99-26710. Airworthiness Directives; Pratt & Whitney JT9D Series Turbofan Engines; Correction  

  • [Federal Register Volume 64, Number 199 (Friday, October 15, 1999)]
    [Rules and Regulations]
    [Page 55815]
    From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
    [FR Doc No: 99-26710]
    
    
    
    [[Page 55815]]
    
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    DEPARTMENT OF TRANSPORTATION
    
    Federal Aviation Administration
    
    14 CFR Part 39
    
    [Docket No. 98-ANE-31-AD; Amendment 39-11221; AD 99-15-02]
    RIN 2120-AA64
    
    
    Airworthiness Directives; Pratt & Whitney JT9D Series Turbofan 
    Engines; Correction
    
    AGENCY: Federal Aviation Administration, DOT.
    
    ACTION: Final rule; correction.
    
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    SUMMARY: This document makes a correction to Airworthiness Directive 
    (AD) 99-15-02 applicable to certain Pratt &Whitney (PW) JT9D series 
    turbofan engines that was published in the Federal Register on July 16, 
    1999 (64 FR 38299). Part number (P/N) and service bulletin (SB) 
    references in the compliance section are incorrect. This document 
    corrects those references. In all other respects, the original document 
    remains the same.
    
    EFFECTIVE DATE: October 15, 1999.
    
    FOR FURTHER INFORMATION CONTACT: Peter White, Aerospace Engineer, 
    Engine Certification Office, FAA, Engine and Propeller Directorate, 12 
    New England Executive Park, Burlington, MA 01803-5299; telephone (781) 
    238-7128, fax (781) 238-7199.
    
    SUPPLEMENTARY INFORMATION: A final rule airworthiness directive 
    applicable to Pratt & Whitney (PW) JT9D-3A, -7, -7H, -7A, -7AH, -7F, -
    7J, -20, and -20J series turbofan engines, was published in the Federal 
    Register on July 16, 1999 (64 FR 38299). The part number referenced in 
    the AD should read 734514 instead of 734515. After performing the 
    required actions on the flange, P/N 734514, the entire case becomes P/N 
    734515. Thus, there is no flange with P/N 734715, and the AD must be 
    corrected to eliminate this typographical error. In addition, the 
    Service Bulletin referenced for performing the inspections is changed 
    to refer to the SB that contains the actual inspection procedure. ASB 
    6343 only refers to ASB 4482. The following correction is needed:
    
    
    Sec. 39.13  [Corrected]
    
        1. On page 38300, in the third column, in the Compliance Section, 
    in paragraph (d), in the fifth line, ``P/N 734515'' is corrected to 
    read ``P/N 734514''.
        2. On page 38300, in the third column, in the Compliance Section, 
    in paragraph (d), in the seventh and eighth line, ``PW ASB No. 6343 
    Revision 1, dated October 8, 1998'' is corrected to read ``PW SB No. 
    4482, Revision 1, dated July 8, 1976''.
        3. On page 38300, in the third column, in the Compliance Section, 
    in paragraph (e), in the second line, ``P/Ns 734515'' is corrected to 
    read ``P/Ns 734514''.
    
        Issued in Burlington, Massachusetts, on October 6, 1999.
    Thomas A. Boudreau,
    Acting Manager, Engine and Propeller Directorate, Aircraft 
    Certification Service.
    [FR Doc. 99-26710 Filed 10-14-99; 8:45 am]
    BILLING CODE 4910-13-U
    
    
    

Document Information

Effective Date:
10/15/1999
Published:
10/15/1999
Department:
Federal Aviation Administration
Entry Type:
Rule
Action:
Final rule; correction.
Document Number:
99-26710
Dates:
October 15, 1999.
Pages:
55815-55815 (1 pages)
Docket Numbers:
Docket No. 98-ANE-31-AD, Amendment 39-11221, AD 99-15-02
RINs:
2120-AA64: Airworthiness Directives
RIN Links:
https://www.federalregister.gov/regulations/2120-AA64/airworthiness-directives
PDF File:
99-26710.pdf
CFR: (1)
14 CFR 39.13