Airworthiness Directives; General Electric Company (GE) CF6-80A1/A3 and CF6-80C2A Series Turbofan Engines, Installed on Airbus Industrie A300-600 and A310 Series Airplanes; Correction, 23783-23784 [05-8883]

Download as PDF Federal Register / Vol. 70, No. 86 / Thursday, May 5, 2005 / Rules and Regulations editions of Form I–129 until May 30, 2005. In addition, by increasing the number of Forms I–129 and Forms I– 907 being submitted as a result of the OAA, USCIS has submitted to OMB for emergency clearance the Paperwork Reduction Change Worksheet (OMB– 83C) increasing the total annual burden hours. Further, USCIS has submitted to OMB for emergency clearance Paperwork Reduction Act Submission (OMB 83–I) to permit USCIS to concurrent use of the Form I–129 (edition date 3–17–05, OMB 1615–0009 and the old Form I–129 (edition date 12–10–01, OMB 1115–0168, OMB 1615– 0093) until May 30, 2005. Due to this temporary information collection, USCIS submitted the OMB 83–I to formally request that OMB adjust the burden hours for the use of the 12–10– 01 version of the Form I–129. The public should reference the Federal Register notice contained at 70 FR 20590 (Apr. 20, 2005) for information about this collection. Please note however that USCIS hereby extends the deadline for comments solicited in that notice until May 30, 2005. (2) * * * (i) * * * (A) General. A United States employer seeking to classify an alien as an H–1B, H–2A, H–2B, or H–3, temporary employee shall file a petition on Form I–129, Petition for Nonimmigrant Worker, only with the USCIS Service Center which has jurisdiction in the area where the alien will perform services, or receive training, even in emergent situations, except as provided in this section or as specifically designated by USCIS via notice in the Federal Register. * * * * * (8) * * * (ii) * * * (B) When calculating the numerical limitations for a given fiscal year, USCIS will make numbers available to petitions in the order in which the petitions are filed. USCIS will make projections of the number of petitions necessary to achieve the numerical limit of approvals, taking into account historical data related to approvals, denials, revocations, and other relevant List of Subjects in 8 CFR Part 214 factors. USCIS will monitor the number Administrative practice and of petitions (including the number of procedure, Aliens, Employment, beneficiaries requested when necessary) Foreign officials, Health professions, received and will notify the public of Reporting and recordkeeping the date that USCIS has received the requirements, Students. necessary number of petitions (the I Accordingly, chapter I of title 8 of the ‘‘final receipt date’’). The date of Code of Federal Regulations is amended publication will not control the final as follows: receipt date. When necessary to ensure PART 214—NONIMMIGRANT CLASSES the fair and orderly allocation of numbers in a particular classification I 1. The authority citation for part 214 is subject to numerical limits, USCIS may revised to read as follows: randomly select from among the Authority: 8 U.S.C. 1101, 1102, 1103, 1182, petitions received on the final receipt date the remaining number of petitions 1184, 1185 (pursuant to E.O. 13323, 69 FR deemed necessary to generate the 241, 3 CFR, 2003 Comp., p. 278), 1186a, 1187, 1221, 1281, 1282, 1301–1305, 1372, numerical limit of approvals. This 1379, 1731–32; section 643, Pub. L. 104–208, random selection will be made via 110 Stat. 3009–708; section 141 of the computer-generated selection as Compacts of Free Association with the validated by the Office of Immigration Federated States of Micronesia and the Statistics. Petitions not randomly Republic of the Marshall Islands, and with selected, and petitions received after the the Government of Palau, 48 U.S.C. 1901 final receipt date, will be rejected. If the note, and 1931 note, respectively, 8 CFR part final receipt date is the same as the first 2. date on which petitions subject to the I 2. Section 214.2 is amended by applicable cap may be filed (i.e., if the I (a) Revising (h)(2)(i)(A); cap is reached on the first day filings I (b) Revising (h)(8)(ii)(B); can be made), USCIS will randomly I (c) Removing (h)(8)(ii)(C) and apply all of the numbers among the redesignating (h)(8)(ii)(D) through (F) petitions filed on the final receipt date respectively as (h)(8)(ii)(C) through (E); and the following day. I (d) Revising the last sentence of newly designated (h)(8)(ii)(C) to read as follows: (C) * * * The petition shall be revoked pursuant to paragraph § 214.2 Special requirements for (h)(11)(ii) of this section and USCIS will admission, extension, and maintenance of take into account the unused number status. during the appropriate fiscal year. * * * * * * * * * * (h) * * * VerDate jul<14>2003 14:24 May 04, 2005 Jkt 205001 PO 00000 Frm 00009 Fmt 4700 Sfmt 4700 23783 Dated: May 2, 2005. Michael Chertoff, Secretary. [FR Doc. 05–8992 Filed 5–2–05; 3:58 pm] BILLING CODE 4410–10–P DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 99–NE–41–AD; Amendment 39– 14015; AD 2005–06–07] RIN 2120–AA64 Airworthiness Directives; General Electric Company (GE) CF6–80A1/A3 and CF6–80C2A Series Turbofan Engines, Installed on Airbus Industrie A300–600 and A310 Series Airplanes; Correction Federal Aviation Administration, DOT. AGENCY: ACTION: Final rule; correction SUMMARY: This document makes a correction to Airworthiness Directive (AD) 2005–06–07. That AD applies to GE CF6–80A1/A3 and CF6–80C2A series turbofan engines. We published AD 2005–06–07 in the Federal Register on March 21, 2005, (70 FR 13365). A service bulletin number in the compliance section is incorrect. This document corrects that service bulletin number. In all other respects, the original document remains the same. EFFECTIVE DATE: Effective May 5, 2005. FOR FURTHER INFORMATION CONTACT: Karen Curtis, Aerospace Engineer, Engine Certification Office, FAA, Engine and Propeller Directorate, 12 New England Executive Park, Burlington, MA 01803–5299; telephone (781) 238–7192; fax (781) 238–7199. A final rule AD, FR Doc. 05–5299, that applies to GE CF6–80A1/A3 and CF6–80C2A series turbofan engines, was published in the Federal Register on March 21, 2005, (70 FR 13365). The following correction is needed: