X97-40124. Airworthiness Directives; Boeing Model 737-100 and -200 Series Airplanes  

  • [Federal Register Volume 62, Number 16 (Friday, January 24, 1997)]
    [Corrections]
    [Page 3739]
    From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
    [FR Doc No: X97-40124]
    
    
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    DEPARTMENT OF TRANSPORTATION
    
    Federal Aviation Administration
    
    14 CFR Part 39
    
    [Docket No. 96-NM-145-AD; Amendment 39-9881; AD 97-01-10]
    
    
    Airworthiness Directives; Boeing Model 737-100 and -200 Series 
    Airplanes
    
    Correction
    
        In rule document 97-537 beginning on page 2007 in the issue of 
    Wednesday, January 15, 1997, make the following correction:
    
    
    Sec. 39.13   [Corrected]
    
        1. On page 2009, in the first column, in Sec. 39.13(a)(1), in the 
    fourth line, ``II'' should read ``I''.
        2. On the same page, in the same column, in the same section, in 
    the sixth line, after ``bulletin.'' add ``Or''.
        3. On the same page, in the same column, in the same section, 
    paragraph (2) was inadvertently omitted and should read as printed 
    below:
        ``(2) Rework the existing aileron control transfer mechanism, P/N 
    65-54200-4 or -5, in accordance with Procedure II of the Accomplishment 
    Instructions of the service bulletin.''
    
    BILLING CODE 1505-01-D
    
    
    

Document Information

Published:
01/24/1997
Department:
Federal Aviation Administration
Entry Type:
Correction
Document Number:
X97-40124
Pages:
3739-3739 (1 pages)
Docket Numbers:
Docket No. 96-NM-145-AD, Amendment 39-9881, AD 97-01-10
PDF File:
x97-40124.pdf
CFR: (1)
14 CFR 39.13