97-8372. Advisory Circular; Continued Rotation and Rotor Locking  

  • [Federal Register Volume 62, Number 63 (Wednesday, April 2, 1997)]
    [Notices]
    [Page 15743]
    From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
    [FR Doc No: 97-8372]
    
    
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    DEPARTMENT OF TRANSPORTATION
    
    Advisory Circular; Continued Rotation and Rotor Locking
    
    AGENCY: Federal Aviation Administration, DOT.
    
    ACTION: Notice of issuance Advisory Circular (AC) on turbine engine 
    continued rotation and rotor locking.
    
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    SUMMARY: This notice announces the issuance of Advisory Circular (AC), 
    No. 33.74/92, Turbine Engine Continued Rotation and Rotor Locking. This 
    AC is combining part 33 sections 33.74 and 33.92. This AC is on the 
    subject of continued rotation and rotor locking tests. A set of 
    improved and harmonized requirements were incorporated into part 33 of 
    the Federal Aviation Regulations (FAR's), and this AC is meant to 
    provide information and guidance concerning an acceptable method, but 
    not the only method, for complying with those new harmonized 
    requirements.
    
    DATES: Advisory Circular No. 33.74/92, was issued by the new England 
    Aircraft Certification Service, Engine and Propeller Directorate on 
    February 14, 1997.
    
    FOR FURTHER INFORMATION CONTACT: Marc Bouthillier, Engine and Propeller 
    Standards Staff, ANE-110, 12 New England Executive Park, Burlington, 
    MA, 01803, telephone (617) 238-7117, fax (617) 238-7120.
    
    SUPPLEMENTARY INFORMATION:
    
    Background
    
        This AC is on the subject of turbine engine continued rotation and 
    rotor locking tests that were identified as one where differences 
    existed between the Joint Aviation Requirements--Engines, and part 33 
    of the Federal Aviation Regulations (FAR's). A study group composed of 
    representatives of the Federal Aviation Administration, the Joint 
    Aviation Authorities, Transport Canada and industry worked to produce a 
    set of improved and harmonized requirements that was subsequently 
    incorporated into part 33 of the FAR.
        Interested parties were given the opportunity to review and comment 
    on the draft AC during the proposal and development phases. Notice was 
    published in the Federal Register on April 18, 1995 (60 FR 19442), to 
    announce the availability of, and comment to the draft AC.
        This advisory circular, published under the authority granted to 
    the Administrator by 49 U.S.C. 106(g), 4113, 44701-44702, 44704, 
    provides guidance for these new requirements that were published in the 
    Federal Register on June 4, 1996 (61 FR 28430).
    
        Issued in Burlington, Massachusetts, on March 26, 1997.
    James C. Jones,
    Acting Manager, Engine and Propeller Directorate, Aircraft 
    Certification Service.
    [FR Doc. 97-8372 Filed 4-1-97; 8:45 am]
    BILLING CODE 4910-13-M
    
    
    

Document Information

Published:
04/02/1997
Department:
Transportation Department
Entry Type:
Notice
Action:
Notice of issuance Advisory Circular (AC) on turbine engine continued rotation and rotor locking.
Document Number:
97-8372
Dates:
Advisory Circular No. 33.74/92, was issued by the new England Aircraft Certification Service, Engine and Propeller Directorate on February 14, 1997.
Pages:
15743-15743 (1 pages)
PDF File:
97-8372.pdf