[Federal Register Volume 76, Number 202 (Wednesday, October 19, 2011)]
[Rules and Regulations]
[Pages 64798-64801]
[FR Doc No: 2011-26082]

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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2011-0478; Directorate Identifier 2010-NM-138-AD;
Amendment 39-16832; AD 2011-21-09]
RIN 2120-AA64

Airworthiness Directives; Airbus Model A300 B4-103, B4-203, and
B4-2C Airplanes

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

ACTION: Final rule.

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SUMMARY: We are superseding an existing airworthiness directive (AD)
that applies to the products listed above. This AD results from
mandatory continuing airworthiness information (MCAI) originated by an
aviation authority of another country to identify and correct an unsafe
condition on an aviation product. The MCAI describes the unsafe
condition as:

    One operator reported a failure of the MLG [main landing gear]
retraction actuator sliding rod. This incident occurred at a number
of operating flight cycles lower than the limit value imposed by the
MLG manufacturer.
    This condition, if not detected and corrected, results in
undampened extension of the MLG, leading to higher than usual loads
on the MLG attachment. Higher loads affect the structural integrity
of the MLG and could lead to MLG failure.
* * * * *
We are issuing this AD to require actions to correct the unsafe
condition on these products.

DATES: This AD becomes effective November 23, 2011.
    The Director of the Federal Register approved the incorporation by
reference of certain publications listed in this AD as of November 23,
2011.

ADDRESSES: You may examine the AD docket on the Internet at http://www.regulations.gov or in person at the U.S. Department of
Transportation, Docket Operations, M-30, West Building Ground Floor,
Room W12-140, 1200 New Jersey Avenue, SE., Washington, DC.

FOR FURTHER INFORMATION CONTACT: Dan Rodina, Aerospace Engineer,
International Branch, ANM-116, Transport Airplane Directorate, FAA,
1601 Lind Avenue SW., Renton, Washington 98057-3356; telephone (425)
227-2125; fax<PHONE_NUMBER>.

SUPPLEMENTARY INFORMATION:

Discussion

    We issued a notice of proposed rulemaking (NPRM) to amend 14 CFR
part 39 to include an AD that would apply to the specified products.
That NPRM was published in the Federal Register on June 8, 2011 (76 FR
33176), and proposed to supersede AD 2007-25-15, Amendment 39-15297 (72
FR 69601, December 10, 2007). That NPRM proposed to correct an unsafe
condition for the specified products. The MCAI states:

    One operator reported a failure of the MLG [main landing gear]
retraction actuator sliding rod. This incident occurred at a number
of operating flight cycles lower than the limit value imposed by the
MLG manufacturer.
    This condition, if not detected and corrected, results in
undampened extension of the MLG, leading to higher than usual loads
on the MLG attachment. Higher loads affect the structural integrity
of the MLG and could lead to MLG failure.
    To address and correct this unsafe condition, EASA issued AD
2006-0075 (now at Revision 2) [which corresponds to FAA AD 2007-25-
15 (72 FR 69601, December 10, 2007)] to require repetitive
inspections of the retraction actuator sliding rod as installed on
A300, A300-600 and A300-600ST aeroplanes and, depending on findings,
repair or replacement of the affected parts.
    Since this event, studies have been performed by Airbus, the
consequences of which are that for A300 aeroplanes, a new inspection
program (new threshold and interval) has been established.
    For the reason described above, this new [EASA] AD retains the
requirements of AD

2006-0075R2, which is superseded and requires the accomplishment of
the repetitive inspections and associated corrective actions at the
new intervals. In addition, the Airbus A300 Aircraft Maintenance
Manual (AMM) Chapter 12-22-32 (associated to Maintenance Planning
Document (MPD) task<PHONE_NUMBER>-1) has been revised to introduce a
greasing action at the level of the pick-up jack fitting.
Consequently, this AD also requires the repetitive lubrication task.
    For A300-600 and A300-600ST aeroplanes, the analyses have shown
that, due to design differences, the loads induced on the MLG
attachments are within acceptable margins. For that reason, this AD
does not apply to those aeroplanes which were previously included in
the applicability of EASA AD 2006-0075R2.

You may obtain further information by examining the MCAI in the AD
docket.

Comments

    We gave the public the opportunity to participate in developing
this AD. We considered the comment received.

Request To Change Proposed Compliance Time

    The Air Line Pilots Association, International (ALPA) stated it
supports the intent and language of the subject NPRM (76 FR 33176, June
8, 2011), but requested the compliance time be changed in paragraph (g)
of the NPRM to ``not to exceed 1000 flight hours or 12 months,
whichever occurs first, under any circumstances.''
    We disagree with this request because the unsafe condition is
flight-cycle dependent, and the commenter did not provide any
supporting data to justify a change in the compliance time. We have not
changed the AD in this regard.

Conclusion

    We reviewed the available data, including the comment received, and
determined that air safety and the public interest require adopting the
AD as proposed.

Differences Between This AD and the MCAI or Service Information

    We have reviewed the MCAI and related service information and, in
general, agree with their substance. But we might have found it
necessary to use different words from those in the MCAI to ensure the
AD is clear for U.S. operators and is enforceable. In making these
changes, we do not intend to differ substantively from the information
provided in the MCAI and related service information.
    We might also have required different actions in this AD from those
in the MCAI in order to follow our FAA policies. Any such differences
are highlighted in a NOTE within the AD.

Costs of Compliance

    We estimate that this AD will affect 3 products of U.S. registry.
We also estimate that it will take about 6 work-hours per product to
comply with the basic requirements of this AD. The average labor rate
is $85 per work-hour. Based on these figures, we estimate the cost of
this AD to the U.S. operators to be $1,530, or $510 per product.
    In addition, we estimate that any necessary follow-on actions would
take about 6 work-hours and require parts costing $0, for a cost of
$510 per product. We have no way of determining the number of products
that may need these actions.

Authority for This Rulemaking

    Title 49 of the United States Code specifies the FAA's authority to
issue rules on aviation safety. Subtitle I, section 106, describes the
authority of the FAA Administrator. ``Subtitle VII: Aviation
Programs,'' describes in more detail the scope of the Agency's
authority.
    We are issuing this rulemaking under the authority described in
``Subtitle VII, Part A, Subpart III, Section 44701: General
requirements.'' Under that section, Congress charges the FAA with
promoting safe flight of civil aircraft in air commerce by prescribing
regulations for practices, methods, and procedures the Administrator
finds necessary for safety in air commerce. This regulation is within
the scope of that authority because it addresses an unsafe condition
that is likely to exist or develop on products identified in this
rulemaking action.

Regulatory Findings

    We determined that this AD will not have federalism implications
under Executive Order 13132. This AD will not have a substantial direct
effect 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.
    For the reasons discussed above, I certify this AD:
    1. Is not a ''significant regulatory action'' under Executive Order
12866;
    2. Is not a ''significant rule'' under the DOT Regulatory Policies
and Procedures (44 FR 11034, February 26, 1979); and
    3. Will not have a significant economic impact, positive or
negative, on a substantial number of small entities under the criteria
of the Regulatory Flexibility Act.
    We prepared a regulatory evaluation of the estimated costs to
comply with this AD and placed it in the AD docket.

Examining the AD Docket

    You may examine the AD docket on the Internet at http://www.regulations.gov; or in person at the Docket Operations office
between 9 a.m. and 5 p.m., Monday through Friday, except Federal
holidays. The AD docket contains the NPRM (76 FR 33176, June 8, 2011),
the regulatory evaluation, any comments received, and other
information. The street address for the Docket Operations office
(telephone<PHONE_NUMBER>) is in the ADDRESSES section. Comments will
be available in the AD docket shortly after receipt.

List of Subjects in 14 CFR Part 39

    Air transportation, Aircraft, Aviation safety, Incorporation by
reference, Safety.

Adoption of the Amendment

    Accordingly, under the authority delegated to me by the
Administrator, the FAA amends 14 CFR part 39 as follows:

PART 39--AIRWORTHINESS DIRECTIVES

0
1. The authority citation for part 39 continues to read as follows:

    Authority: 49 U.S.C. 106(g), 40113, 44701.

Sec.  39.13  [Amended]

0
2. The FAA amends Sec.  39.13 by removing Amendment 39-15297 (72 FR
69601, December 10, 2007) and adding the following new AD:

2011-21-09 Airbus: Amendment 39-16832. Docket No. FAA-2011-0475;
Directorate Identifier 2010-NM-138-AD.

Effective Date

    (a) This airworthiness directive (AD) becomes effective November
23, 2011.

Affected ADs

    (b) This AD supersedes AD 2007-25-15, Amendment 39-15297 (72 FR
69601, December 10, 2007).

Applicability

    (c) This AD applies to Airbus Model A300 B4-103, B4-203, and B4-
2C airplanes; certificated in any category; equipped with main
landing gear (MLG) retraction actuator having part number (P/N)
C23129 fitted with sliding rod P/N C69029-2 or C69029-3.

Subject

    (d) Air Transport Association (ATA) of America Code 32: Landing
gear.

Reason

    (e) The mandatory continuing airworthiness information (MCAI)
states:

    One operator reported a failure of the MLG [main landing gear]
retraction actuator sliding rod. This incident occurred at a number
of operating flight cycles lower than

the limit value imposed by the MLG manufacturer.
    This condition, if not detected and corrected, results in
undampened extension of the MLG, leading to higher than usual loads
on the MLG attachment. Higher loads affect the structural integrity
of the MLG and could lead to MLG failure.
* * * * *

Compliance

    (f) You are responsible for having the actions required by this
AD performed within the compliance times specified, unless the
actions have already been done.

