95-22592. Airworthiness Directives; Boeing Model 737 Series Airplanes Equipped With BFGoodrich Main Landing Gear Brake Assemblies  

  • [Federal Register Volume 60, Number 176 (Tuesday, September 12, 1995)]
    [Proposed Rules]
    [Page 47314]
    From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
    [FR Doc No: 95-22592]
    
    
    
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    DEPARTMENT OF TRANSPORTATION
    
    Federal Aviation Administration
    
    14 CFR Part 39
    
    [Docket No. 95-NM-40-AD]
    
    
    Airworthiness Directives; Boeing Model 737 Series Airplanes 
    Equipped With BFGoodrich Main Landing Gear Brake Assemblies
    
    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 
    Boeing Model 737 series airplanes. That action would have required 
    inspection of certain brake assemblies to determine the part number of 
    the torque plates, measurement of the amount of wear remaining on the 
    brake wear pin indicator, and removal of brake assemblies on which 
    misidentified torque plates were installed and replacement with 
    serviceable brakes. Since the issuance of the NPRM, the Federal 
    Aviation Administration (FAA) has received new data indicating that all 
    misidentified torque plates have been removed from airplanes and spare 
    part inventories. Accordingly, the proposed rule is withdrawn.
    
    FOR FURTHER INFORMATION CONTACT: David M. Herron, 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 (206) 227-2672; fax 
    (206) 227-1181.
    
    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 Boeing Model 737 series 
    airplanes, was published in the Federal Register as a Notice of 
    Proposed Rulemaking (NPRM) on April 17, 1995 (60 FR 19181). The 
    proposed rule would have required a one-time inspection of certain 
    brake assemblies to determine the part number of the torque plates, 
    measurement of the amount of wear remaining on the brake wear pin 
    indicator, and removal of brake assemblies on which misidentified 
    torque plates were installed and replacement with serviceable brakes. 
    That action was prompted by a report indicating that certain torque 
    plates were misidentified and installed on certain brake assemblies. 
    The proposed actions were intended to prevent decreased brake 
    performance during a rejected takeoff or landing when these brakes are 
    at or near their indicated wear limit.
        Since the issuance of that NPRM, Boeing and BFGoodrich have 
    initiated an aggressive inspection program to ensure that the 
    misidentified torque plates are removed from airplanes and spare part 
    inventories. These manufacturers have provided substantiating data to 
    the FAA to account for all misidentified torque plates. (Boeing 
    submitted a letter dated May 3, 1995, and BFGoodrich transmitted a fax 
    memorandum dated May 17, 1995, which account for each misidentified 
    torque plate.)
        Based upon the FAA's review of the data submitted by these 
    manufacturers, the FAA has determined that the previously identified 
    unsafe condition no longer exists. Accordingly, the proposed rule is 
    hereby withdrawn.
        Withdrawal of this notice of proposed rulemaking 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.
        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 95-NM-40-AD, 
    published in the Federal Register on April 17, 1995 (60 FR 19181), is 
    withdrawn.
    
        Issued in Renton, Washington, on September 6, 1995.
    Darrell M. Pederson,
    Acting Manager, Transport Airplane Directorate, Aircraft Certification 
    Service.
    [FR Doc. 95-22592 Filed 9-11-95; 8:45 am]
    BILLING CODE 4910-13-U
    
    

Document Information

Published:
09/12/1995
Department:
Federal Aviation Administration
Entry Type:
Proposed Rule
Action:
Proposed rule; withdrawal.
Document Number:
95-22592
Pages:
47314-47314 (1 pages)
Docket Numbers:
Docket No. 95-NM-40-AD
PDF File:
95-22592.pdf
CFR: (1)
14 CFR 39