C0-24901. Airworthiness Directives; General Electric Company CF6-50 Series Turbofan Engines  

  • [Federal Register Volume 65, Number 200 (Monday, October 16, 2000)]
    [Corrections]
    [Page 61216]
    From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
    [FR Doc No: C0-24901]
    
    
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    DEPARTMENT OF TRANSPORTATION
    
    Federal Aviation Administration
    
    14 CFR Part 39
    
    [Docket No. 2000-NE-38-AD; Amendment 39-11913; AD 2000-20-02]
    
    
    Airworthiness Directives; General Electric Company CF6-50 Series 
    Turbofan Engines
    
    Correction
    
        In rule document 00-24901, beginning on page 58645, in the issue of 
    Monday, October 2, 2000, make the following correction:
    
    
    Sec. 39.13  [Corrected]
    
        1.On page 58646, in the second column, under the heading  Initial 
    Inspection of Stage 2 LPT Nozzle Lock Assemblies, in paragraph (a), the 
    fourth line, ``information'' should read ``Information''.
        2. On page 58646, in the third column, under the heading  
    Repetitive Inspection of Stage 2 LPT Nozzle Lock Assemblies, in 
    paragraph (c), the fourth line, ``information'' should read `` 
    Information''.
    
        3. On page 58646, in the third column, in paragraph (d), the second 
    line, ``place'' should read ``replace''.
    [FR Doc. C0-24901 Filed 10-13-00; 8:45 am]
    BILLING CODE 1505-01-D
    
    
    

Document Information

Published:
10/16/2000
Department:
Federal Aviation Administration
Entry Type:
Correction
Document Number:
C0-24901
Pages:
61216-61216 (1 pages)
Docket Numbers:
Docket No. 2000-NE-38-AD, Amendment 39-11913, AD 2000-20-02
PDF File:
c0-24901.pdf
CFR: (1)
14 CFR 39.13