[Federal Register Volume 70, Number 189 (Friday, September 30, 2005)]
[Rules and Regulations]
[Pages 57126-57127]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 05-19554]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2005-22404; Directorate Identifier 2005-NM-018-AD; 
Amendment 39-14268; AD 2005-19-03]
RIN 2120-AA64


Airworthiness Directives; BAe Systems (Operations) Limited Model 
ATP Airplanes

AGENCY: Federal Aviation Administration (FAA), Department of 
Transportation (DOT).

ACTION: Final rule; correction.

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SUMMARY: The FAA is correcting a typographical error in an existing 
airworthiness directive (AD) that was published in the Federal Register 
on September 13, 2005 (70 FR 53915). The error resulted in an incorrect 
Docket No. This AD applies to all BAe Systems (Operations) Limited 
Model ATP airplanes. This AD requires revising the Airworthiness 
Limitations Section of the Instructions for Continued Airworthiness to 
incorporate life limits for certain items and new inspections to detect 
fatigue cracking in certain structures and of certain significant 
structural items, and to revise life limits for certain equipment and 
various components.

DATES: Effective September 28, 2005.

ADDRESSES: The AD docket contains the proposed AD, comments, and any 
final disposition. You may examine the AD docket on the Internet at 
http://dms.dot.gov, or in person at the Docket Management Facility 
office between 9 a.m. and 5 p.m., Monday through Friday, except Federal 
holidays. The Docket Management Facility office (telephone (800) 647-
5227) is located on the plaza level of the Nassif Building at the U.S. 
Department of Transportation, 400 Seventh Street, SW., room PL-401, 
Washington, DC. This docket number is FAA-2005-22404; the directorate 
identifier for this docket is 2005-NM-018-AD.

FOR FURTHER INFORMATION CONTACT: Todd Thompson, Aerospace Engineer, 
International Branch, ANM-116, FAA, Transport Airplane Directorate, 
1601 Lind Avenue, SW., Renton, Washington 98055-4056; telephone (425) 
227-1175; fax (425) 227-1149.

SUPPLEMENTARY INFORMATION: On September 6, 2005, the FAA issued AD 
2005-19-03, amendment 39-14268 (70 FR 53915, September 13, 2005), for 
all BAe Systems (Operations) Limited Model ATP airplanes. The AD 
requires revising the Airworthiness Limitations Section of the 
Instructions for Continued Airworthiness to incorporate life limits for 
certain items and new inspections to detect fatigue cracking in certain 
structures and of certain significant structural items, and to revise 
life limits for certain equipment and various components.
    As published, that AD specifies an incorrect Docket No. (i.e., FAA-
2005-20404) throughout preamble and the regulatory text of the AD. The 
correct Docket No. is FAA-2005-22404.
    No other part of the regulatory information has been changed; 
therefore, the final rule is not republished in the Federal Register.
    The effective date of this AD remains September 28, 2005.


Sec.  39.13  [Corrected]

0
In the Federal Register of September 13, 2005, on page 53916, in the 
third column, paragraph 2. of PART 39--AIRWORTHINESS DIRECTIVES of AD 
2005-19-03 is corrected to read as follows:
* * * * *
2005-19-03 BAe Systems (Operations) Limited (Formerly British 
Aerospace Regional Aircraft): Amendment 39-14268. Docket No. FAA-
2005-22404; Directorate Identifier 2005-NM-018-AD.
* * * * *


[[Page 57127]]


    Issued in Renton, Washington, on September 26, 2005.
Ali Bahrami,
Manager, Transport Airplane Directorate, Aircraft Certification 
Service.
[FR Doc. 05-19554 Filed 9-29-05; 8:45 am]
BILLING CODE 4910-13-P