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]
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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
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Fmt 4700
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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