Airworthiness Directives; Boeing Model 737-100, -200, -200C, -300, -400, and -500 Series Airplanes, 46559 [E7-16304]
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Federal Register / Vol. 72, No. 161 / Tuesday, August 21, 2007 / Rules and Regulations
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2007–28253; Directorate
Identifier 2007–NM–031–AD; Amendment
39–15064; AD 2007–11–07]
RIN 2120–AA64
Airworthiness Directives; Boeing
Model 737–100, –200, –200C, –300,
–400, and –500 Series Airplanes
Federal Aviation
Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule; correction.
rmajette on PROD1PC64 with RULES
AGENCY:
SUMMARY: The FAA is correcting a
typographical error in an existing
airworthiness directive (AD) that was
published in the Federal Register on
May 22, 2007 (72 FR 28597). The error
resulted in a confusing compliance
time. This AD applies to all Boeing
Model 737–100, –200, –200C, –300,
–400, and –500 series airplanes. This
AD requires repetitive detailed
inspections for damage of the electrical
wire and sleeve that run to the fuel
boost pump through a conduit in the
fuel tank, and arcing damage of the
conduit and signs of fuel leakage into
the conduit; replacement of the sleeve
with a new, smaller-diameter sleeve;
and related investigative and corrective
actions, as applicable.
DATES: Effective June 6, 2007.
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
Operations office between 9 a.m. and 5
p.m., Monday through Friday, except
Federal holidays. The Docket
Operations office (telephone (800) 647–
5527) is located on the ground level of
the West Building at the DOT street
address stated in the ADDRESSES section.
This docket number is FAA–2007–
28253; the directorate identifier for this
docket is 2007–NM–031–AD.
FOR FURTHER INFORMATION CONTACT:
Suzanne Lucier, Aerospace Engineer,
Propulsion Branch, ANM–140S, FAA,
Seattle Aircraft Certification Office,
1601 Lind Avenue, SW., Renton,
Washington 98057–3356; telephone
(425) 917–6438; fax (425) 917–6590.
SUPPLEMENTARY INFORMATION: On May 2,
2007, the FAA issued AD 2007–11–07,
amendment 39–15064 (72 FR 28597,
May 22, 2007), for all Boeing Model
737–100, –200, –200C, –300, –400, and
–500 series airplanes. The AD requires
repetitive detailed inspections for
VerDate Aug<31>2005
15:05 Aug 20, 2007
Jkt 211001
damage of the electrical wire and sleeve
that run to the fuel boost pump through
a conduit in the fuel tank, and arcing
damage of the conduit and signs of fuel
leakage into the conduit; replacement of
the sleeve with a new, smaller-diameter
sleeve; and related investigative and
corrective actions, as applicable.
As published, paragraph (k) of AD
2007–11–07 reads ‘‘* * * Thereafter,
repeat the detailed inspection at
intervals not to exceed 15,000 flight
cycles. * * *’’ The correct term, ‘‘flight
hours’’ (not flight cycles), appears in all
other compliance times cited in the AD,
as intended.
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
June 6, 2007.
§ 39.13
[Corrected]
In the Federal Register of May 22,
2007, on page 28600, in the third
column, paragraph (k) of AD 2007–11–
07 is corrected to read as follows:
*
*
*
*
*
I
(k) At the applicable time specified by
paragraph (k)(1) or (k)(2) of this AD: Do a
detailed inspection for damage of the sleeve
and electrical wire of the fuel boost pump;
and, before further flight, install a new,
smaller-diameter sleeve, and do related
investigative and corrective actions, as
applicable; in accordance with the
Accomplishment Instructions of Boeing Alert
Service Bulletin 737–28A1263, Revision 1,
dated March 19, 2007. Thereafter, repeat the
detailed inspection at intervals not to exceed
15,000 flight hours. Accomplishment of the
initial inspection, applicable corrective
actions, and sleeve installation required by
this paragraph terminates the requirements of
paragraphs (f), (g), (h), and (i) of this AD.
*
*
*
*
*
Issued in Renton, Washington, on August
14, 2007.
Stephen P. Boyd,
Acting Manager, Transport Airplane
Directorate, Aircraft Certification Service.
[FR Doc. E7–16304 Filed 8–20–07; 8:45 am]
BILLING CODE 4910–13–P
SECURITIES AND EXCHANGE
COMMISSION
17 CFR Part 232
[Release Nos. 33–8834; 34–56256; 39–2448;
IC–27928]
RIN 3235–AG96
Adoption of Updated EDGAR Filer
Manual
Securities and Exchange
Commission.
AGENCY:
PO 00000
Frm 00021
Fmt 4700
Sfmt 4700
ACTION:
46559
Final rule.
SUMMARY: The Securities and Exchange
Commission (the Commission) is
adopting revisions to the Electronic Data
Gathering, Analysis, and Retrieval
System (EDGAR) Filer Manual to reflect
updates to the EDGAR system.
Revisions are being made primarily to
support the expansion of the current
interactive data voluntary reporting
program to enable mutual funds
voluntarily to submit supplemental
tagged information contained in the
risk/return summary section of their
prospectuses on Form N–1A. The
EDGAR system is being upgraded to
support this functionality on August 20,
2007.
