Proposed Modification of Class B Airspace; Charlotte, NC, 13049-13050 [2010-5879]
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Federal Register / Vol. 75, No. 52 / Thursday, March 18, 2010 / Proposed Rules
13049
TABLE 1—INITIAL COMPLIANCE TIME
For airplanes on which Structural Significant
Items (SSIs) F–25G, F–25H, and F–25I—
Inspect—
(1) Have not been inspected in accordance with
paragraph (i) of AD 2004–07–22 R1, amendment 39–15326, using the HFEC method.
(2) Have been inspected in accordance with
paragraph (i) of AD 2004–07–22 R1, using
the HFEC method.
Before the accumulation of 22,000 total flight cycles, or within 1,000 flight cycles after April 13,
2006 (the effective date of AD 2006–05–09), whichever occurs later.
Repetitive Inspections
(h) Repeat the applicable inspections
required by paragraph (g) of this AD
thereafter at intervals not to exceed those
specified in paragraph 1.E., ‘‘Compliance,’’
(including the note) of Boeing Alert Service
Bulletin 747–53A2499, dated August 11,
2005; or Revision 1, dated October 30, 2008.
As of the effective date of this AD, only
Revision 1, dated October 30, 2008, of Boeing
Alert Service Bulletin 747–53A2499 may be
used.
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New Requirements of This AD
Repetitive Inspections/Investigative and
Corrective Actions
(i) For all airplanes: Do an external HFEC
inspection of the lap joints in Sections 41, 42,
and 46 for cracks, by doing all the actions,
including all applicable related investigative
and corrective actions, specified in the
Accomplishment Instructions of Boeing Alert
Service Bulletin 747–53A2499, Revision 1,
dated October 30, 2008. Do the inspection at
the applicable time specified in paragraph
1.E. of Boeing Alert Service Bulletin 747–
53A2499, Revision 1, dated October 30, 2008;
except as required by paragraph (m) of this
AD. Do all applicable related investigative
and corrective actions before further flight.
Repeat the inspection thereafter at the times
specified in paragraph 1.E. of Boeing Alert
Service Bulletin 747–53A2499, Revision 1,
dated October 30, 2008. Accomplishment of
the inspections required by this paragraph
terminates the inspections required by
paragraphs (g) and (h) of this AD.
(j) For areas on which a lap joint repair was
installed and the repair doubler is greater
than or equal to 40 inches long: Do initial
and repetitive internal HFEC inspections for
cracks by doing all the actions, including all
applicable corrective actions, specified in the
Accomplishment Instructions of Boeing Alert
Service Bulletin 747–53A2499, Revision 1,
dated October 30, 2008, except as required by
paragraph (l) of this AD. Do the inspections
and corrective actions at the times specified
in paragraph 1.E. of Boeing Alert Service
Bulletin 747–53A2499, Revision 1, dated
October 30, 2008, except as required by
paragraph (m) of this AD.
Terminating Action
(k) Modify the applicable lap joints in
sections 41 and 42 by doing all the applicable
actions specified in the Accomplishment
Instructions of Boeing Alert Service Bulletin
747–53A2499, Revision 1, dated October 30,
2008, at the time specified in paragraph 1.E.
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12:44 Mar 17, 2010
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Within 3,000 flight cycles after the most recent supplemental structural inspection document
(SSID) inspection of each applicable structural significant item (as given in Boeing Document D6–35022, ‘‘SSID for Model 747 Airplanes,’’ Revision G, dated December 2000), or
within 1,000 flight cycles after April 13, 2006, whichever occurs later.
of Boeing Alert Service Bulletin 747–
53A2499, Revision 1, dated October 30, 2008;
except as required by paragraphs (l) and (m)
of this AD. Accomplishing this modification
terminates the repetitive inspections of the
skin lap joints in sections 41 and 42 required
by paragraphs (i) and (j) of this AD for the
length of lap joint that is modified.
compliance with the corresponding
requirements of this AD.
Exceptions to Service Bulletin Procedures
(l) Where Boeing Alert Service Bulletin
747–53A2499, Revision 1, dated October 30,
2008, specifies to contact Boeing for
appropriate action, before further flight,
repair the crack using a method approved in
accordance with the procedures specified in
paragraph (n) of this AD.
(m) Where Boeing Alert Service Bulletin
747–53A2499, Revision 1, dated October 30,
2008, specifies a compliance time after the
date of the service bulletin, this AD requires
compliance within the specified compliance
time after the effective date of this AD.
[FR Doc. 2010–5940 Filed 3–17–10; 8:45 am]
Alternative Methods of Compliance
(AMOCs)
(n)(1) The Manager, Seattle Aircraft
Certification Office (ACO), FAA, has the
authority to approve AMOCs for this AD, if
requested using the procedures found in 14
CFR 39.19. Send information to Ivan Li,
Aerospace Engineer, Airframe Branch, ANM–
120S, FAA, Seattle ACO, 1601 Lind Avenue,
SW., Renton, Washington 98057–3356;
telephone (425) 917–6437; fax (425) 917–
6590. Information may be e-mailed to: 9ANM-Seattle-ACO-AMOC-Requests@faa.gov.
(2) To request a different method of
compliance or a different compliance time
for this AD, follow the procedures in 14 CFR
39.19. Before using any approved AMOC on
any airplane to which the AMOC applies,
notify your principal maintenance inspector
(PMI) or principal avionics inspector (PAI),
as appropriate, or lacking a principal
inspector, your local Flight Standards District
Office. The AMOC approval letter must
specifically reference this AD.