Revised Compliance Times for Inspection of MLG Retraction Actuator and
Corrective Actions

    (g) At the applicable time specified in paragraphs (g)(1),
(g)(2), and (g)(3) of this AD: Remove the MLG retraction actuator
having P/N C23129 and do a detailed and high frequency eddy current
inspection for defects that exceed the criteria defined in Messier-
Dowty Special Inspection Service Bulletin 470-32-806, dated October
27, 2005, of the retraction actuator sliding rods having P/N C69029-
2 or C69029-3, in accordance with the Accomplishment Instructions of
Airbus Mandatory Service Bulletin A300-32-0450, Revision 02, dated
July 28, 2009.
    (1) For airplanes on which the retraction actuator sliding rod
has accumulated 12,000 or fewer total flight cycles as of the
effective date of this AD: Inspect at the later of the times
specified in paragraphs (g)(1)(i) and (g)(1)(ii) of this AD.
    (i) Before the accumulation of 12,000 total flight cycles on the
retraction actuator sliding rod.
    (ii) Within 2,000 flight cycles or 24 months after the effective
date of this AD, whichever occurs first.
    (2) For airplanes on which the retraction actuator sliding rod
has accumulated more than 12,000 total flight cycles, and 22,000 or
fewer total flight cycles, as of the effective date of this AD:
Inspect at the earliest of the times specified in paragraphs
(g)(2)(i), (g)(2)(ii), and (g)(2)(iii) of this AD.
    (i) Before the accumulation of 23,000 total flight cycles on the
retraction actuator sliding rod.
    (ii) Within 2,000 flight cycles after the effective date of this
AD.
    (iii) Within 24 months after the effective date of this AD.
    (3) For airplanes on which the retraction actuator sliding rod
has accumulated more than 22,000 total flight cycles as of the
effective date of this AD: Inspect within 1,000 flight cycles or 12
months after the effective date of this AD, whichever occurs first.
    (h) Thereafter, repeat the inspections required by paragraph (g)
of this AD at intervals not to exceed 12,000 flight cycles.
    (i) If, during any inspection required by paragraph (g) or (h)
of this AD, any defect is detected that exceeds the criteria defined
in Messier-Dowty Special Inspection Service Bulletin 470-32-806,
dated October 27, 2005, before further flight, replace the affected
sliding rod with a serviceable unit in accordance with the
Accomplishment Instructions of Airbus Mandatory Service Bulletin
A300-32-0450, Revision 02, dated July 28, 2009.
    (j) Before the accumulation of 32,000 flight cycles on any
retraction actuator sliding rod, it must be replaced with a
serviceable unit in accordance with the Accomplishment Instructions
of Airbus Mandatory Service Bulletin A300-32-0450, Revision 02,
dated July 28, 2009. Parts removed from an airplane as required by
this paragraph must be returned to Messier-Dowty within 30 days
after removing the part from the airplane.
    (k) As of the effective date of this AD, any MLG retraction
actuator sliding rod having P/N C69029-2 or C69029-3 that has
accumulated less than 32,000 total flight cycles, may be installed
on any airplane, provided that the inspections required by
paragraphs (g) and (h) of this AD are accomplished at the compliance
times specified in paragraphs (g) and (h) of this AD and all
applicable replacements required by paragraphs (i) and (j) of this
AD are done.

Lubrication of the MLG Assembly

    (l) Within 1,500 flight hours after the effective date of this
AD: Clean and lubricate the MLG assembly, in accordance with Task
321112-0505-1 ``Main Landing Gear Assy,'' of Section 2-32, ``Systems
and Powerplant Program: Landing Gear,'' of the Airbus A300
Maintenance Planning Document, Revision 30, dated April 1, 2010.
Repeat the cleaning and lubrication thereafter at intervals not to
exceed 1,500 flight hours.

Credit for Actions Accomplished in Accordance With Previous Service
Information

    (m) Inspections accomplished before the effective date of this
AD, in accordance with Airbus Mandatory Service Bulletin A300-32-
0450, dated December 1, 2005; or Airbus Mandatory Service Bulletin
A300-32-0450, Revision 01, dated May 10, 2006; are acceptable for
compliance with the corresponding requirements of this AD.

FAA AD Differences

    Note 1: This AD differs from the MCAI and/or service information
as follows: No differences.

Other FAA AD Provisions

    (n) The following provisions also apply to this AD:
    (1) Alternative Methods of Compliance (AMOCs): The Manager,
International Branch, ANM-116, Transport Airplane Directorate, FAA,
has the authority to approve AMOCs for this AD, if requested using
the procedures found in 14 CFR 39.19. In accordance with 14 CFR
39.19, send your request to your principal inspector or local Flight
Standards District Office, as appropriate. If sending information
directly to the International Branch, send it to ATTN: Dan Rodina,
Aerospace Engineer, International Branch, ANM-116, Transport
Airplane Directorate, FAA, 1601 Lind Avenue, SW., Renton, Washington
98057-3356; telephone<PHONE_NUMBER>; fax<PHONE_NUMBER>.
Information may be e-mailed to<EMAIL_ADDRESS>
Before using any approved AMOC, notify your appropriate principal
inspector, or lacking a principal inspector, the manager of the
local flight standards district office/certificate holding district
office. The AMOC approval letter must specifically reference this
AD. AMOCs approved previously in accordance with AD 2007-25-15,
Amendment 39-15297 (72 FR 69601, December 10, 2007), are approved as
AMOCs for the corresponding provisions of this AD.
    (2) Airworthy Product: For any requirement in this AD to obtain
corrective actions from a manufacturer or other source, use these
actions if they are FAA-approved. Corrective actions are considered
FAA-approved if they are approved by the State of Design Authority
(or their delegated agent). You are required to assure the product
is airworthy before it is returned to service.

Related Information

    (o) Refer to MCAI European Aviation Safety Agency Airworthiness
Directive 2010-0102, dated June 8, 2010; Airbus Mandatory Service
Bulletin A300-32-0450, Revision 02, dated July 28, 2009; Messier-
Dowty Special Inspection Service Bulletin 470-32-806, dated October
27, 2005; and Task<PHONE_NUMBER>-1, ``Main Landing Gear Assy,'' of
Section 2-32, ``Systems and Powerplant Program: Landing Gear,'' of
the Airbus A300 Maintenance Planning Document, Revision 30, dated
April 1, 2010; for related information.

Material Incorporated by Reference

    (p) You must use Airbus Mandatory Service Bulletin A300-32-0450,
Revision 02, excluding Appendix 1, dated July, 28, 2009; Messier-
Dowty Special Inspection Service Bulletin 470-32-806, dated October
27, 2005; and Task<PHONE_NUMBER>-1, ``Main Landing Gear Assy,'' of
Section 2-32, ``Systems and Powerplant Program: Landing Gear,'' of
the Airbus A300 Maintenance Planning Document, Revision 30, dated
April 1, 2010; to do the actions required by this AD, unless the AD
specifies otherwise. (The revision level of the Airbus A300
Maintenance Planning Document is identified in only the title page
and transmittal letter of this document.)
    (1) The Director of the Federal Register approved the
incorporation by reference of this service information under 5
U.S.C. 552(a) and 1 CFR part 51.
    (2) For Messier-Dowty service information identified in this AD,
contact Messier Services Americas, Customer Support Center, 45360
Severn Way, Sterling, Virginia 20166-8910; telephone<PHONE_NUMBER>;
fax<PHONE_NUMBER>; Internet https://techpubs.services/messier-dowty.com.
    (3) For Airbus service information identified in this AD,
contact Airbus SAS-EAW (Airworthiness Office), 1 Rond Point Maurice
Bellonte, 31707 Blagnac Cedex, France; telephone +33 5 61 93 36 96;
fax +33 5 61 93 44 51; e-mail<EMAIL_ADDRESS>
Internet http://www.airbus.com.
    (4) You may review copies of the service information at the FAA,
Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton,
Washington. For information on the availability of this material at
the FAA, call<PHONE_NUMBER>.

    (5) You may also review copies of the service information that
is incorporated by reference at the National Archives and Records
Administration (NARA). For information on the availability of this
material at NARA, call<PHONE_NUMBER>, or go to: http://www.archives.gov/federal_register/code_of_federal_regulations/ibr_locations.html.

    Issued in Renton, Washington, on September 28, 2011.
Ali Bahrami,
Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 2011-26082 Filed 10-18-11; 8:45 am]
BILLING CODE 4910-13-P


[Federal Register Volume 82, Number 53 (Tuesday, March 21, 2017)]
[Rules and Regulations]
[Pages 14429-14433]
[FR Doc No: 2017-05162]

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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2017-0129; Directorate Identifier 2017-NM-020-AD;
Amendment 39-18825; AD 2017-06-01]
RIN 2120-AA64

Airworthiness Directives; The Boeing Company Airplanes

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Final rule; request for comments.

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SUMMARY: We are superseding Airworthiness Directive (AD) 2017-03-04,
which applied to all The Boeing Company Model 737-500 series airplanes.
AD 2017-03-04 required inspections to detect cracks in the fuselage
skin panels, permanent repairs of time-limited repairs, skin panel
replacement, and related investigative and corrective actions if
necessary. This AD reduces the applicability of AD 2017-03-04. This AD
was prompted by a determination that airplanes were inadvertently
included in the applicability of AD 2017-03-04. We are

issuing this AD to address the unsafe condition on these products.

DATES: This AD is effective April 5, 2017.
    The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in this AD as of March 28,
2017 (82 FR 11140, February 21, 2017).
    We must receive comments on this AD by May 5, 2017.

ADDRESSES: You may send comments, using the procedures found in 14 CFR
11.43 and 11.45, by any of the following methods:
     Federal eRulemaking Portal: Go to http://www.regulations.gov. Follow the instructions for submitting comments.
     Fax:<PHONE_NUMBER>.
     Mail: U.S. Department of Transportation, Docket
Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New
Jersey Avenue SE., Washington, DC 20590.
     Hand Delivery: Deliver to Mail address above between 9
a.m. and 5 p.m., Monday through Friday, except Federal holidays.
    For service information identified in this final rule, contact
Boeing Commercial Airplanes, Attention: Contractual & Data Services
(C&DS), 2600 Westminster Blvd., MC 110-SK57, Seal Beach, CA 90740-5600;
telephone<PHONE_NUMBER>; Internet https://www.myboeingfleet.com. You may
view this referenced service information at the FAA, Transport Airplane
Directorate, 1601 Lind Avenue SW., Renton, WA. For information on the
availability of this material at the FAA, call<PHONE_NUMBER>. It is also
available on the Internet at http://www.regulations.gov by searching
for and locating Docket No. FAA-2017-0129.

