequencies, which could 
    cause distortion of the navigation audio and deflection of the 
    desired flight path of the airplane during landing operations with 
    possible loss of control of the airplane, accomplish the following:
        (a) Within the next 90 calendar days after the effective date of 
    this AD or upon replacement or repair of any affected AlliedSignal 
    VHF navigation receiver, whichever occurs first, remove the 
    navigation receiver and install one where an AlliedSignal Bendix/
    King service center has incorporated Modification 21, in accordance 
    with AlliedSignal Bendix/King Service Bulletin VN 411B-21, dated 
    November 1996.
        (b) As of the effective date of this AD, no person may install, 
    on any airplane, one of the affected VHF navigation receivers that 
    does not have Modification 21 incorporated in accordance with 
    AlliedSignal Bendix/King Service Bulletin VN 411B-21, dated November 
    1996.
        (c) 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.
        (d) An alternative method of compliance or adjustment of the 
    compliance time that provides an equivalent level of safety may be 
    approved by the Manager, Wichita Aircraft Certification Office 
    (ACO), 1801 Airport Road, Room 100, Wichita, Kansas 67209. The 
    request shall be forwarded through an appropriate FAA Maintenance 
    Inspector, who may add comments and then send it to the Manager, 
    Wichita ACO.
    
        Note 2: Information concerning the existence of approved 
    alternative methods of compliance with this AD, if any, may be 
    obtained from the Wichita ACO.
    
        (e) The removal and installation required by this AD shall be 
    done in accordance with AlliedSignal Bendix/King Service Bulletin VN 
    411B-21, dated November 1996. 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, Inc., 23500 W. 105th Street, Olathe, Kansas 66051-
    1950. Copies may be inspected at the FAA, Central Region, Office of 
    the Regional Counsel, Room 1558, 601 E. 12th Street, Kansas City, 
    Missouri, or at the Office of the Federal Register, 800 North 
    Capitol Street, NW, suite 700, Washington, DC.
        (f) This amendment becomes effective on July 23, 1999.
    
        Issued in Kansas City, Missouri, on June 2, 1999.
    Marvin R. Nuss,
    Acting Manager, Small Airplane Directorate, Aircraft Certification 
    Service.
    [FR Doc. 99-14537 Filed 6-10-99; 8:45 am]
    BILLING CODE 4910-13-P
    
    
    

Document Information

Effective Date:
7/23/1999
Published:
06/11/1999
Department:
Federal Aviation Administration
Entry Type:
Rule
Action:
Final rule.
Document Number:
99-14537
Dates:
Effective July 23, 1999.
Pages:
31490-31491 (2 pages)
Docket Numbers:
Docket No. 95-CE-91-AD, Amendment 39-11190, AD 99-12-06
RINs:
2120-AA64: Airworthiness Directives
RIN Links:
https://www.federalregister.gov/regulations/2120-AA64/airworthiness-directives
PDF File:
99-14537.pdf
CFR: (1)
14 CFR 39.13