(3) An AMOC that provides an acceptable
level of safety may be used for any repair
required by this AD, if it is approved by the
Boeing Commercial Airplanes Organization
Designation Authorization (ODA) or other
person authorized by the Manager, Seattle
ACO, to make those findings. For a repair
method to be approved, the repair must meet
the certification basis of the airplane and the
approval must specifically refer to this AD.
(4) AMOCS approved previously in
accordance with AD 2006–05–09 are
approved as alternative methods of
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Issued in Renton, Washington, on March
10, 2010.
Jeffrey E. Duven,
Acting Manager, Transport Airplane
Directorate, Aircraft Certification Service.
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 71
[Docket No. FAA–2010–0049; Airspace
Docket No. 08–AWA–1]
RIN 2120–AA66
Proposed Modification of Class B
Airspace; Charlotte, NC
AGENCY: Federal Aviation
Administration (FAA), DOT.
ACTION: Notice of proposed rulemaking
(NPRM); correction.
SUMMARY: This action provides the
graphic chart for the proposed rule
published in the Federal Register of
March 3, 2010, regarding the
modification of Class B airspace,
Charlotte, NC. This correction adds the
chart that was inadvertently omitted
from the NPRM.
DATES: Comments must be received on
or before May 3, 2010.
FOR FURTHER INFORMATION CONTACT: Paul
Gallant, Airspace and Rules Group,
Office of System Operations Airspace
and AIM, Federal Aviation
Administration, 800 Independence
Avenue, SW., Washington, DC 20591;
telephone: (202) 267–8783.
Correction
In proposed rule FR Doc. 2010–4377,
beginning on page 9538 in the issue of
March 3, 2010, make the following
correction: On page 9544 in the first
column, add the attached graphic chart
before the Issue Date line.
E:\FR\FM\18MRP1.SGM
18MRP1
Federal Register / Vol. 75, No. 52 / Thursday, March 18, 2010 / Proposed Rules
Issued in Washington, DC, on March 9,
2010.
Edith V. Parish,
Manager, Airspace and Rules Group.
AGENCY: Office of General Counsel
(OGC), National Oceanic and
Atmospheric Administration (NOAA),
Commerce.
ACTION: Proposed rule.
SUMMARY: This rule amends the
procedures governing NOAA’s
administrative proceedings for the
[FR Doc. 2010–5879 Filed 3–17–10; 8:45 am]
assessment of civil penalties;
suspension, revocation, modification, or
denial of permits; issuance and use of
written warnings; and release or
forfeiture of seized property. The
principal change removes the
requirement that an Administrative Law
Judge state good reason(s) for departing
from the civil penalty or permit sanction
assessed by NOAA in its charging
document. This revision eliminates any
presumption in favor of the civil penalty
or permit sanction assessed by NOAA.
The other change corrects a clerical
error in a citation to rules pertaining to
protective orders issued by
Administrative Law Judges.
DATES: Written comments on this
proposed rule must be submitted by
April 16, 2010.
DEPARTMENT OF COMMERCE
National Oceanic and Atmospheric
Administration
15 CFR Part 904
BILLING CODE 4910–13–P
[Docket No. 100216090–0123–01]
RIN 0648–AY66
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Regulations to Amend the Civil
Procedures
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EP18MR10.004</GPH>
13050
]]>Agencies
[Federal Register Volume 75, Number 52 (Thursday, March 18, 2010)]
[Proposed Rules]
[Pages 13049-13050]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: 2010-5879]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 71
[Docket No. FAA-2010-0049; Airspace Docket No. 08-AWA-1]
RIN 2120-AA66
Proposed Modification of Class B Airspace; Charlotte, NC
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Notice of proposed rulemaking (NPRM); correction.
-----------------------------------------------------------------------
SUMMARY: This action provides the graphic chart for the proposed rule
published in the Federal Register of March 3, 2010, regarding the
modification of Class B airspace, Charlotte, NC. This correction adds
the chart that was inadvertently omitted from the NPRM.
DATES: Comments must be received on or before May 3, 2010.
FOR FURTHER INFORMATION CONTACT: Paul Gallant, Airspace and Rules
Group, Office of System Operations Airspace and AIM, Federal Aviation
Administration, 800 Independence Avenue, SW., Washington, DC 20591;
telephone: (202) 267-8783.
Correction
In proposed rule FR Doc. 2010-4377, beginning on page 9538 in the
issue of March 3, 2010, make the following correction: On page 9544 in
the first column, add the attached graphic chart before the Issue Date
line.
[[Page 13050]]
[GRAPHIC] [TIFF OMITTED] TP18MR10.004
Issued in Washington, DC, on March 9, 2010.
Edith V. Parish,
Manager, Airspace and Rules Group.
[FR Doc. 2010-5879 Filed 3-17-10; 8:45 am]
BILLING CODE 4910-13-P