Examining the AD Docket

    You may examine the AD docket on the Internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2017-
0129; or in person at the Docket Management Facility between 9 a.m. and
5 p.m., Monday through Friday, except Federal holidays. The AD docket
contains this AD, the regulatory evaluation, any comments received, and
other information. The street address for the Docket Office (phone:
800-647-5527) is in the ADDRESSES section. Comments will be available
in the AD docket shortly after receipt.

FOR FURTHER INFORMATION CONTACT: Jennifer Tsakoumakis, Aerospace
Engineer, Airframe Branch, ANM-120L, FAA, Los Angeles Aircraft
Certification Office (ACO), 3960 Paramount Boulevard, Lakewood, CA
90712-4137; phone:<PHONE_NUMBER>; fax:<PHONE_NUMBER>; email:
<EMAIL_ADDRESS>
SUPPLEMENTARY INFORMATION:

Discussion

    On January 31, 2017, we issued AD 2017-03-04, Amendment 39-18795
(82 FR 11140, February 21, 2017) (``AD 2017-03-04''), for all The
Boeing Company Model 737-500 series airplanes. AD 2017-03-04 required
inspections to detect cracks in the fuselage skin panels, permanent
repairs of time-limited repairs, skin panel replacement, and related
investigative and corrective actions if necessary. AD 2017-03-04
resulted from an evaluation by the design approval holder (DAH) that
indicates the fuselage skin is subject to widespread fatigue damage
(WFD), and reports of cracks at the chem-milled steps in the fuselage
skin. We issued AD 2017-03-04 to detect and correct cracking on the aft
lower lobe fuselage skins, which could result in rapid decompression of
the airplane.

Actions Since AD 2017-03-04 Was Issued

    Since we issued AD 2017-03-04, we determined that airplanes were
inadvertently included in the applicability of AD 2017-03-04. AD 2017-
03-04 superseded AD 2012-16-07, Amendment 39-17154 (77 FR 48423, August
14, 2012) (``AD 2012-16-07''), which applied to certain The Boeing
Company Model 737-500 series airplanes. The identified unsafe condition
only applies to the airplanes identified in AD 2012-16-07 and,
therefore, the applicability of AD 2017-03-04 should not have included
additional airplanes.
    The affected airplanes are identified in Boeing Special Attention
Service Bulletin 737-53-1315, Revision 1, dated June 30, 2015 (which is
referred to as the appropriate source of service information for
accomplishing the actions required by AD 2017-03-04). In order to
correct the applicability, we have referred to Boeing Special Attention
Service Bulletin 737-53-1315, Revision 1, dated June 30, 2015, in
paragraph (c)(1) of this AD. We are issuing this AD to address the
unsafe condition on these products.

Related Service Information Under 1 CFR Part 51

    We reviewed Boeing Special Attention Service Bulletin 737-53-1315,
Revision 1, dated June 30, 2015. The service information describes
procedures for inspections to detect cracks in the fuselage skin
panels, permanent repairs of time-limited repairs, skin panel
replacement, and related investigative and corrective actions. This
service information is reasonably available because the interested
parties have access to it through their normal course of business or by
the means identified in the ADDRESSES section.

FAA's Determination

    We are issuing this AD because we evaluated all the relevant
information and determined the unsafe condition described previously is
likely to exist or develop in other products of the same type design.

AD Requirements

    This AD requires accomplishing the actions specified in the service
information described previously, except as discussed under
``Differences Between this AD and the Service Information.'' This AD
also reduces the applicability of AD 2017-03-04. For information on the
procedures and compliance times, see this service information at http://www.regulations.gov by searching for and locating Docket No. FAA-2017-
0129.
    The phrase ``related investigative actions'' is used in this AD.
Related investigative actions are follow-on actions that (1) are
related to the primary action, and (2) further investigate the nature
of any condition found. Related investigative actions in an AD could
include, for example, inspections.
    The phrase ``corrective actions'' is used in this AD. Corrective
actions correct or address any condition found. Corrective actions in
an AD could include, for example, repairs.

Differences Between This AD and the Service Information

    Boeing Special Attention Service Bulletin 737-53-1315, Revision 1,
dated June 30, 2015, specifies to contact the manufacturer for
instructions on how to repair certain conditions and also to obtain
certain work instructions, but this AD requires repairing those
conditions and also to obtain those work instructions in one of the
following ways:
     In accordance with a method that we approve; or
     Using data that meet the certification basis of the
airplane, and that have been approved by the Boeing Commercial
Airplanes Organization Designation Authorization (ODA) whom we have
authorized to make those findings.

FAA's Justification and Determination of the Effective Date

    We determined that airplanes were inadvertently included in the
applicability of AD 2017-03-04, which applies to all Model 737-500
series airplanes. However, only airplanes identified in Boeing Special
Attention Service Bulletin 737-53-1315, Revision 1, dated June 30,
2015, are affected by the identified unsafe condition. The actions
required by this AD are not required to be done on airplanes that are
not identified in Boeing Special Attention Service Bulletin 737-53-
1315, Revision 1, dated June 30, 2015. Therefore, we are superseding AD
2017-03-04 to correct the applicability. We find that notice and
opportunity for prior public comment are unnecessary and that good
cause exists for making this amendment effective in less than 30 days.

Comments Invited

    This AD is a final rule that involves requirements affecting flight
safety and was not preceded by notice and an opportunity for public
comment. However, we invite you to send any written data, views, or
arguments about this AD. Send your comments to an address listed under
the ADDRESSES section. Include the docket number FAA-2017-0129 and
Directorate Identifier 2017-NM-020-AD at the beginning of your
comments. We specifically invite comments on the overall regulatory,
economic, environmental, and energy aspects of this AD. We will
consider all comments received by the closing date and may amend this
AD because of those comments.
    We will post all comments we receive, without change, to http://www.regulations.gov, including any personal information you provide. We
will also post a report summarizing each substantive verbal contact we
receive about this AD.

Costs of Compliance

    We estimate that this AD affects 33 airplanes of U.S. registry.
    We estimate the following costs to comply with this AD:

                                                 Estimated Costs
----------------------------------------------------------------------------------------------------------------
                                                                                Cost  on U.S.
              Action                    Labor cost        Parts cost      Cost per product        operators
----------------------------------------------------------------------------------------------------------------
Inspections (actions retained      Up to 1,538 work-                $0  Up to $130,730 per   Up to $4,314,090
 from AD 2017-03-04).               hours x $85 per                      inspection cycle.    per inspection
                                    hour = $130,730                                           cycle.
                                    per inspection
                                    cycle.
Skin panel replacement (action     688 work-hours x             96,000  $154,480...........  $5,097,840.
 retained from AD 2017-03-04).      $85 per hour =
                                    $58,480.
----------------------------------------------------------------------------------------------------------------

    We estimate the following costs to do any necessary repairs that
would be required based on the results of the inspection. We have no
way of determining the number of aircraft that might need these
repairs:

                                               On-Condition Costs
----------------------------------------------------------------------------------------------------------------
              Action                     Labor cost         Parts cost               Cost per product
----------------------------------------------------------------------------------------------------------------
Time-limited repair...............  24 work-hours x $85            \(1)\  $2,040.
                                     per hour = $2,040.
Permanent repair..................  31 work-hours x $85            \(1)\  $2,635.
                                     per hour = $2,635.
Permanent repair inspection.......  4 work-hours x $85             \(1)\  $340 per inspection cycle.
                                     per hour = $340 per
                                     inspection cycle.
----------------------------------------------------------------------------------------------------------------
\1\ We have received no definitive data that would enable us to provide parts cost estimates for the on-
  condition actions specified in this AD.

Authority for This Rulemaking

    Title 49 of the United States Code specifies the FAA's authority to
issue rules on aviation safety. Subtitle I, section 106, describes the
authority of the FAA Administrator. ``Subtitle VII: Aviation Programs''
describes in more detail the scope of the Agency's authority.
    We are issuing this rulemaking under the authority described in
Subtitle VII, Part A, Subpart III, Section 44701: ``General
requirements.'' Under that section, Congress charges the FAA with
promoting safe flight of civil aircraft in air commerce by prescribing
regulations for practices, methods, and procedures the Administrator
finds necessary for safety in air commerce. This regulation is within
the scope of that authority because it addresses an unsafe condition
that is likely to exist or develop on products identified in this
rulemaking action.

Regulatory Findings

    This AD will not have federalism implications under Executive Order
13132. This AD will not have a substantial direct effect 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.
    For the reasons discussed above, I certify that this AD:
    (1) Is not a ``significant regulatory action'' under Executive
Order 12866,
    (2) Is not a ``significant rule'' under DOT Regulatory Policies and
Procedures (44 FR 11034, February 26, 1979),
    (3) Will not affect intrastate aviation in Alaska, and
    (4) Will not have a significant economic impact, positive or
negative, on a substantial number of small entities under the criteria
of the Regulatory Flexibility Act.

List of Subjects in 14 CFR Part 39

    Air transportation, Aircraft, Aviation safety, Incorporation by
reference, Safety.

Adoption of the Amendment

    Accordingly, under the authority delegated to me by the
Administrator, the FAA amends 14 CFR part 39 as follows:

PART 39--AIRWORTHINESS DIRECTIVES

0
1. The authority citation for part 39 continues to read as follows:

    Authority: 49 U.S.C. 106(g), 40113, 44701.

Sec.  39.13  [Amended]

0
2. The FAA amends Sec.  39.13 by removing Airworthiness Directive (AD)
2017-03-04, Amendment 39-18795 (82 FR 11140, February 21, 2017), and
adding the following new AD:

2017-06-01 The Boeing Company: Amendment 39-18825; Docket No. FAA-
2017-0129; Directorate Identifier 2017-NM-020-AD.

