Airworthiness Directives; Boeing Model 747-100, 747-100B, 747-100B SUD, 747-200B, 747-200C, 747-200F, 747-300, 747SR, and 747SP Series Airplanes, 57124-57125 [05-19564]

Download as PDF 57124 Federal Register / Vol. 70, No. 189 / Friday, September 30, 2005 / Rules and Regulations List of Subjects in 7 CFR Part 301 Agricultural commodities, Plant diseases and pests, Quarantine, Reporting and recordkeeping requirements, Transportation. PART 301—DOMESTIC QUARANTINE NOTICES Accordingly, we are adopting as a final rule, without change, the interim rules that amended 7 CFR part 301 and that were published at 68 FR 8817–8820 on February 26, 2003, and 68 FR 61323– 61324 on October 28, 2003. I Done in Washington, DC, this 26th day of September 2005. Elizabeth E. Gaston, Acting Administrator, Animal and Plant Health Inspection Service. [FR Doc. 05–19575 Filed 9–29–05; 8:45 am] BILLING CODE 3410–34–P DEPARTMENT OF COMMERCE Economic Development Administration 13 CFR Chapter III [Docket No.: 050729210–5250–02] RIN 0610–AA63 Economic Development Administration Reauthorization Act of 2004 Implementation; Regulatory Revision Economic Development Administration, Department of Commerce. ACTION: Final rule; delay of effective date of certain provisions and extension of public comment period. AGENCY: SUMMARY: On August 11, 2005, the Economic Development Administration (‘‘EDA’’) published an interim final rule in the Federal Register. This final rule delays the effective date of certain provisions in the interim final rule from October 1, 2005 until November 14, 2005. This final rule also extends the deadline for submitting public comments on the interim final rule from October 11, 2005 until November 14, 2005. The delay in effective date and the extension of the public comment period are necessary to provide additional time for the submission of public comments and to allow for EDA’s additional consideration of matters pertaining to the effective implementation of the interim final rule. Capitalized terms used but not otherwise defined in this final rule have the meanings ascribed to them in the interim final rule. DATES: The effective date of the following provisions of the interim final VerDate Aug<31>2005 15:28 Sep 29, 2005 Jkt 205001 rule is delayed from October 1, 2005 until November 14, 2005: (i) Section 304.2(c)(2), pertaining to membership of a District Organization’s governing body; and (ii) Section 301.4, as the provisions of this section relate to Investment Rates for EDA Planning Investments. The deadline for submitting public comments on the interim final rule is extended from 5 p.m. (e.s.t.) on October 11, 2005 until 5 p.m. (e.s.t.) on November 14, 2005. FOR FURTHER INFORMATION CONTACT: Office of Chief Counsel, Economic Development Administration, Department of Commerce, Room 7005, 1401 Constitution Avenue, NW., Washington DC 20230; telephone: (202) 482–4687. SUPPLEMENTARY INFORMATION: EDA published an interim final rule in the Federal Register (70 FR 47002) on August 11, 2005. The interim final rule reflects the amendments made to EDA’s authorizing statute, the Public Works and Economic Development Act of 1965 (42 U.S.C. 3121 et seq.) (‘‘PWEDA’’), by the Economic Development Reauthorization Act of 2004 (Pub. L. 108–373). In addition to tracking the statutory amendments to PWEDA, the interim final rule reflects EDA’s current practices and policies in administering its economic development programs that have evolved since the promulgation of EDA’s current regulations (codified at 13 CFR Chapter III). The interim final rule also provides for a public comment period. This final rule delays the effective date of the provisions specified above relating to EDA’s Planning Investments, Investment Rates for Planning Investments, and District Organizations from October 1, 2005 until November 14, 2005. The effective date of all other provisions of the interim final rule remains October 1, 2005. This final rule also extends the deadline for submitting public comments on the entire interim final rule from 5 p.m. (e.s.t.) on October 11, 2005 until 5 p.m. (e.s.t.) on November 14, 2005. The procedure for filing public comments is set forth in the interim final rule and is not changed by this final rule. The delay in effective date and the extension of the public comment period are necessary to provide additional time for the submission of public comments and to allow for EDA’s additional consideration of matters pertaining to the effective implementation of the interim final rule. Classification Prior notice and opportunity for public comment are not required for PO 00000 Frm 00004 Fmt 4700 Sfmt 4700 rules concerning public property, loans, grants, benefits, and contracts (5 U.S.C. 553(a)(2)). Because prior notice and an opportunity for public comment are not required pursuant to 5 U.S.C. 553 or any other law, the analytical requirements of the Regulatory Flexibility Act (5 U.S.C. 601 et seq.) are inapplicable. Therefore, a regulatory flexibility analysis has not been prepared. Executive Order No. 12866 It has been determined that this final rule is not significant for purposes of Executive Order 12866. Congressional Review Act This final rule is not ‘‘major’’ under the Congressional Review Act (5 U.S.C. 801 et seq.). Executive Order No. 13132 Executive Order 13132 requires agencies to develop an accountable process to ensure ‘‘meaningful and timely input by State and local officials in the development of regulatory policies that have federalism implications.’’ ‘‘Policies that have federalism implications’’ is defined in Executive Order 13132 to include regulations that have ‘‘substantial direct effects on the States, on the relationship between the national government and the States, or on the distribution of power and responsibilities among the various levels of government.’’ It has been determined that this final rule does not contain policies that have federalism implications. Dated: September 28, 2005. Benjamin Erulkar, Chief Counsel, Economic Development Administration. [FR Doc. 05–19705 Filed 9–29–05; 8:45 am] BILLING CODE 3510–24–P DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA–2005–22413; Directorate Identifier 2005–NM–167–AD; Amendment 39–14271; AD 2005–19–06] RIN 2120–AA64 Airworthiness Directives; Boeing Model 747–100, 747–100B, 747–100B SUD, 747–200B, 747–200C, 747–200F, 747–300, 747SR, and 747SP Series Airplanes Federal Aviation Administration (FAA), Department of Transportation (DOT). ACTION: Final rule; correction. AGENCY: E:\FR\FM\30SER1.SGM 30SER1 Federal Register / Vol. 70, No. 189 / Friday, September 30, 2005 / Rules and Regulations SUMMARY: The FAA is correcting a typographical error in an existing airworthiness directive (AD) that was published in the Federal Register on September 15, 2005 (70 FR 54474). The error resulted in an inadvertent reference to a nonexistent paragraph. This AD applies to certain Boeing Model 747–100, 747–100B, 747–100B SUD, 747–200B, 747–200C, 747–200F, 747–300, 747SR, and 747SP series airplanes. This AD requires repetitive detailed and ultrasonic inspections of the thrust links of the rear engine mounts for any crack or fracture and corrective actions if necessary. DATES: Effective September 30, 2005. ADDRESSES: The AD docket contains the proposed AD, comments, and any final disposition. You may examine the AD docket on the Internet at https:// 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–2005–22413; the directorate identifier for this docket is 2005–NM– 167–AD. FOR FURTHER INFORMATION CONTACT: Ivan Li, Aerospace Engineer, Airframe Branch, ANM–120S, FAA, Seattle Aircraft Certification Office, 1601 Lind Avenue, SW., Renton, Washington 98055–4056; telephone (425) 917–6437; fax (425) 917–6590. SUPPLEMENTARY INFORMATION: On September 6, 2005, the FAA issued AD 2005–19–06, amendment 39–14271 (70 FR 54474, September 15, 2005), for certain Boeing Model 747–100, 747– 100B, 747–100B SUD, 747–200B, 747– 200C, 747–200F, 747–300, 747SR, and 747SP series airplanes; equipped with Pratt & Whitney JT9D–3 and –7 series engines, except JT9D–70 engines. The AD requires repetitive detailed and ultrasonic inspections of the thrust links of the rear engine mounts for any crack or fracture and corrective actions if necessary. As published, the requirements of paragraph (h)(1) of the AD inadvertently reference doing the repetitive replacements ‘‘* * * at the applicable compliance time specified in paragraph (h)(1)(i) or (h)(2)(ii) of this AD.’’ However, there is no paragraph (h)(2)(ii) in the AD. We have removed reference to paragraph (h)(2)(ii) and replaced it with the correct reference to paragraph (h)(1)(ii). VerDate Aug<31>2005 15:28 Sep 29, 2005 Jkt 205001 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 30, 2005. § 39.13 [Corrected] In the Federal Register of September 15, 2005, on page 54476, in the third column, paragraph (h)(1) of AD 2005– 19–06 is corrected to read as follows: * * * * * (1) Replace the cracked thrust link with a new or overhauled thrust link in accordance with Part 2 of the service bulletin; except as provided by paragraph (i) of this AD. Repeat the replacement at the applicable compliance time specified in paragraph (h)(1)(i) or (h)(1)(ii) of this AD. * * * * * I Issued in Renton, Washington, on September 26, 2005. Ali Bahrami, Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. 05–19564 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–2005–22405; Directorate Identifier 2002–NM–243–AD; Amendment 39–14269; AD 2005–19–04] RIN 2120–AA64 Airworthiness Directives; Airbus Model A340–200 and –300 Series 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 54251). The error resulted in in an incorrect Docket No. This AD applies to certain Airbus Model A340–200 and –300 series airplanes. This AD requires revising the airplane flight manual to incorporate new procedures for the flightcrew to follow to correct miscalculation of the takeoff and accelerating or stopping distance of the airplane during a ferry flight under certain conditions. DATES: Effective September 29, 2005. ADDRESSES: The AD docket contains the proposed AD, comments, and any final PO 00000 Frm 00005 Fmt 4700 Sfmt 4700 57125 disposition. You may examine the AD docket on the Internet at https:// 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–2005–22405; the directorate identifier for this docket is 2002–NM– 243–AD. Dan Rodina, Aerospace Engineer, International Branch, ANM–116, FAA, Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton, Washington 98055–4056; telephone (425) 227–2125; fax (425) 227–1149. FOR FURTHER INFORMATION CONTACT: On September 6, 2005, the FAA issued AD 2005–19–04, amendment 39–14269 (70 FR 54251, September 14, 2005), for certain Airbus Model A340–200 and –300 series airplanes. The AD requires revising the airplane flight manual to incorporate new procedures for the flightcrew to follow to correct miscalculation of the takeoff and accelerating or stopping distance of the airplane during a ferry flight under certain conditions. As published, that AD specifies an incorrect Docket No. (i.e., FAA–2005– 20405) throughout preamble and the regulatory text of the AD. The correct Docket No. is FAA–2005–22405. 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. SUPPLEMENTARY INFORMATION: § 39.13 [Corrected] I In the Federal Register of September 14, 2005, on page 54253, in the first column, paragraph 2. of PART 39— AIRWORTHINESS DIRECTIVES of AD 2005–19–04 is corrected to read as follows: * * * * * 2005–19–04 Airbus: Amendment 39–14269. Docket No. FAA–2005–22405; Directorate Identifier 2002–NM–243–AD. * * * * * Issued in Renton, Washington, on September 26, 2005. Ali Bahrami, Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. 05–19556 Filed 9–29–05; 8:45 am] BILLING CODE 4910–13–P E:\FR\FM\30SER1.SGM 30SER1