The filer manual is also being revised
to incorporate changes in support of
several final rules previously adopted
by the Commission and implemented in
EDGAR. Those rules include the
termination of a foreign private issuer’s
registration of a class of securities under
Section 12(g) and duty to file reports
under Section 13(a) or 15(d) of the
Securities Exchange Act of 1934
(‘‘Exchange Act’’); the electronic filing
of Transfer Agent (‘‘TA’’) forms TA–1,
TA–2 and TA–W; and revisions to the
accelerated filer definition under the
Exchange Act. Other revisions were
made to allow an issuer to indicate
whether it is subject to reporting
obligations after terminating registration
of a class of equity securities under the
Exchange Act and to remove references
to submission types N–14AE and N–
14AE/A for the filing of Form N–14
from ‘‘Table 3–5: Investment Company
Submission Types Accepted by
EDGAR’’ of the Filer Manual.
Revisions to the Filer Manual reflect
changes within Volumes I and II,
entitled EDGAR Filer Manual, Volume I:
‘‘General Information,’’ Version 4
(August 2007) and EDGAR Filer
Manual, Volume II: ‘‘EDGAR Filing,’’
Version 5 (August 2007) respectively.
The updated manual will be
incorporated by reference into the Code
of Federal Regulations.
DATES: Effective Date: August 20, 2007.
The incorporation by reference of the
EDGAR Filer Manual is approved by the
Director of the Federal Register as of
August 20, 2007.
FOR FURTHER INFORMATION CONTACT: In
the Office of Information Technology,
Rick Heroux, at (202) 551–8800; in the
Division of Investment Management, for
questions concerning the expansion of
the current interactive data voluntary
reporting program, Alberto H. Zapata,
Senior Counsel, or Brent J. Fields,
Assistant Director, Office of Disclosure
Regulation, at (202) 551–6784, and for
E:\FR\FM\21AUR1.SGM
21AUR1
]]>Agencies
[Federal Register Volume 72, Number 161 (Tuesday, August 21, 2007)]
[Rules and Regulations]
[Page 46559]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: E7-16304]
[[Page 46559]]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2007-28253; Directorate Identifier 2007-NM-031-AD;
Amendment 39-15064; AD 2007-11-07]
RIN 2120-AA64
Airworthiness Directives; Boeing Model 737-100, -200, -200C, -
300, -400, and -500 Series Airplanes
AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule; correction.
-----------------------------------------------------------------------
SUMMARY: The FAA is correcting a typographical error in an existing
airworthiness directive (AD) that was published in the Federal Register
on May 22, 2007 (72 FR 28597). The error resulted in a confusing
compliance time. This AD applies to all Boeing Model 737-100, -200, -
200C, -300, -400, and -500 series airplanes. This AD requires
repetitive detailed inspections for damage of the electrical wire and
sleeve that run to the fuel boost pump through a conduit in the fuel
tank, and arcing damage of the conduit and signs of fuel leakage into
the conduit; replacement of the sleeve with a new, smaller-diameter
sleeve; and related investigative and corrective actions, as
applicable.
DATES: Effective June 6, 2007.
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 Operations office
between 9 a.m. and 5 p.m., Monday through Friday, except Federal
holidays. The Docket Operations office (telephone (800) 647-5527) is
located on the ground level of the West Building at the DOT street
address stated in the ADDRESSES section. This docket number is FAA-
2007-28253; the directorate identifier for this docket is 2007-NM-031-
AD.
FOR FURTHER INFORMATION CONTACT: Suzanne Lucier, Aerospace Engineer,
Propulsion Branch, ANM-140S, FAA, Seattle Aircraft Certification
Office, 1601 Lind Avenue, SW., Renton, Washington 98057-3356; telephone
(425) 917-6438; fax (425) 917-6590.
SUPPLEMENTARY INFORMATION: On May 2, 2007, the FAA issued AD 2007-11-
07, amendment 39-15064 (72 FR 28597, May 22, 2007), for all Boeing
Model 737-100, -200, -200C, -300, -400, and -500 series airplanes. The
AD requires repetitive detailed inspections for damage of the
electrical wire and sleeve that run to the fuel boost pump through a
conduit in the fuel tank, and arcing damage of the conduit and signs of
fuel leakage into the conduit; replacement of the sleeve with a new,
smaller-diameter sleeve; and related investigative and corrective
actions, as applicable.
As published, paragraph (k) of AD 2007-11-07 reads ``* * *
Thereafter, repeat the detailed inspection at intervals not to exceed
15,000 flight cycles. * * *'' The correct term, ``flight hours'' (not
flight cycles), appears in all other compliance times cited in the AD,
as intended.
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 June 6, 2007.
Sec. 39.13 [Corrected]
0
In the Federal Register of May 22, 2007, on page 28600, in the third
column, paragraph (k) of AD 2007-11-07 is corrected to read as follows:
* * * * *
(k) At the applicable time specified by paragraph (k)(1) or
(k)(2) of this AD: Do a detailed inspection for damage of the sleeve
and electrical wire of the fuel boost pump; and, before further
flight, install a new, smaller-diameter sleeve, and do related
investigative and corrective actions, as applicable; in accordance
with the Accomplishment Instructions of Boeing Alert Service
Bulletin 737-28A1263, Revision 1, dated March 19, 2007. Thereafter,
repeat the detailed inspection at intervals not to exceed 15,000
flight hours. Accomplishment of the initial inspection, applicable
corrective actions, and sleeve installation required by this
paragraph terminates the requirements of paragraphs (f), (g), (h),
and (i) of this AD.
* * * * *
Issued in Renton, Washington, on August 14, 2007.
Stephen P. Boyd,
Acting Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. E7-16304 Filed 8-20-07; 8:45 am]
BILLING CODE 4910-13-P
