99-3733. Airworthiness Directives; Empresa Brasileira de Aeronautica S.A. (EMBRAER) Model EMB-145 Series Airplanes  

  • [Federal Register Volume 64, Number 32 (Thursday, February 18, 1999)]
    [Rules and Regulations]
    [Pages 7993-7994]
    From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
    [FR Doc No: 99-3733]
    
    
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    DEPARTMENT OF TRANSPORTATION
    
    Federal Aviation Administration
    
    14 CFR Part 39
    
    [Docket No. 98-NM-317-AD; Amendment 39-10904; AD 98-24-19]
    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; correcting amendment.
    
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    SUMMARY: This document corrects information in an existing 
    airworthiness directive (AD) that applies to certain Empresa Brasileira 
    de Aeronautica S.A. (EMBRAER) Model EMB-145 series airplanes. That AD 
    currently requires revising the Performance Section of the Airplane 
    Flight Manual (AFM) to provide the flightcrew with procedures to adjust 
    landing distances for landings performed with the anti-icing system 
    active. That AD also requires revising the Limitations Section of the 
    AFM to prohibit certain types of approaches with the anti-icing system 
    active. This document corrects a typographical error that resulted in 
    reference to a supplement of the AFM that does not exist. This 
    correction is necessary to ensure that the appropriate supplement of 
    the AFM is revised.
    
    DATES: Effective December 10, 1998.
        The incorporation by reference of certain publications listed in 
    the regulations was approved previously by the Director of the Federal 
    Register as of December 10, 1998 (63 FR 65050, November 25, 1998).
    
    FOR FURTHER INFORMATION CONTACT: Thomas Peters, Aerospace Engineer, 
    ACE-118A, FAA, Small Airplane Directorate, Atlanta Aircraft 
    Certification Office, One Crown Center, 1895 Phoenix Boulevard, suite 
    450, Atlanta, Georgia 30349; telephone (770) 703-6063; fax (770) 703-
    6097.
    
    SUPPLEMENTARY INFORMATION: On November 16, 1998, the Federal Aviation 
    Administration (FAA) issued AD 98-24-19, amendment 39-10904 (63 FR 
    65050, November 25, 1998), which applies to certain Empresa Brasileira 
    de Aeronautica S.A. (EMBRAER) Model EMB-145 series airplanes. That AD 
    requires revising the Performance Section of the Airplane Flight Manual 
    (AFM) to provide the flightcrew with procedures to adjust landing 
    distances for landings performed with the anti-icing system active. 
    That AD also requires revising the Limitations Sections of the AFM to 
    prohibit certain types of approaches with the anti-icing system active. 
    That AD was prompted by a report that increased (i.e., higher than 
    normal) flight idle thrust may occur when the anti-icing system is 
    active. The actions required by that AD are intended to ensure that the 
    flightcrew is advised of appropriate landing field lengths when 
    operating with the anti-icing system active, and that instrument 
    approaches at certain flap settings are prohibited with the anti-icing 
    system active. Increased flight idle thrust when the anti-icing system 
    is active, if not corrected, could result in landing overrun.
    
    Need for the Correction
    
        As published, AD 98-24-19 contains a typographical error in 
    paragraph (a)(2) of the AD. That paragraph specified a revision to the 
    Limitations Section of Supplement 12 of the FAA-approved AFM; however, 
    the correct supplement is Supplement 6. Supplement 12 of the AFM does 
    not exist.
        The FAA has determined that a correction to AD 98-24-19 is 
    necessary. The correction will ensure that the appropriate supplement 
    of the AFM is revised.
    
    Correction of Publication
    
        This document corrects the error and revises the AD as an amendment 
    to section 39.13 of the Federal Aviation Regulations (14 CFR 39.13).
        The AD is reprinted in its entirety for the convenience of affected 
    operators. The effective date of the AD remains December 10, 1998.
        Since this action only corrects a typographical error, it has no 
    adverse economic impact and imposes no additional burden on any person. 
    Therefore, the FAA has determined that notice and public procedures are 
    unnecessary.
    
