96-13611. Airworthiness Directives; Airbus Model A300-600 Series Airplanes  

  • [Federal Register Volume 61, Number 106 (Friday, May 31, 1996)]
    [Proposed Rules]
    [Pages 27321-27322]
    From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
    [FR Doc No: 96-13611]
    
    
    
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    [[Page 27322]]
    
    DEPARTMENT OF TRANSPORTATION
    
    Federal Aviation Administration
    
    14 CFR Part 39
    
    [Docket No. 94-NM-55-AD]
    RIN 2120-AA64
    
    
    Airworthiness Directives; Airbus Model A300-600 Series Airplanes
    
    AGENCY: Federal Aviation Administration, DOT.
    
    ACTION: Proposed rule; withdrawal.
    
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    SUMMARY: This action withdraws a notice of proposed rulemaking (NPRM) 
    that proposed a new airworthiness directive (AD), applicable to certain 
    Airbus Model A300-600 series airplanes. That action would have required 
    replacement of certain feel and limitation computers (FLC) with 
    modified FLC's. Since the issuance of the NPRM, the Federal Aviation 
    Administration (FAA) has issued other rulemaking that requires actions 
    equivalent to and beyond those proposed. Accordingly, the proposed rule 
    is withdrawn.
    
    FOR FURTHER INFORMATION CONTACT: Tom Groves, Aerospace Engineer, 
    Standardization Branch, ANM-113, FAA, Transport Airplane Directorate, 
    1601 Lind Avenue, SW., Renton, Washington 98055-4056; telephone (206) 
    227-1503; fax (206) 227-1149.
    
    SUPPLEMENTARY INFORMATION: A proposal to amend part 39 of the Federal 
    Aviation Regulations (14 CFR part 39) to add a new airworthiness 
    directive (AD), applicable to certain Airbus Model A300-600 series 
    airplanes, was published in the Federal Register as a Notice of 
    Proposed Rulemaking (NPRM) on May 18, 1994 (59 FR 25844). The proposed 
    rule would have required the replacement of certain feel and limitation 
    computers (FLC) with modified FLC's, in accordance with instructions 
    contained in Airbus Service Bulletin A300-27-6025, dated September 15, 
    1993. That action was prompted by reports that the elevator control on 
    several in-service airplanes operated with stiffness. The proposed 
    actions were intended to prevent stiff operation of the elevator 
    control and undetected loss of the rudder travel limitation function, 
    which may adversely affect the controllability of the airplane.
    
    Actions That Occurred Since the NPRM Was Issued
    
        Since the issuance of that NPRM, the FAA has issued AD 96-09-02, 
    amendment 39-9576 (61 FR 18665, April 29, 1996). That AD requires the 
    installation of modified FLC's on Airbus Model A300-600 series 
    airplanes, as well as other Airbus models. Like the NPRM, that AD was 
    prompted by reports indicating that the elevator control operated with 
    stiffness. The actions required by that AD are intended to prevent 
    stiff operation of the elevator control and undetected loss of rudder 
    travel limitation function, which could adversely affect the 
    controllability of the airplane.
    
    FAA's Conclusions
    
        The requirements of AD 96-09-02 address the same unsafe condition 
    that would have been addressed by the NPRM issued as Docket 94-NM-55-
    AD. That AD also incorporates and implements the same actions that were 
    proposed by the NPRM, as well as additional actions found necessary to 
    address the unsafe condition comprehensively. In light of this, the 
    issuance of a final action for this NPRM is unnecessary. Accordingly, 
    the proposed rule is hereby withdrawn.
        Withdrawal of this NPRM constitutes only such action, and does not 
    preclude the agency from issuing another notice in the future, nor does 
    it commit the agency to any course of action in the future.
    
    Regulatory Impact
    
        Since this action only withdraws a notice of proposed rulemaking, 
    it is neither a proposed nor a final rule and therefore, is not covered 
    under Executive Order 12866, the Regulatory Flexibility Act, or DOT 
    Regulatory Policies and Procedures (44 FR 11034, February 26, 1979).
    
    List of Subjects in 14 CFR Part 39
    
        Air transportation, Aircraft, Aviation safety, Safety.
    
    The Withdrawal
    
        Accordingly, the notice of proposed rulemaking, Docket 94-NM-55-AD, 
    published in the Federal Register on May 18, 1994 (59 FR 25844), is 
    withdrawn.
    
        Issued in Renton, Washington, on May 23, 1996.
    John J. Hickey,
    Acting Manager, Transport Airplane Directorate, Aircraft Certification 
    Service.
    [FR Doc. 96-13611 Filed 5-30-96; 8:45 am]
    BILLING CODE 4910-13-U
    
    

Document Information

Published:
05/31/1996
Department:
Federal Aviation Administration
Entry Type:
Proposed Rule
Action:
Proposed rule; withdrawal.
Document Number:
96-13611
Pages:
27321-27322 (2 pages)
Docket Numbers:
Docket No. 94-NM-55-AD
RINs:
2120-AA64: Airworthiness Directives
RIN Links:
https://www.federalregister.gov/regulations/2120-AA64/airworthiness-directives
PDF File:
96-13611.pdf
CFR: (1)
14 CFR 39