98-16050. Airworthiness Directives; Empresa Brasileira de Aeronautica S.A. (EMBRAER) Model EMB-145 Series Airplanes  

  • [Federal Register Volume 63, Number 122 (Thursday, June 25, 1998)]
    [Rules and Regulations]
    [Pages 34559-34560]
    From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
    [FR Doc No: 98-16050]
    
    
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    DEPARTMENT OF TRANSPORTATION
    
    Federal Aviation Administration
    
    14 CFR Part 39
    
    [Docket No. 98-NM-66-AD; Amendment 39-10605; AD 98-13-17]
    RIN 2120-AA64
    
    
    Airworthiness Directives; Empresa Brasileira de Aeronautica S.A. 
    (EMBRAER) Model EMB-145 Series Airplanes
    
    AGENCY: Federal Aviation Administration, DOT.
    
    ACTION: Final rule.
    
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    SUMMARY: This amendment adopts a new airworthiness directive (AD), 
    applicable to certain EMBRAER EMB-145 series airplanes, that requires 
    modification of the windshield heating system in the flight 
    compartment. This amendment is prompted by reports of overheating and 
    delamination of the windshield because the windshield heating system 
    failed to shut off during flight. The action specified by this AD is 
    intended to prevent failure of the windshield heating system, which 
    could result in reduced pilot visibility, structural degradation of the 
    windshield, and depressurization of the airplane during flight.
    
    DATES: Effective July 30, 1998.
        The incorporation by reference of certain publications listed in 
    the regulations is approved by the Director of the Federal Register as 
    of July 30, 1998.
    
    ADDRESSES: The service information referenced in this AD may be 
    obtained from Empresa Brasileira de Aeronautica S.A. (EMBRAER), P.O. 
    Box 343--CEP 12.225, Sao Jose dos Campos--SP, Brazil. This information 
    may be examined at the Federal Aviation Administration (FAA), Transport 
    Airplane Directorate, Rules Docket, 1601 Lind Avenue, SW., Renton, 
    Washington; or at the FAA, Small Airplane Directorate, Atlanta Aircraft 
    Certification Office, One Crown Center, 1895 Phoenix Boulevard, suite 
    450, Atlanta, Georgia; or at the Office of the Federal Register, 800 
    North Capitol Street, NW., suite 700, Washington, DC.
    
    FOR FURTHER INFORMATION CONTACT: John W. McGraw, Aerospace Engineer, 
    Systems and Flight Test Branch, ACE-116A, FAA, Small Airplane 
    Directorate, Atlanta Aircraft Certification Office, One Crown Center, 
    1895 Phoenix Boulevard, suite 450, Atlanta, Georgia 30337-2748; 
    telephone (770) 703-6098; fax (770) 703-6097.
    
    
    [[Page 34560]]
    
    
    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 certain EMBRAER EMB-145 series 
    airplanes was published in the Federal Register on April 21, 1998 (63 
    FR 19677). That action proposed to require modification of the 
    windshield heating system in the flight compartment.
    
    Comments
    
        Interested persons have been afforded an opportunity to participate 
    in the making of this amendment. Due consideration has been given to 
    the single comment received.
        The commenter supports the proposed rule.
    
    Conclusion
    
        After careful review of the available data, including the comment 
    noted above, the FAA has determined that air safety and the public 
    interest require the adoption of the rule as proposed.
    
    Cost Impact
    
        The FAA estimates that 17 airplanes of U.S. registry will be 
    affected by this AD. It will take approximately 12 work hours per 
    airplane to accomplish the required modification, at an average labor 
    rate of $60 per work hour. Required parts will be supplied by the 
    manufacturer at no cost to the operators. Based on these figures, the 
    cost impact of the modification required by this AD on U.S. operators 
    is estimated to be $12,240, or $720 per airplane.
        The cost impact figure discussed above is based on assumptions that 
    no operator has yet accomplished any of the requirements of this AD 
    action, and that no operator would accomplish those actions in the 
    future if this AD were not adopted.
    
    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:
    
    98-13-17  EMPRESA BRASILEIRA dE AERONAUTICA S.A. (EMBRAER): 
    Amendment 39-10605. Docket 98-NM-66-AD.
    
        Applicability: Model EMB-145 series airplanes, serial numbers 
    145004 through 145029 inclusive; certificated in any category.
    
        Note 1: This AD applies to each airplane 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 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 (b) 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 prevent failure of the windshield heating system, which could 
    result in reduced pilot visibility, structural degradation of the 
    windshield, and depressurization of the airplane during flight, 
    accomplish the following:
        (a) Within 60 days after the effective date of this AD, modify 
    the windshield heating system in accordance with EMBRAER Service 
    Bulletin 145-30-0008, dated November 10, 1997.
        (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, Atlanta Aircraft Certification 
    Office (ACO), FAA, Small Airplane Directorate. Operators shall 
    submit their requests through an appropriate FAA Principal 
    Maintenance Inspector, who may add comments and then send it to the 
    Manager, Atlanta ACO.
    
        Note 2: Information concerning the existence of approved 
    alternative methods of compliance with this AD, if any, may be 
    obtained from the Atlanta ACO.
    
        (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) The modification shall be done in accordance with EMBRAER 
    Service Bulletin 145-30-0008, dated November 10, 1997. 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 Empresa Brasileira de Aeronautica 
    S.A. (EMBRAER), P.O. Box 343--CEP 12.225, Sao Jose dos Campos--SP, 
    Brazil. Copies may be inspected at the FAA, Transport Airplane 
    Directorate, 1601 Lind Avenue, SW., Renton, Washington; or at the 
    FAA, Small Airplane Directorate, Atlanta Aircraft Certification 
    Office, One Crown Center, 1895 Phoenix Boulevard, suite 450, 
    Atlanta, Georgia; or at the Office of the Federal Register, 800 
    North Capitol Street, NW., suite 700, Washington, DC.
        (e) This amendment becomes effective on July 30, 1998.
    
        Issued in Renton, Washington, on June 11, 1998.
    Darrell M. Pederson,
    Acting Manager, Transport Airplane Directorate, Aircraft Certification 
    Service.
    [FR Doc. 98-16050 Filed 6-24-98; 8:45 am]
    BILLING CODE 4910-13-U
    
    
    

Document Information

Effective Date:
7/30/1998
Published:
06/25/1998
Department:
Federal Aviation Administration
Entry Type:
Rule
Action:
Final rule.
Document Number:
98-16050
Dates:
Effective July 30, 1998.
Pages:
34559-34560 (2 pages)
Docket Numbers:
Docket No. 98-NM-66-AD, Amendment 39-10605, AD 98-13-17
RINs:
2120-AA64: Airworthiness Directives
RIN Links:
https://www.federalregister.gov/regulations/2120-AA64/airworthiness-directives
PDF File:
98-16050.pdf
CFR: (1)
14 CFR 39.13