[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