    [[Page 7994]]
    
    List of Subjects in 14 CFR Part 39
    
        Air transportation, Aircraft, Aviation safety, Incorporation by 
    reference, Safety.
    
    Adoption of the Correction
    
        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) by making the 
    following correcting amendment:
    
    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  [Corrected]
    
        2. Section 39.13 is amended by revising the following airworthiness 
    directive (AD):
    
    98-24-19  Empresa Brasileira de Aeronautica S.A. (EMBRAER): 
    Amendment 39-10904. Docket 98-NM-317-AD.
    
        Applicability: Model EMB-145 series airplanes, equipped with 
    Allison Model AE3007A1/2 engines; certificated in any category.
        Compliance: Required as indicated, unless accomplished 
    previously.
        To ensure that the flightcrew is advised of appropriate landing 
    field lengths when operating with the anti-icing system active, and 
    that instrument approaches at certain flap settings are prohibited 
    with the anti-icing system active, accomplish the following:
        (a) Within 10 days after the effective date of this AD, 
    accomplish the actions specified by paragraphs (a)(1) and (a)(2) of 
    this AD.
        (1) Revise the Performance Section of the FAA-approved Airplane 
    Flight Manual (AFM) by inserting a copy of EMBRAER EMB-145 AFM 145/
    1153, Revision 19, dated October 23, 1998, into the AFM.
    
        Note 1: When landing in abnormal configurations per the 
    emergency and abnormal procedures of Section 3 of the AFM and 
    operating with the anti-icing system active, the landing field 
    length multiples specified in Section 3 should be applied to the 
    landing field lengths specified in Supplement 6 of Revision 19 of 
    the AFM.
    
        (2) Revise the Limitations Section of Supplement 6 of the FAA-
    approved AFM to include the following statement. This action may be 
    accomplished by inserting a copy of this AD into the AFM.
    
    ``Flaps 22 instrument approaches with anti-ice on are not 
    approved.''
    
        (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 AFM revision specified in paragraph (a)(1) of this AD 
    shall be done in accordance with EMBRAER EMB-145 Airplane Flight 
    Manual 145/1153, Revision 19, dated October 23, 1998, which contains 
    the following list of effective pages:
    
    ------------------------------------------------------------------------
                                       Revision
               Page No.               level shown      Date shown  on page
                                        on page
    ------------------------------------------------------------------------
    List of Effective Pages, Pages              19  October 23, 1998.
     A, S6-i, S6-ii.
    List of Effective Pages, Page               18  August 6, 1998.
     B.
    ------------------------------------------------------------------------
    
    This incorporation by reference was approved previously by the 
    Director of the Federal Register in accordance with 5 U.S.C. 552(a) 
    and 1 CFR part 51 as of December 10, 1998 (63 FR 65050, November 25, 
    1998). 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) The effective date of this amendment remains December 10, 
    1998.
    
        Issued in Renton, Washington, on February 9, 1999.
    John J. Hickey,
    Acting Manager, Transport Airplane Directorate, Aircraft Certification 
    Service.
    [FR Doc. 99-3733 Filed 2-17-99; 8:45 am]
    BILLING CODE 4910-13-U
    
    
    

Document Information

Effective Date:
12/10/1998
Published:
02/18/1999
Department:
Federal Aviation Administration
Entry Type:
Rule
Action:
Final rule; correcting amendment.
Document Number:
99-3733
Dates:
Effective December 10, 1998.
Pages:
7993-7994 (2 pages)
Docket Numbers:
Docket No. 98-NM-317-AD, Amendment 39-10904, AD 98-24-19
RINs:
2120-AA64: Airworthiness Directives
RIN Links:
https://www.federalregister.gov/regulations/2120-AA64/airworthiness-directives
PDF File:
99-3733.pdf
CFR: (1)
14 CFR 39.13