Agencies

[Federal Register Volume 70, Number 189 (Friday, September 30, 2005)]
[Rules and Regulations]
[Pages 57124-57125]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: 05-19564]


=======================================================================
-----------------------------------------------------------------------

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2005-22413; Directorate Identifier 2005-NM-167-AD; 
Amendment 39-14271; AD 2005-19-06]
RIN 2120-AA64


Airworthiness Directives; Boeing Model 747-100, 747-100B, 747-
100B SUD, 747-200B, 747-200C, 747-200F, 747-300, 747SR, and 747SP 
Series Airplanes

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

ACTION: Final rule; correction.

-----------------------------------------------------------------------

[[Page 57125]]

SUMMARY: The FAA is correcting a typographical error in an existing 
airworthiness directive (AD) that was published in the Federal Register 
on September 15, 2005 (70 FR 54474). The error resulted in an 
inadvertent reference to a nonexistent paragraph. This AD applies to 
certain Boeing Model 747-100, 747-100B, 747-100B SUD, 747-200B, 747-
200C, 747-200F, 747-300, 747SR, and 747SP series airplanes. This AD 
requires repetitive detailed and ultrasonic inspections of the thrust 
links of the rear engine mounts for any crack or fracture and 
corrective actions if necessary.

DATES: Effective September 30, 2005.

ADDRESSES: The AD docket contains the proposed AD, comments, and any 
final disposition. You may examine the AD docket on the Internet at 
https://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-2005-22413; the directorate 
identifier for this docket is 2005-NM-167-AD.

FOR FURTHER INFORMATION CONTACT: Ivan Li, Aerospace Engineer, Airframe 
Branch, ANM-120S, FAA, Seattle Aircraft Certification Office, 1601 Lind 
Avenue, SW., Renton, Washington 98055-4056; telephone (425) 917-6437; 
fax (425) 917-6590.

SUPPLEMENTARY INFORMATION: On September 6, 2005, the FAA issued AD 
2005-19-06, amendment 39-14271 (70 FR 54474, September 15, 2005), for 
certain Boeing Model 747-100, 747-100B, 747-100B SUD, 747-200B, 747-
200C, 747-200F, 747-300, 747SR, and 747SP series airplanes; equipped 
with Pratt & Whitney JT9D-3 and -7 series engines, except JT9D-70 
engines. The AD requires repetitive detailed and ultrasonic inspections 
of the thrust links of the rear engine mounts for any crack or fracture 
and corrective actions if necessary.
    As published, the requirements of paragraph (h)(1) of the AD 
inadvertently reference doing the repetitive replacements ``* * * at 
the applicable compliance time specified in paragraph (h)(1)(i) or 
(h)(2)(ii) of this AD.'' However, there is no paragraph (h)(2)(ii) in 
the AD. We have removed reference to paragraph (h)(2)(ii) and replaced 
it with the correct reference to paragraph (h)(1)(ii).
    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 30, 2005.


Sec.  39.13  [Corrected]

0
In the Federal Register of September 15, 2005, on page 54476, in the 
third column, paragraph (h)(1) of AD 2005-19-06 is corrected to read as 
follows:
* * * * *
    (1) Replace the cracked thrust link with a new or overhauled thrust 
link in accordance with Part 2 of the service bulletin; except as 
provided by paragraph (i) of this AD. Repeat the replacement at the 
applicable compliance time specified in paragraph (h)(1)(i) or 
(h)(1)(ii) of this AD.
* * * * *

    Issued in Renton, Washington, on September 26, 2005.
Ali Bahrami,
Manager, Transport Airplane Directorate, Aircraft Certification 
Service.
[FR Doc. 05-19564 Filed 9-29-05; 8:45 am]
BILLING CODE 4910-13-P

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