(a) Effective Date

    This AD is effective April 5, 2017.

(b) Affected ADs

    This AD replaces AD 2017-03-04, Amendment 39-18795 (82 FR 11140,
February 21, 2017) (``AD 2017-03-04'').

(c) Applicability

    (1) This AD applies to The Boeing Company Model 737-500 series
airplanes, certificated in any category; as identified in Boeing
Special Attention Service Bulletin 737-53-1315, Revision 1, dated
June 30, 2015 (``SASB 737-53-1315 R1'').
    (2) Installation of Supplemental Type Certificate (STC)
ST01219SE (http://rgl.faa.gov/Regulatory_and_Guidance_Library/
rgstc.nsf/0/ebd1cec7b301293e86257cb30045557a/$FILE/ST01219SE.pdf)
does not affect the ability to accomplish the actions required by
this AD. Therefore, for airplanes on which STC ST01219SE is
installed, a ''change in product'' alternative method of compliance
(AMOC) approval request is not necessary to comply with the
requirements of 14 CFR 39.17.

(d) Subject

    Air Transport Association (ATA) of America Code 53, Fuselage.

(e) Unsafe Condition

    This AD was prompted by an evaluation by the design approval
holder (DAH) that indicates the fuselage skin is subject to
widespread fatigue damage (WFD), and reports of cracks at the chem-
milled steps in the fuselage skin. We are issuing this AD to detect
and correct cracking on the aft lower lobe fuselage skins, which
could result in rapid decompression of the airplane.

(f) Compliance

    Comply with this AD within the compliance times specified,
unless already done.

(g) Retained Inspections, Related Investigative and Corrective Actions,
With No Changes

    This paragraph restates the requirements of paragraph (g) of AD
2017-03-04, with no changes. At the applicable times specified in
table 1 of paragraph 1.E., ``Compliance,'' of SASB 737-53-1315 R1,
except as required by paragraphs (h)(1) and (h)(2) of this AD: Do
the applicable inspections to detect cracks in the fuselage skin
panels; and do all applicable related investigative and corrective
actions; in accordance with the Accomplishment Instructions of SASB
737-53-1315 R1, except as required by paragraphs (h)(3) and (h)(4)
of this AD. Do all applicable related investigative and corrective
actions before further flight. Repeat the applicable inspections
thereafter at the applicable intervals specified in SASB 737-53-1315
R1. Accomplishment of a repair in accordance with ``Part 3: Repair''
of the Accomplishment Instructions of SASB 737-53-1315 R1, except as
required by paragraph (h)(3) of this AD, is terminating action for
the repetitive inspections required by this paragraph at the
repaired locations only.

(h) Retained Exceptions to SASB 737-53-1315 R1, With No Changes

    This paragraph restates the service information exceptions
specified in paragraph (h) of AD 2017-03-04, with no changes.
    (1) Where SASB 737-53-1315 R1, specifies compliance times
``after the Revision 1 date of this service bulletin,'' this AD
requires compliance within the specified compliance times ``after
March 28, 2017 (the effective date of AD 2017-03-04).''
    (2) The Condition column of table 1 of Paragraph 1.E.,
``Compliance,'' of SASB 737-53-1315 R1, refers to airplanes in
certain configurations ``as of the issue date of Revision 1 of this
service bulletin.'' However, this AD applies to airplanes in the
specified configurations ``as of March 28, 2017 (the effective date
of AD 2017-03-04).''
    (3) Where SASB 737-53-1315 R1, specifies contacting Boeing for
repair instructions or work instructions, before further flight,
repair or perform the work instructions using a method approved in
accordance with the procedures specified in paragraph (m) of this
AD, except as required by paragraph (h)(4) of this AD.
    (4) For airplanes on which an operator has a record that a skin
panel was replaced with a production skin panel before 53,000 total
flight cycles: At the applicable time for the next inspection, as
specified in table 1 of paragraph 1.E., ``Compliance,'' of SASB 737-
53-1315 R1, except as provided by paragraphs (h)(1) and (h)(2) of
this AD: Perform inspections and applicable corrective actions using
a method approved in accordance with the procedures specified in
paragraph (m) of this AD.
    (5) The Condition column of table 2 of Paragraph 1.E.,
``Compliance,'' of SASB 737-53-1315 R1 refers to airplanes in
certain configurations as of the ``issue date of Revision 1 of this
service bulletin.'' However, this AD applies to airplanes in the
specified configurations regardless of when the time-limited repair
is installed.

(i) Retained Actions for Airplanes With a Time-Limited Repair
Installed, With No Changes

    This paragraph restates the requirements of paragraph (i) of AD
2017-03-04, with no changes. For airplanes with a time-limited
repair installed as specified in Boeing Special Attention Service
Bulletin 737-53-1315, dated July 29, 2011; or SASB 737-53-1315 R1:
At the applicable times specified in table 2 of paragraph 1.E.,
``Compliance,'' of SASB 737-53-1315 R1, except as provided by
paragraphs (h)(1) and (h)(5) of this AD, do the actions specified in
paragraphs (i)(1) and (i)(2) of this AD.
    (1) Do the applicable inspections to detect missing or loose
fasteners and any disbonding or cracking of bonded doublers; and do
all applicable related investigative and corrective actions; in
accordance with the Accomplishment Instructions of SASB 737-53-1315
R1, except as required by paragraph (h)(3) of this AD. Do all
applicable related investigative and corrective actions before
further flight. Repeat the applicable inspections thereafter at the
applicable intervals specified in SASB 737-53-1315 R1.
    (2) Make the time-limited repair permanent and do all applicable
related investigative and corrective actions in accordance with the
Accomplishment Instructions of SASB 737-53-1315 R1, except as
required by paragraph (h)(3) of this AD. Do all applicable related
investigative and corrective actions before further flight.
Accomplishing the permanent repair required by this paragraph
terminates the inspections required by paragraph (i)(1) of this AD
for the permanently repaired area only.

(j) Retained AD Provisions for Part 26 Supplemental Inspections, With
No Changes

    This paragraph restates the provisions specified in paragraph
(j) of AD 2017-03-04, with no changes. Table 3 of paragraph 1.E.,
``Compliance,'' of SASB 737-53-1315 R1, specifies post-modification
airworthiness limitation inspections in compliance with 14 CFR
25.571(a)(3) at the modified locations, which support compliance
with 14 CFR 121.1109(c)(2) or 129.109(b)(2). As airworthiness
limitations, these inspections are required by maintenance and
operational rules. It is therefore unnecessary to mandate them in
this AD. Deviations from these inspections require FAA approval, but
do not require an alternative method of compliance.

(k) Retained Skin Panel Replacement, With No Changes

    This paragraph restates the requirements of paragraph (k) of AD
2017-03-04, with no changes. At the later of the times specified in
paragraphs (k)(1) and (k)(2) of this AD: Replace the applicable skin
panels, and do all applicable related investigative and corrective
actions, in accordance with the Accomplishment Instructions of SASB
737-53-1315 R1. Do all applicable related investigative and
corrective actions before further flight. Doing the skin panel
replacement required by this paragraph terminates the inspection
requirements of paragraph (g) of this AD for that skin panel only,
provided the skin panel replacement was done with a production skin
panel at or after 53,000 total flight cycles.
    (1) Before 60,000 total flight cycles, but not before 53,000
total flight cycles.
    (2) Within 6,000 flight cycles after March 28, 2017 (the
effective date of AD 2017-03-04), but not before 53,000 total flight
cycles.

(l) Retained Credit for Previous Actions, With No Changes

    This paragraph restates the credit specified in paragraph (l) of
AD 2017-03-04, with no changes. This paragraph provides credit for
the zone 1 actions required by paragraph (g) of this AD, as
described in SASB 737-53-1315 R1, if the zone 1, 2, and 3 actions,
as described in Boeing Special Attention

Service Bulletin 737-53-1315, dated July 29, 2011, were performed
before March 28, 2017 (the effective date of AD 2017-03-04) using
Boeing Special Attention Service Bulletin 737-53-1315, dated July
29, 2011, except as required by paragraph (h)(4) of this AD. Boeing
Special Attention Bulletin 737-53-1315, dated July 29, 2011, was
incorporated by reference in AD 2012-16-07.

(m) Alternative Methods of Compliance (AMOCs)

    (1) The Manager, Los Angeles 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. In accordance
with 14 CFR 39.19, send your request to your principal inspector or
local Flight Standards District Office, as appropriate. If sending
information directly to the manager of the ACO, send it to the
attention of the person identified in paragraph (n) of this AD.
Information may be emailed to<EMAIL_ADDRESS>    (2) Before using any approved AMOC, notify your appropriate
principal inspector, or lacking a principal inspector, the manager
of the local flight standards district office/certificate holding
district office.
    (3) An AMOC that provides an acceptable level of safety may be
used for any repair, modification, or alteration required by this AD
if it is approved by the Boeing Commercial Airplanes Organization
Designation Authorization (ODA) that has been authorized by the
Manager, Los Angeles ACO, to make those findings. To be approved,
the repair method, modification deviation, or alteration deviation
must meet the certification basis of the airplane, and the approval
must specifically refer to this AD.
    (4) AMOCs approved previously for AD 2012-16-07 are approved as
AMOCs for the corresponding provisions of paragraph (g) of this AD.

