[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