SUPPLEMENTARY INFORMATION: PART 39—[CORRECTED] § 39.13 [Corrected] On page 13368, in the first column, in compliance section paragraph (i)(2), in the sixth line, ‘‘No. CF6–80C2A SB 78A4022, Revision 2,’’ is corrected to read ‘‘No. CF6–80C2A SB 78A1081, Revision 2’’. I E:\FR\FM\05MYR1.SGM 05MYR1 23784 Federal Register / Vol. 70, No. 86 / Thursday, May 5, 2005 / Rules and Regulations Issued in Burlington, MA, on April 26, 2005. Jay J. Pardee, Manager, Engine and Propeller Directorate, Aircraft Certification Service. [FR Doc. 05–8883 Filed 5–4–05; 8:45 am] BILLING CODE 4910–13–P DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA–2005–21029; Directorate Identifier 2005–NM–045–AD; Amendment 39–14077; AD 2005–09–08] RIN 2120–AA64 Airworthiness Directives; McDonnell Douglas Model MD–90–30 Airplanes Federal Aviation Administration (FAA), Department of Transportation (DOT). ACTION: Final rule; request for comments. AGENCY: SUMMARY: The FAA is superseding two existing airworthiness directives (ADs); both apply to the same certain McDonnell Douglas Model MD–90–30 airplanes. The superseded ADs currently require a one-time general visual inspection to detect wire chafing damage and to determine adequate clearance between the disconnect panel structure and the wires above the aft left lavatory; and corrective actions, if necessary. This new AD retains those requirements and clarifies certain requirements for recording AD compliance. This AD is prompted by the determination that the form of the existing ADs could result in confusion to operators in recording compliance with the potentially conflicting requirements. We are issuing this AD to prevent damage to certain wires due to contact between the wires and the adjacent structure, which could result in electrical arcing and consequent smoke and fire in the cabin. DATES: Effective May 20, 2005. The incorporation by reference of Boeing Alert Service Bulletin MD90– 24A074, excluding Appendix, Revision 02, dated June 3, 2003, as listed in the regulations, was approved previously by the Director of the Federal Register as of February 22, 2005 (70 FR 5920, February 4, 2005). We must receive comments on this AD by July 5, 2005. VerDate jul<14>2003 14:24 May 04, 2005 Jkt 205001 Use one of the following addresses to submit comments on this AD. • DOT Docket Web site: Go to https://dms.dot.gov and follow the instructions for sending your comments electronically. • Government-wide rulemaking Web site: Go to https://www.regulations.gov and follow the instructions for sending your comments electronically. • Mail: Docket Management Facility; U.S. Department of Transportation, 400 Seventh Street SW., Nassif Building, Room PL–401, Washington, DC 20590. • Fax: (202) 493–2251. • Hand Delivery: Room PL–401 on the plaza level of the Nassif Building, 400 Seventh Street SW., Washington, DC, between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. • For service information identified in this AD, contact Boeing Commercial Airplanes, Long Beach Division, 3855 Lakewood Boulevard, Long Beach, California 90846; Attention: Data and Service Management, Dept. C1–L5A (D800–0024). You can examine the contents of this AD docket on the Internet at https:// dms.dot.gov, or in person at the Docket Management Facility, U.S. Department of Transportation, 400 Seventh Street SW., room PL–401, on the plaza level of the Nassif Building, Washington, DC. This docket number is FAA–2005– 21029; the directorate identifier for this docket is 2005–NM–045–AD. ADDRESSES: Examining the Docket You can 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 DOT street address stated in the ADDRESSES section. Comments will be available in the AD docket shortly after the DMS receives them. FOR FURTHER INFORMATION CONTACT: George Y. Mabuni, Senior Aerospace Engineer, Systems and Equipment Branch, ANM–130L, FAA, Los Angeles Aircraft Certification Office, 3960 Paramount Boulevard, Lakewood, California 90712–4137; telephone (562) 627–5341; fax (562) 627–5210. SUPPLEMENTARY INFORMATION: On February 14, 2003, we issued AD 2003– 04–10, amendment 39–13058 (68 FR 9513, February 28, 2003). On January PO 00000 Frm 00010 Fmt 4700 Sfmt 4700 26, 2005, we issued AD 2005–03–05, amendment 39–13961 (70 FR 5920, February 4, 2005). Both ADs apply to the same certain McDonnell Douglas MD–90–30 airplanes. Both require a one-time general visual inspection to detect wire chafing damage and to determine adequate clearance between the disconnect panel structure and the wires above the aft left lavatory; and corrective actions, if necessary. The actions specified in the ADs are intended to prevent damage to certain wires due to contact between the wires and the adjacent structure, which could result in electrical arcing and consequent smoke and fire in the cabin. Actions Since ADs Were Issued Since we issued those ADs, we discovered some procedural regulatory complications that could prevent operators from complying with either AD. We had initially determined that AD 2003–04–10 should be revised when in fact it should have been superseded. Although a revised AD is identified by adding ‘‘R1’’ to the original AD number, in this case the ‘‘revised’’ AD was instead given a new AD number (AD 2005–03–05). As a result, two essentially identical ADs apply to the same airplanes. We have determined that superseding both AD 2003–04–10 and AD 2005–03–05 will eliminate the confusion associated with recording compliance with potentially conflicting requirements in the two ADs. FAA’s Determination and Requirements of This AD The unsafe condition described previously is likely to exist or develop on other airplanes of the same type design. This AD is being issued to supersede AD 2003–04–10 and AD 2005–03–05. This new AD retains the requirements of the existing AD. Costs of Compliance The requirements of this new AD are unchanged from those of AD 2003–04– 10 and AD 2005–03–05; therefore, this AD imposes no additional economic burden on operators. The estimated costs associated with this AD are repeated for the convenience of affected operators, as follows: There are about 89 airplanes of the affected design worldwide. The following table provides the estimated costs for U.S. operators to comply with this AD. E:\FR\FM\05MYR1.SGM 05MYR1