(n) Related Information

    For more information about this AD, contact Jennifer
Tsakoumakis, Aerospace Engineer, Airframe Branch, ANM-120L, FAA, Los
Angeles Aircraft Certification Office (ACO), 3960 Paramount
Boulevard, Lakewood, CA 90712-4137; phone:<PHONE_NUMBER>; fax: 562-
627-5210; email<EMAIL_ADDRESS>
(o) Material Incorporated by Reference

    (1) The Director of the Federal Register approved the
incorporation by reference (IBR) of the service information listed
in this paragraph under 5 U.S.C. 552(a) and 1 CFR part 51.
    (2) You must use this service information as applicable to do
the actions required by this AD, unless the AD specifies otherwise.
    (3) The following service information was approved for IBR on
March 28, 2017 (82 FR 11140, February 21, 2017).
    (i) Boeing Special Attention Service Bulletin 737-53-1315,
Revision 1, dated June 30, 2015.
    (ii) Reserved.
    (4) For service information identified in this AD, contact
Boeing Commercial Airplanes, Attention: Contractual & Data Services
(C&DS), 2600 Westminster Blvd., MC 110-SK57, Seal Beach, CA 90740-
5600; telephone<PHONE_NUMBER>; Internet https://www.myboeingfleet.com.
    (5) You may view this service information at the FAA, Transport
Airplane Directorate, 1601 Lind Avenue SW., Renton, WA. For
information on the availability of this material at the FAA, call
425-227-1221.
    (6) You may view this service information that is incorporated
by reference at the National Archives and Records Administration
(NARA). For information on the availability of this material at
NARA, call<PHONE_NUMBER>, or go to: http://www.archives.gov/federal-register/cfr/ibr-locations.html.

    Issued in Renton, Washington, on March 7, 2017.
Michael Kaszycki,
Acting Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 2017-05162 Filed 3-20-17; 8:45 am]
 BILLING CODE 4910-13-P


[Federal Register Volume 79, Number 22 (Monday, February 3, 2014)]
[Notices]
[Pages 6195-6196]
[FR Doc No: 2014-02131]

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DEPARTMENT OF ENERGY

Federal Energy Regulatory Commission

[Docket No. RM98-1-000]

Records Governing Off-the-Record Communications; Public Notice

    This constitutes notice, in accordance with 18 CFR 385.2201(b), of
the receipt of prohibited and exempt off-the-record communications.
    Order No. 607 (64 FR 51222, September 22, 1999) requires Commission
decisional employees, who make or receive a prohibited or exempt off-
the-record communication relevant to the merits of a contested
proceeding, to deliver to the Secretary of the Commission, a copy of
the communication, if written, or a summary of the substance of any
oral communication.
    Prohibited communications are included in a public, non-decisional
file associated with, but not a part of, the decisional record of the
proceeding. Unless the Commission determines that the prohibited
communication and any responses thereto should become a part of the
decisional record, the prohibited off-the-record communication will not
be considered by the Commission in reaching its decision. Parties to a
proceeding may seek the opportunity to respond to any facts or
contentions made in a prohibited off-the-record communication, and may
request that the Commission place the prohibited communication and
responses thereto in the decisional record. The Commission will grant
such a request only when it determines that fairness so requires. Any
person identified below as having made a prohibited off-the-record
communication shall serve the document on all parties listed on the
official service list for the applicable proceeding in accordance with
Rule 2010, 18 CFR 385.2010.
    Exempt off-the-record communications are included in the decisional
record of the proceeding, unless the communication was with a
cooperating agency as described by 40 CFR 1501.6, made under 18 CFR
385.2201(e)(1)(v).
    The following is a list of off-the-record communications recently
received by the Secretary of the Commission. The communications listed
are grouped chronologically, in ascending order. These filings are
available for review at the Commission in the Public Reference Room or
may be viewed on the Commission's Web site at http://www.ferc.gov using
the eLibrary link. Enter the docket number, excluding the last three
digits, in the docket number field to access the document. For
assistance, please contact FERC, Online Support at
<EMAIL_ADDRESS>or toll free at<PHONE_NUMBER>, or for TTY,
contact<PHONE_NUMBER>.

------------------------------------------------------------------------
                                                         Presenter or
           Docket No.                 Filed date          requester
------------------------------------------------------------------------
Prohibited:
    1. CP13-113-000.............            1-16-14  Phyllis S. Johnson.
Exempt:
    1. CP12-29-000..............           11-20-13  FERC Staff. \1\
    2. P-12790-000..............            1-08-14  FERC Staff. \2\
    3. CP13-483-000 CP13-492-000            1-08-14  FERC Staff. \3\
    4. CP13-84-000..............            1-13-14  Hon. Bill Shuster.
    5. CP13-499-000.............            1-15-14  Hon. James L.
                                                      Seward.
    6. P-12796-004..............            1-27-14  Wilma Reip.
------------------------------------------------------------------------
\1\ Telephone record.
\2\ Email record.
\3\ Telephone record.

    Dated: January 27, 2014.
Kimberly D. Bose,
Secretary.
[FR Doc. 2014-02131 Filed 1-31-14; 8:45 am]
BILLING CODE 6717-01-P


P-18-0214-0216 Sanitized Support Documents Index:
 P-18-0214-0216 Sanitized Determination Document (linked)
 P-18-0214 Sanitized CHEM Report (attached)
 P-18-0215 Sanitized CHEM Report (attached)
 P-18-0216 Sanitized CHEM Report (attached)
 P-18-0214 Sanitized ECO Report (attached)
 P-18-0215 Sanitized ECO Report (attached)
 P-18-0216 Sanitized ECO Report (attached)
 P-18-0214 Sanitized ENG Report (attached)
 P-18-0215 Sanitized ENG Report (attached)
 P-18-0216 Sanitized ENG Report (attached)
 P-18-0214 Sanitized EXP Report (attached)
 P-18-0215 Sanitized EXP Report (attached)
 P-18-0216 Sanitized EXP Report (attached)
 P-18-0214 Sanitized Fate Report (attached)
 P-18-0215 Sanitized Fate Report (attached)
 P-18-0216 Sanitized Fate Report (attached)
 P-18-0214-0216 Sanitized HLTH Report_POST-FOCUS FINAL (attached)


[Federal Register Volume 78, Number 43 (Tuesday, March 5, 2013)]
[Notices]
[Page 14316]
[FR Doc No: 2013-04980]

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DEPARTMENT OF HOMELAND SECURITY

Federal Emergency Management Agency

[Internal Agency Docket No. FEMA-3361-EM; Docket ID FEMA-2013-0001]

Connecticut; Amendment No. 1 to Notice of an Emergency
Declaration

AGENCY: Federal Emergency Management Agency, DHS.

ACTION: Notice.

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

SUMMARY: This notice amends the notice of an emergency declaration for
the State of Connecticut (FEMA-3361-EM), dated February 10, 2013, and
related determinations.

DATES: Effective Date: February 11, 2013.

FOR FURTHER INFORMATION CONTACT: Dean Webster, Office of Response and
Recovery, Federal Emergency Management Agency, 500 C Street SW.,
Washington, DC 20472,<PHONE_NUMBER>.

SUPPLEMENTARY INFORMATION: Notice is hereby given that the incident
period for this disaster is closed effective February 11, 2013.

    The following Catalog of Federal Domestic Assistance Numbers
(CFDA) are to be used for reporting and drawing funds: 97.030,
Community Disaster Loans; 97.031, Cora Brown Fund; 97.032, Crisis
Counseling; 97.033, Disaster Legal Services; 97.034, Disaster
Unemployment Assistance (DUA); 97.046, Fire Management Assistance
Grant; 97.048, Disaster Housing Assistance to Individuals and
Households In Presidentially Declared Disaster Areas; 97.049,
Presidentially Declared Disaster Assistance--Disaster Housing
Operations for Individuals and Households; 97.050, Presidentially
Declared Disaster Assistance to Individuals and Households--Other
Needs; 97.036, Disaster Grants--Public Assistance (Presidentially
Declared Disasters); 97.039, Hazard Mitigation Grant.

W. Craig Fugate,
Administrator, Federal Emergency Management Agency.
[FR Doc. 2013-04980 Filed 3-4-13; 8:45 am]
BILLING CODE 9111-23-P


[Federal Register Volume 80, Number 9 (Wednesday, January 14, 2015)]
[Notices]
[Pages 1917-1919]
[FR Doc No: 2015-00442]

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DEPARTMENT OF HEALTH AND HUMAN SERVICES

Food and Drug Administration

[Docket No. FDA-2014-N-1951]

CHEMBIOMED, LTD., Opportunity for a Hearing on a Proposal To
Revoke U.S. License No. 0916

AGENCY: Food and Drug Administration, HHS.

ACTION: Notice.

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

SUMMARY: The Food and Drug Administration (FDA) is announcing an
opportunity for a hearing on a proposal to revoke the biologics license
(U.S. License No. 0916) issued to CHEMBIOMED, LTD. (CHEMBIOMED), for
the manufacture of Anti-A (Murine Monoclonal), Anti-B (Murine
Monoclonal), Anti-Le\a\ (Murine Monoclonal) and Anti-Le\b\ (Murine
Monoclonal). The proposed revocation is based on information that the
firm is no longer in operation and the manufacture of its licensed
products has been discontinued.

DATES: CHEMBIOMED may submit electronic or written requests for a
hearing by February 13, 2015, and any data and information justifying a
hearing by March 16, 2015. Other interested persons may submit
electronic or written comments on the proposed revocation by March 16,
2015.

ADDRESSES: Submit electronic requests for a hearing, any data and
information justifying a hearing, and comments to http://www.regulations.gov. Submit written requests for a hearing, any data
and information justifying a hearing,

and any written comments on the proposed revocation to the Division of
Dockets Management (HFA-305), Food and Drug Administration, 5630
Fishers Lane, rm. 1061, Rockville, MD 20852.

FOR FURTHER INFORMATION CONTACT: John Reilly, Center for Biologics
Evaluation and Research, Food and Drug Administration, 10903 New
Hampshire Ave., Bldg. 71, Rm. 7301, Silver Spring, MD 20993-0002, 240-
402-7911.

