Airworthiness Directives; Aerospatiale Model ATR42-500 Airplanes, 57126 [05-19555]

Download as PDF 57126 Federal Register / Vol. 70, No. 189 / Friday, September 30, 2005 / Rules and Regulations DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA–2005–22406; Directorate Identifier 2002–NM–242–AD; Amendment 39–14270; AD 2005–19–05] RIN 2120–AA64 Airworthiness Directives; Aerospatiale Model ATR42–500 Airplanes Federal Aviation Administration (FAA), Department of Transportation (DOT). ACTION: Final rule; correction. AGENCY: SUMMARY: The FAA is correcting a typographical error in an existing airworthiness directive (AD) that was published in the Federal Register on September 14, 2005 (70 FR 54249). The error resulted in an incorrect Docket No. This AD applies to certain Aerospatiale Model ATR42–500 airplanes. This AD requires inspecting for correct installation of the fastener that attaches the ground braids on the elevator, modifying the forward bonded assembly of the elevator control rod, and corrective action if necessary. DATES: Effective September 29, 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–2005–22406; the directorate identifier for this docket is 2002–NM– 242–AD. FOR FURTHER INFORMATION CONTACT: Dan Rodina, Aerospace Engineer, International Branch, ANM–116, Transport Airplane Directorate, FAA, 1601 Lind Avenue, SW., Renton, Washington 98055–4056; telephone (425) 227–2125; fax (425) 227–1149. SUPPLEMENTARY INFORMATION: On September 6, 2005, the FAA issued AD 2005–19–05, amendment 39–14270 (70 FR 54249, September 14, 2005), for certain Aerospatiale Model ATR42–500 airplanes. This AD requires inspecting for correct installation of the fastener that attaches the ground braids on the elevator, modifying the forward bonded assembly of the elevator control rod, and corrective action if necessary. VerDate Aug<31>2005 15:28 Sep 29, 2005 Jkt 205001 As published, that AD specifies an incorrect Docket No. (i.e., FAA–2005– 20406) throughout preamble and the regulatory text of the AD. The correct Docket No. is FAA–2005–22406. 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 29, 2005. § 39.13 [Corrected] I In the Federal Register of September 14, 2005, on page 54250, in the third column, paragraph 2. of PART 39— AIRWORTHINESS DIRECTIVES of AD 2005–19–05 is corrected to read as follows: * * * * * 2005–19–05 Aerospatiale: Amendment 39– 14270. Docket No. FAA–2005–22406; Directorate Identifier 2002–NM–242–AD. * * * * * Issued in Renton, Washington, on September 26, 2005. Ali Bahrami, Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. 05–19555 Filed 9–29–05; 8:45 am] BILLING CODE 4910–13–P 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 Federal Aviation Administration (FAA), Department of Transportation (DOT). ACTION: Final rule; correction. AGENCY: 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 PO 00000 Frm 00006 Fmt 4700 Sfmt 4700 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. § 39.13 [Corrected] I 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. * E:\FR\FM\30SER1.SGM * * 30SER1 * *

Agencies

[Federal Register Volume 70, Number 189 (Friday, September 30, 2005)]
[Rules and Regulations]
[Page 57126]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: 05-19555]



[[Page 57126]]

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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2005-22406; Directorate Identifier 2002-NM-242-AD; 
Amendment 39-14270; AD 2005-19-05]
RIN 2120-AA64


Airworthiness Directives; Aerospatiale Model ATR42-500 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 14, 2005 (70 FR 54249). The error resulted in an incorrect 
Docket No. This AD applies to certain Aerospatiale Model ATR42-500 
airplanes. This AD requires inspecting for correct installation of the 
fastener that attaches the ground braids on the elevator, modifying the 
forward bonded assembly of the elevator control rod, and corrective 
action if necessary.

DATES: Effective September 29, 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-2005-22406; the directorate 
identifier for this docket is 2002-NM-242-AD.

FOR FURTHER INFORMATION CONTACT: Dan Rodina, Aerospace Engineer, 
International Branch, ANM-116, Transport Airplane Directorate, FAA, 
1601 Lind Avenue, SW., Renton, Washington 98055-4056; telephone (425) 
227-2125; fax (425) 227-1149.

SUPPLEMENTARY INFORMATION: On September 6, 2005, the FAA issued AD 
2005-19-05, amendment 39-14270 (70 FR 54249, September 14, 2005), for 
certain Aerospatiale Model ATR42-500 airplanes. This AD requires 
inspecting for correct installation of the fastener that attaches the 
ground braids on the elevator, modifying the forward bonded assembly of 
the elevator control rod, and corrective action if necessary.
    As published, that AD specifies an incorrect Docket No. (i.e., FAA-
2005-20406) throughout preamble and the regulatory text of the AD. The 
correct Docket No. is FAA-2005-22406.
    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 29, 2005.


Sec.  39.13  [Corrected]

0
In the Federal Register of September 14, 2005, on page 54250, in the 
third column, paragraph 2. of PART 39--AIRWORTHINESS DIRECTIVES of AD 
2005-19-05 is corrected to read as follows:
* * * * *
2005-19-05 Aerospatiale: Amendment 39-14270. Docket No. FAA-2005-
22406; Directorate Identifier 2002-NM-242-AD.
* * * * *

    Issued in Renton, Washington, on September 26, 2005.
Ali Bahrami,
Manager, Transport Airplane Directorate, Aircraft Certification 
Service.
[FR Doc. 05-19555 Filed 9-29-05; 8:45 am]
BILLING CODE 4910-13-P