Agencies

[Federal Register Volume 70, Number 86 (Thursday, May 5, 2005)]
[Rules and Regulations]
[Pages 23783-23784]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: 05-8883]


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

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. 99-NE-41-AD; Amendment 39-14015; AD 2005-06-07]
RIN 2120-AA64


Airworthiness Directives; General Electric Company (GE) CF6-80A1/
A3 and CF6-80C2A Series Turbofan Engines, Installed on Airbus Industrie 
A300-600 and A310 Series Airplanes; Correction

AGENCY: Federal Aviation Administration, DOT.

ACTION: Final rule; correction

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

SUMMARY: This document makes a correction to Airworthiness Directive 
(AD) 2005-06-07. That AD applies to GE CF6-80A1/A3 and CF6-80C2A series 
turbofan engines. We published AD 2005-06-07 in the Federal Register on 
March 21, 2005, (70 FR 13365). A service bulletin number in the 
compliance section is incorrect. This document corrects that service 
bulletin number. In all other respects, the original document remains 
the same.

EFFECTIVE DATE: Effective May 5, 2005.

FOR FURTHER INFORMATION CONTACT: Karen Curtis, Aerospace Engineer, 
Engine Certification Office, FAA, Engine and Propeller Directorate, 12 
New England Executive Park, Burlington, MA 01803-5299; telephone (781) 
238-7192; fax (781) 238-7199.

SUPPLEMENTARY INFORMATION: A final rule AD, FR Doc. 05-5299, that 
applies to GE CF6-80A1/A3 and CF6-80C2A series turbofan engines, was 
published in the Federal Register on March 21, 2005, (70 FR 13365). The 
following correction is needed:

PART 39--[CORRECTED]


Sec.  39.13  [Corrected]

0
On page 13368, in the first column, in compliance section paragraph 
(i)(2), in the sixth line, ``No. CF6-80C2A SB 78A4022, Revision 2,'' is 
corrected to read ``No. CF6-80C2A SB 78A1081, Revision 2''.


[[Page 23784]]


    Issued in Burlington, MA, on April 26, 2005.
Jay J. Pardee,
Manager, Engine and Propeller Directorate, Aircraft Certification 
Service.
[FR Doc. 05-8883 Filed 5-4-05; 8:45 am]
BILLING CODE 4910-13-P
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