SUPPLEMENTARY INFORMATION:

I. Background

    FDA is initiating proceedings to revoke the biologics license (U.S.
License No. 0916) issued to CHEMBIOMED, 9515 107th St., Rm. 401,
Edmonton AB T5K 2C3, Canada, for the manufacture of Anti-A (Murine
Monoclonal), Anti-B (Murine Monoclonal), Anti-Le\a\ (Murine Monoclonal)
and Anti-Le\b\ (Murine Monoclonal). Proceedings to revoke U.S. License
No. 0916 are being initiated under 21 Code of Federal Regulations (CFR)
601.5(b) because FDA has determined through various means that a
meaningful inspection of CHEMBIOMED cannot be conducted because the
manufacturer is no longer in operation. In addition, Health Canada has
advised FDA that CHEMBIOMED is no longer in operation. According to the
Industry Canada Web site (www.ic.gc.ca), CHEMBIOMED (Corporation No.
0228176 and Business No. (BN) 100938521RC0001 under the governing
legislation of the Canada Business Corporations Act) was issued a
Certificate of Incorporation on August 15, 1977, and later was issued a
Certificate of Dissolution on March 17, 1999.
    In a phone conversation that occurred on July 7, 1992, a former
CHEMBIOMED employee informed FDA that CHEMBIOMED was no longer in
business, had ceased the manufacture of licensed products, and had also
ceased shipments of licensed products to the United States.
    In a letter dated June 16, 1995, FDA requested from the Authorized
Official (Responsible Head) of CHEMBIOMED a status update for the
production of all of the products for which CHEMBIOMED held a U.S.
license. This letter requested that the firm notify FDA in writing of
the firm's status and also informed the Authorized Official that in the
absence of a response to this letter that FDA would take action to
revoke CHEMBIOMED's U.S. license. FDA did not receive a response to its
letter dated June 16, 1995.
    In a certified, return-receipt letter dated October 18, 1995, FDA
requested that the Authorized Official of CHEMBIOMED inform FDA whether
or not the firm intended to pursue a product license application
supplement request dated May 6, 1987. In the October 18, 1995 letter,
FDA also informed the Authorized Official that the product license
application supplement request had been placed in the FDA inactive
files. FDA did not receive a response to its certified, return-receipt
letter dated October 18, 1995.
    In a letter to CHEMBIOMED dated December 19, 2012, FDA provided
notice of FDA's intent to revoke U.S. License No. 0916 and announced
its intent to offer an opportunity for a hearing. FDA indicated that
FDA registrations for CHEMBIOMED facilities have not been updated since
May 12, 1994. The letter also advised the Authorized Official that,
under 21 CFR 601.5(b)(1)(i) and (ii) of FDA's regulations, proceedings
for license revocation may be instituted when FDA finds that authorized
FDA employees have been unable to gain access to an establishment for
the purpose of carrying out an inspection, or when the manufacturing of
a product has been discontinued to an extent that a meaningful
inspection cannot be made. The December 19, 2012 letter to CHEMBIOMED,
sent via United Parcel Service (UPS), was returned as undeliverable.

II. Notice of Opportunity for Hearing

    Because FDA has made reasonable efforts to notify CHEMBIOMED of the
proposed revocation and no response has been received from the firm,
FDA is proceeding under 21 CFR 12.21(b) and issuing this notice of
opportunity for a hearing on a proposal to revoke the biologics license
(US. License No. 0916) issued to CHEMBIOMED for the manufacture of
Anti-A (Murine Monoclonal), Anti-B (Murine Monoclonal), Anti-Le\a\
(Murine Monoclonal) and Anti-Le\b\ (Murine Monoclonal).
    FDA has placed copies of the documents relevant to the proposed
revocation on file with the Division of Dockets Management (see
ADDRESSES) under the docket number found in brackets in the heading of
this notice. These documents include the following: (1) A phone
conversation record dated July 7, 1992 between FDA and a former
CHEMBIOMED employee; (2) an FDA letter to the Authorized Official of
CHEMBIOMED dated June 16, 1995; (3) a certified, return-receipt letter
from FDA to the Authorized Official of CHEMBIOMED dated October 18,
1995; (4) a UPS Express Mail, signature required letter from FDA to the
Authorized Official of CHEMBIOMED, dated December 19, 2012, and
returned as undeliverable; and (5) Industry Canada information that
documents CHEMBIOMED, Corporation No. 0228176 and BN 100938521RC0001
under the governing legislation of the Canada Business Corporations
Act, was issued a Certificate of Incorporation on August 15, 1977, and
later was issued a Certificate of Dissolution on March 17, 1999. These
documents are available for public examination in the Division of
Dockets Management between 9 a.m. and 4 p.m., Monday through Friday,
and will be posted to the docket at http://www.regulations.gov.
    CHEMBIOMED may submit an electronic or written request for a
hearing to the Division of Dockets Management by February 13, 2015, and
any data and information justifying a hearing to the Division of
Dockets Management by March 16, 2015. Other interested persons may
submit electronic or written comments on the proposed license
revocation to the Division of Dockets Management by March 16, 2015. The
failure of the licensee, CHEMBIOMED, to file a timely electronic or
written request for a hearing constitutes an election by the licensee
not to avail itself of the opportunity for a hearing concerning the
proposed license revocation (Sec.  12.22(b)).
    FDA's procedures and requirements governing a notice of opportunity
for a hearing, notice of appearance and request for a hearing, grant or
denial of a hearing, and submission of data and information to justify
a hearing on a proposed revocation of a license are contained in 21 CFR
parts 12 and 601. A request for a hearing may not rest on mere
allegations or denials, but must set forth a genuine and substantial
issue of fact that requires a hearing (Sec.  12.24(b)). If it
conclusively appears from the face of the data, information, and
factual analyses submitted in support of the request for a hearing that
there is no genuine and substantial issue of fact for resolution at a
hearing, the Commissioner of Food and Drugs (the Commissioner) will
deny the hearing request, making findings and conclusions that justify
the denial (Sec.  12.24(b)(3)).
    Only one copy of any submission need be provided to FDA.
Submissions are to be identified with the docket number found in
brackets in the heading of this document. Such submissions, except for
data and information prohibited from public disclosure under 21 CFR
10.20(j)(2)(i), 21 U.S.C. 331(j) or 18 U.S.C. 1905, may be examined in
the Division of Dockets

Management (see ADDRESSES) between 9 a.m. and 4 p.m., Monday through
Friday and will be posted to the docket at  http://www.regulations.gov.
    This notice is issued under section 351 of the Public Health
Service Act (42 U.S.C. 262) and sections 201, 501, 502, 505, and 701 of
the Federal Food, Drug, and Cosmetic Acts (21 U.S.C. 321, 351, 352,
355, and 371), and under the authority delegated to the Commissioner
and redelegated to the Director and Deputy Director of the Center for
Biologics Evaluation and Research (FDA Staff Manual Guide 1410.203).

    Dated: January 9, 2015.
Leslie Kux,
Associate Commissioner for Policy.
[FR Doc. 2015-00442 Filed 1-13-15; 8:45 am]
BILLING CODE 4164-01-P


[Federal Register Volume 80, Number 212 (Tuesday, November 3, 2015)]
[Notices]
[Pages 67818-67819]
[FR Doc No: 2015-27905]

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

SECURITIES AND EXCHANGE COMMISSION

[Extension: Rule 17Ad-16; SEC File No. 270-363, OMB Control No. 3235-
0413]

Proposed Collection; Comment Request

Upon Written Request, Copies Available From: Securities and Exchange
Commission, Office of FOIA Services, 100 F Street NE., Washington, DC
20549-2736.

    Notice is hereby given that, pursuant to the Paperwork Reduction
Act of 1995 (44 U.S.C. 3501 et seq.) (``PRA''), the Securities and
Exchange Commission (``Commission'') is soliciting comments on the
existing collection of information

provided for in Rule 17Ad-16 (17 CFR 240.17Ad-16) under the Securities
Exchange Act of 1934 (15 U.S.C. 78a et seq.). The Commission plans to
submit this existing collection of information to the Office of
Management and Budget (``OMB'') for extension and approval.
    Rule 17Ad-16 requires a registered transfer agent to provide
written notice to the appropriate qualified registered securities
depository when assuming or terminating transfer agent services on
behalf of an issuer or when changing its name or address. In addition,
transfer agents that provide such notice shall maintain such notice for
a period of at least two years in an easily accessible place. This rule
addresses the problem of certificate transfer delays caused by transfer
requests that are directed to the wrong transfer agent or the wrong
address.
    We estimate that the transfer agent industry submits 6,970 Rule
17Ad-16 notices to appropriate qualified registered securities
depositories. The staff estimates that the average amount of time
necessary to create and submit each notice is approximately 15 minutes
per notice. Accordingly, the estimated total industry burden is 1,743
hours per year (15 minutes multiplied by 6,970 notices filed annually).
    Because the information needed by transfer agents to properly
notify the appropriate registered securities depository is readily
available to them and the report is simple and straightforward, the
cost is relatively minimal. The average internal compliance cost to
prepare and send a notice is approximately $7.50 (15 minutes at $30 per
hour). This yields an industry-wide internal compliance cost estimate
of $52,275 (6,970 notices multiplied by $7.50 per notice).
    Written comments are invited on: (a) whether the proposed
collection of information is necessary for the proper performance of
the functions of the Commission, including whether the information
shall have practical utility; (b) the accuracy of the Commission's
estimates of the burden of the proposed collection of information; (c)
ways to enhance the quality, utility, and clarity of the information
collected; and (d) ways to minimize the burden of the collection of
information on respondents, including through the use of automated
collection techniques or other forms of information technology.
Consideration will be given to comments and suggestions submitted in
writing within 60 days of this publication.
    An agency may not conduct or sponsor, and a person is not required
to respond to, a collection of information under the PRA unless it
displays a currently valid OMB control number.
    Please direct your written comments to: Pamela Dyson, Director/
Chief Information Officer, Securities and Exchange Commission, c/o Remi
Pavlik-Simon, 100 F Street NE., Washington, DC 20549, or send an email
to<EMAIL_ADDRESS>
    Dated: October 28, 2015.
Robert W. Errett,
Deputy Secretary.
[FR Doc. 2015-27905 Filed 11-2-15; 8:45 am]
 BILLING CODE 8011-01-P


[Federal Register: December 2, 2009 (Volume 74, Number 230)]
[Rules and Regulations]
[Page 63063-63066]
[DOCID:fr02de09-2]

=======================================================================
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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2009-0915; Directorate Identifier 2009-NM-224-AD;
Amendment 39-16049; AD 2009-21-10]
RIN 2120-AA64

Airworthiness Directives; AVOX Systems and B/E Aerospace Oxygen
Cylinder Assemblies, as Installed on Various Transport Airplanes

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Final rule; request for comments.

