[Federal Register Volume 70, Number 96 (Thursday, May 19, 2005)]
[Corrections]
[Page 28988]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: C5-9186]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2005-21139; Directorate Identifier 2003-NM-196-AD]
RIN 2120-AA64


Airworthiness Directives; Bombardier Model CL600-1A11 (CL-600), 
Model CL-600-2A12 (CL-601), and Model CL-600-2B16 (CL-601-3A, CL-601-
3R, and CL-604) Series Airplanes

Correction

    In proposed rule document 05-9186 beginning on page 24331 in the 
issue of Monday, May 9, 2005, make the following corrections:
    1. On page 24332, in the table Messier-Dowty Service Bulletins, 
under the column Landing gear component, the seventh entry should read 
``MLG shock strut pin.''
    2. On the same page, in the same table, under the column 
Corresponding Bombardier service bulletin(s), the seventh entry should 
read ``601-0546.''


Sec. 39.13  [Corrected]

    3. On page 24334, in Sec. 39.13, in Table 2, under the column 
Messier-Dowty service bulletin, the last entry should read ``M-DT 
SB7300-32-16, dated July 12, 2001.''.
    4. On the same page, in the same section, in the same table, under 
the column Model, in the eighth entry remove the word ``retraction.''

[FR Doc. C5-9186 Filed 5-18-05; 8:45 am]
BILLING CODE 1505-01-D