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

SUMMARY: We are adopting a new airworthiness directive (AD) for certain
AVOX Systems and B/E Aerospace oxygen cylinder assemblies, as installed
on various transport airplanes. This AD requires removing certain
oxygen cylinder assemblies from the airplane. This AD was prompted by
the reported rupture of a high-pressure gaseous oxygen cylinder, which
had insufficient strength characteristics due to improper heat
treatment. We are issuing this AD to prevent an oxygen cylinder from
rupturing, which, depending on the location, could result in structural
damage and rapid decompression of the airplane, damage to adjacent
essential flight equipment, deprivation of the necessary oxygen supply
for the flightcrew, and injury to cabin occupants or maintenance or
other support personnel.

DATES: This AD is effective December 17, 2009.
    We must receive comments on this AD by January 19, 2010.

ADDRESSES: You may send comments by any of the following methods:
     Federal eRulemaking Portal: Go to http://
www.regulations.gov. Follow the instructions for submitting comments.
     Fax:<PHONE_NUMBER>.
     Mail: U.S. Department of Transportation, Docket
Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New
Jersey Avenue, SE., Washington, DC 20590.
     Hand Delivery: U.S. Department of Transportation, Docket
Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New
Jersey Avenue, SE.,

Washington, DC 20590, between 9 a.m. and 5 p.m., Monday through Friday,
except Federal holidays.

Examining the AD Docket

    You may examine the AD docket on the Internet at http://
www.regulations.gov; or in person at the Docket Management Facility
between 9 a.m. and 5 p.m., Monday through Friday, except Federal
holidays. The AD docket contains this AD, the regulatory evaluation,
any comments received, and other information. The street address for
the Docket Office (telephone<PHONE_NUMBER>) is in the ADDRESSES section.
Comments will be available in the AD docket shortly after receipt.

FOR FURTHER INFORMATION CONTACT: Robert Hettman, Aerospace Engineer,
Cabin Safety and Environmental Systems Branch, ANM-150S, Seattle
Aircraft Certification Office, FAA, 1601 Lind Avenue, SW., Renton,
Washington 98057-3356; telephone<PHONE_NUMBER>; fax<PHONE_NUMBER>.

SUPPLEMENTARY INFORMATION:

Discussion

    During routine hydrostatic testing, a United States Department of
Transportation Type 3HT-1850 high-pressure gaseous oxygen cylinder
ruptured under what would be considered normal operating conditions.
Further investigation indicates that the cylinder had insufficient
strength characteristics due to improper heat treatment. The improper
heat treatment is limited to specific production batches, but the
affected oxygen cylinders may be installed on various transport
airplanes and aircraft certificated in other categories. The oxygen
cylinders contain gaseous oxygen under high pressure. Rupture of an
oxygen cylinder, depending on its location, could result in structural
damage and rapid decompression of the airplane, damage to adjacent
essential flight equipment, deprivation of the necessary oxygen supply
for the flightcrew, and injury to cabin occupants or maintenance or
other support personnel.

FAA's Determination and Requirements of This AD

    Certain affected airplanes have been approved by the aviation
authorities of other countries, and are approved for operation in the
United States.
    We are issuing this AD because we evaluated all the relevant
information and determined the unsafe condition described previously is
likely to exist or develop in other products of these same type
designs. This AD requires removing the affected oxygen cylinder
assemblies from transport airplanes.

Related Rulemaking

    The FAA is currently evaluating the risk associated with these
oxygen cylinder assemblies installed on aircraft certificated in other
categories to determine whether any action is necessary to address the
unsafe condition on these aircraft.

FAA's Justification and Determination of the Effective Date

    This AD addresses the consequences of the potential rupture of
certain oxygen cylinder assemblies. Because of our requirement to
promote safe flight of civil aircraft and thus the critical need to
ensure the proper functioning of the oxygen cylinders and the short
compliance time involved with this action, this AD must be issued
immediately.
    Because an unsafe condition exists that requires the immediate
adoption of this AD, we find notice and opportunity for prior public
comment hereon are impracticable and that good cause exists for making
this amendment effective in less than 30 days.

Comments Invited

    This AD is a final rule that involves requirements affecting flight
safety, and we did not provide you with notice and an opportunity to
provide your comments before it becomes effective. However, we invite
you to send any written data, views, or arguments about this AD. Send
your comments to an address listed under the ADDRESSES section. Include
``Docket No. FAA-2009-0915; Directorate Identifier 2009-NM-224-AD'' at
the beginning of your comments. We specifically invite comments on the
overall regulatory, economic, environmental, and energy aspects of this
AD. We will consider all comments received by the closing date and may
amend this AD because of those comments.
    We will post all comments we receive, without change, to http://
www.regulations.gov, including any personal information you provide. We
will also post a report summarizing each substantive verbal contact we
receive about this AD.

Authority for This Rulemaking

    Title 49 of the United States Code specifies the FAA's authority to
issue rules on aviation safety. Subtitle I, section 106, describes the
authority of the FAA Administrator. ``Subtitle VII: Aviation
Programs,'' describes in more detail the scope of the Agency's
authority.
    We are issuing this rulemaking under the authority described in
``Subtitle VII, Part A, Subpart III, Section 44701: General
requirements.'' Under that section, Congress charges the FAA with
promoting safe flight of civil aircraft in air commerce by prescribing
regulations for practices, methods, and procedures the Administrator
finds necessary for safety in air commerce. This regulation is within
the scope of that authority because it addresses an unsafe condition
that is likely to exist or develop on products identified in this
rulemaking action.

Regulatory Findings

    This AD will not have federalism implications under Executive Order
13132. This AD will not have a substantial direct effect 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.
    For the reasons discussed above, I certify that this AD:
    (1) Is not a ``significant regulatory action'' under Executive
Order 12866,
    (2) Is not a ``significant rule'' under DOT Regulatory Policies and
Procedures (44 FR 11034, February 26, 1979), and
    (3) Will not have a significant economic impact, positive or
negative, on a substantial number of small entities under the criteria
of the Regulatory Flexibility Act.
    You can find our regulatory evaluation and the estimated costs of
compliance in the AD Docket.

List of Subjects in 14 CFR Part 39

    Air transportation, Aircraft, Aviation safety, Safety.

Adoption of the Amendment

0
Accordingly, under the authority delegated to me by the Administrator,
the FAA amends 14 CFR part 39 as follows:

PART 39--AIRWORTHINESS DIRECTIVES

0
1. The authority citation for part 39 continues to read as follows:

    Authority: 49 U.S.C. 106(g), 40113, 44701.

Sec.  39.13  [Amended]

0
2. The FAA amends Sec.  39.13 by adding the following new AD:

2009-21-10 AVOX Systems and B/E Aerospace: Amendment 39-16049.
Docket No. FAA-2009-0915; Directorate Identifier 2009-NM-224-AD.

Effective Date

    (a) This airworthiness directive (AD) is effective December 17,
2009.

Affected ADs

    (b) None.

Applicability

    (c) This AD applies to the oxygen cylinder assemblies, approved
under United States Department of Transportation Regulations for
Type 3HT cylinders, identified in Table 1 of this AD. These oxygen
cylinder assemblies may be installed on various transport airplanes,
certificated in any category, identified in but not limited to the
airplanes included in Table 2 of this AD.

         Table 1--Affected Oxygen Cylinder Assembly Part Numbers
------------------------------------------------------------------------
                  Manufacturer                           Part Nos.
------------------------------------------------------------------------
AVOX Systems....................................  *6350A34 series,
                                                   800112-03, 800112-10,
                                                   800112-13, 801293-03,
                                                   801307-00, 801307-01,
                                                   801307-02, 801307-03,
                                                   801307-07, 801307-09,
                                                   801307-23, 801307-24,
                                                   801365-04, 801365-14,
                                                   801375-00, 801977-05,
                                                   *8915 series.
                                                  (*For example, 6350A34-
                                                   X-X or 8915XX-XX,
                                                   where ``X'' denotes a
                                                   part number digit).
B/E Aerospace...................................  B43570-3, B43570-5,
                                                   176018-115, 176112-
                                                   115, 176177-115,
                                                   176181-115, 176529-
                                                   97.
------------------------------------------------------------------------

                       Table 2--Affected Airplanes
------------------------------------------------------------------------
                  Manufacturer                             Model
------------------------------------------------------------------------
Airbus..........................................  A300 B4-620, B4-622,
                                                   B4-605R, and F4-605R
                                                   airplanes.
                                                  A310-203, -204, -221,
                                                   222, -304, and -324
                                                   airplanes.
                                                  A318-111 and -112
                                                   airplanes.
                                                  A319-111, -112, -113,
                                                   114, -115, -131, -
                                                   132, and -133
                                                   airplanes.
                                                  A320-111, -211, -212,
                                                   214, -231, -232, and
                                                   233 airplanes.
                                                  A321-111, -112, -131,
                                                   211, and -231
                                                   airplanes.
                                                  A330-301, -321, and -
                                                   322 airplanes.
                                                  A340-211 and -212
                                                   airplanes.
                                                  A340-311 and -312
                                                   airplanes.
The Boeing Company..............................  707-100 long body, -
                                                   200, -100B long body,
                                                   and -100B short body
                                                   series airplanes; and
                                                   707-300, -300B, -
                                                   300C, and -400 series
                                                   airplanes.
                                                  727, 727C, 727-100,
                                                   727 -100C, 727-200,
                                                   and 727-200F series
                                                   airplanes.
                                                  737-100, -200, -200C,
                                                   300, -400, -500, -
                                                   600, -700, -700C, -
                                                   800, -900, and -900ER
                                                   series airplanes.
                                                  747-100, 747-100B, 747-
                                                   100B SUD, 747-200B,
                                                   747-200C, 747-200F,
                                                   747-300, 747-400, 747-
                                                   400D, 747-400F,
                                                   747SR, and 747SP
                                                   series airplanes.
                                                  757-200, -200PF, -
                                                   200CB, and -300
                                                   series airplanes.
                                                  767-200, -300, -300F,
                                                   and -400ER series
                                                   airplanes.
                                                  777-200, -200LR, -300,
                                                   -300ER, and 777F
                                                   series airplanes.
Gulfstream Aerospace Company....................  G-IV airplanes.
McDonnell Douglas Corporation...................  DC-8-11, DC-8-12, DC-8-
                                                   21, DC-8-31, DC-8-32,
                                                   DC-8-33, DC-8-41, DC-
                                                   8-42, DC-8-43, DC-8-
                                                   51, DC-8-52, DC-8-53,
                                                   and DC-8-55
                                                   airplanes.
                                                  DC-9-11, DC-9-12, DC-9-
                                                   13, DC-9-14, DC-9-15,
                                                   DC-9-15F, DC-9-21, DC-
                                                   9-31, DC-9-32, DC-9-
                                                   32 (VC-9C), DC-9-32F,
                                                   DC-9-32F (C-9A, C-
                                                   9B), DC-9-33F, DC-9-
                                                   34, DC-9-34F, DC-9-
                                                   41, DC-9-51, DC-9-81
                                                   (MD-81), DC-9-82 (MD-
                                                   82), DC-9-83 (MD-83),
                                                   and DC-9-87 (MD-87)
                                                   airplanes.
                                                  DC-10-10, DC-10-10F,
                                                   DC-10-15, DC-10-30,
                                                   DC-10-30F (KC-10A and
                                                   KDC-10), and DC-10-40
                                                   airplanes.
                                                  MD-10-10F and MD-10-
                                                   30F airplanes.
                                                  MD-11 and MD-11F
                                                   airplanes.
                                                  MD-88 airplanes.
                                                  MD-90-30 airplanes.
Short Brothers..................................  SD3-30, SD3-SHERPA,
                                                   and SD3-60 SHERPA
                                                   airplanes.
------------------------------------------------------------------------

Subject

    (d) Air Transport Association (ATA) of America Code 35: Oxygen.

Unsafe Condition

    (e) This AD was prompted by the reported rupture of a high-
pressure gaseous oxygen cylinder, which had insufficient strength
characteristics due to improper heat treatment. The Federal Aviation
Administration is issuing this AD to prevent an oxygen cylinder from
rupturing, which, depending on the location, could result in
structural damage and rapid decompression of the airplane, damage to
adjacent essential flight equipment, deprivation of the necessary
oxygen supply for the flightcrew, and injury to cabin occupants or
maintenance or other support personnel.

Compliance

    (f) You are responsible for having the actions required by this
AD performed within the compliance times specified, unless the
actions have already been done.

Inspection

    (g) Within 90 days after the effective date of this AD, inspect
to determine the serial number of the oxygen cylinder assemblies
installed in the airplane. The serial number is stamped into the
steel cylinder near the neck. A review of airplane records is
acceptable in lieu of this inspection if the serial numbers of the
oxygen cylinder assemblies can be conclusively determined from that
review. For any oxygen cylinder assembly that has a serial number
identified in Table 3 of this AD: Remove it from the airplane before
further flight.

        Table 3--Affected Oxygen Cylinder Assembly Serial Numbers
------------------------------------------------------------------------
              Cylinder manufacturer                Affected serial Nos.
------------------------------------------------------------------------
AVOX Systems....................................  ST82307 through
                                                   ST82309 inclusive.
                                                  ST82335 through
                                                   ST82378 inclusive.
                                                  ST82385 through
                                                   ST82506 inclusive,
                                                   except for S/N
                                                   ST82498, which
                                                   ruptured.
                                                  ST82550 through
                                                   ST82606 inclusive.
                                                  ST82617 through
                                                   ST82626 inclusive.
                                                  ST83896 through
                                                   ST83905 inclusive.
                                                  ST84209 through
                                                   ST84218 inclusive.
                                                  ST84224 through
                                                   ST84236 inclusive.
                                                  ST86138, ST86143,
                                                   ST86145, ST86150,
                                                   ST86169, ST86172,
                                                   ST86177.
                                                  ST86299 through
                                                   ST86307 inclusive.
B/E Aerospace...................................  K495120 through
                                                   K495121 inclusive.
                                                  K617383 through
                                                   K617423 inclusive.
                                                  K629573 through
                                                   K629577 inclusive.
                                                  K674451 through
                                                   K674455 inclusive.
                                                  K757064 through
                                                   K757066 inclusive.
------------------------------------------------------------------------

Parts Installation

    (h) As of the effective date of this AD, no person may install,
on any airplane, a United States Department of Transportation Type
3HT oxygen cylinder assembly that has a part number identified in
Table 1 of this AD and a serial number identified in Table 3 of this
AD.

Alternative Methods of Compliance (AMOCs)

    (i)(1) The Manager, Seattle Aircraft Certification Office, FAA,
has the authority to approve AMOCs for this AD, if requested using
the procedures found in 14 CFR 39.19. Send information to Attn:
Robert Hettman, Aerospace Engineer, Cabin Safety and Environmental
Systems Branch, ANM-150S, Seattle Aircraft Certification Office,
FAA, 1601 Lind Avenue, SW., Renton, Washington 98057-3356; telephone
(425) 917-6457; fax<PHONE_NUMBER>. Or, e-mail information to 9-ANM-
<EMAIL_ADDRESS>    (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 refer to this AD.

Material Incorporated by Reference

    (j) None.

    Issued in Renton, Washington, on November 25, 2009.
Ali Bahrami,
Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. E9-28807 Filed 12-1-09; 8:45 am]

BILLING CODE 4910-13-P


[Federal Register Volume 87, Number 107 (Friday, June 3, 2022)]
[Notices]
[Pages 33772-33773]
[FR Doc No: 2022-11932]

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

DEPARTMENT OF ENERGY

Federal Energy Regulatory Commission

Combined Notice of Filings

    Take notice that the Commission has received the following Natural
Gas Pipeline Rate and Refund Report filings:

Filings Instituting Proceedings

    Docket Numbers: PR22-45-000.
    Applicants: Targa SouthTex Mustang Transmission Ltd.
    Description: Sec.  284.123 Rate Filing: 311 Statement of Operating
Conditions to be effective 5/26/2022.
    Filed Date: 5/26/22.

    Accession Number: 20220526-5121.
    Comments/Protests Due: 5 p.m. ET 6/16/22.

    Docket Numbers: PR22-46-000.
    Applicants: Targa SouthTex Transmission LP.
    Description: Sec.  284.123 Rate Filing: 311 Statement of Operating
Conditions to be effective 5/26/2022.
    Filed Date: 5/26/22.
    Accession Number: 20220526-5123.
    Comments/Protests Due: 5 p.m. ET 6/16/22.

    Docket Numbers: RP22-933-000.
    Applicants: TransColorado Gas Transmission Company LLC.
    Description: Sec.  4(d) Rate Filing: Qtrly FL&U Update to be
effective 7/1/2022.
    Filed Date: 5/26/22.
    Accession Number: 20220526-5023.
    Comment Date: 5 p.m. ET 6/7/22.

    Docket Numbers: RP22-934-000.
    Applicants: Gulfstream Natural Gas System, L.L.C.
    Description: Sec.  4(d) Rate Filing: Negotiated Rate--Amended
Central Fl Gas 9000107 to be effective 6/1/2022.
    Filed Date: 5/26/22.
    Accession Number: 20220526-5027.
    Comment Date: 5 p.m. ET 6/7/22.

    Docket Numbers: RP22-935-000.
    Applicants: Colorado Interstate Gas Company, L.L.C.
    Description: Sec.  4(d) Rate Filing: Fuel and Lost Unaccounted For
to be effective 7/1/2022.
    Filed Date: 5/26/22.
    Accession Number: 20220526-5045.
    Comment Date: 5 p.m. ET 6/7/22.

    Docket Numbers: RP22-936-000.
    Applicants: El Paso Natural Gas Company, L.L.C.
    Description: Sec.  4(d) Rate Filing: Negotiated Rate Agreement
Update (SoCal Jun-Aug 2022) to be effective 6/1/2022.
    Filed Date: 5/26/22.
    Accession Number: 20220526-5112.
    Comment Date: 5 p.m. ET 6/7/22.

    Docket Numbers: RP22-937-000.
    Applicants: Wyoming Interstate Company, L.L.C.
    Description: Sec.  4(d) Rate Filing: Transportation Agreement
Filing (Continental Replacment TSA) to be effective 6/1/2022.
    Filed Date: 5/26/22.
    Accession Number: 20220526-5120.
    Comment Date: 5 p.m. ET 6/7/22.

    Docket Numbers: RP22-938-000.
    Applicants: El Paso Natural Gas Company, L.L.C.
    Description: Sec.  4(d) Rate Filing: Non-Conforming Agreements
Update (SRP) to be effective 6/1/2022.
    Filed Date: 5/26/22.
    Accession Number: 20220526-5193.
    Comment Date: 5 p.m. ET 6/7/22.

    Docket Numbers: RP22-939-000.
    Applicants: Caledonia Energy Partners, L.L.C.
    Description: Compliance filing: Caledonia Energy Notice of Change
in Circumstances to be effective N/A.
    Filed Date: 5/26/22.
    Accession Number: 20220526-5235.
    Comment Date: 5 p.m. ET 6/7/22.

    Docket Numbers: RP22-940-000.
    Applicants: Freebird Gas Storage, L.L.C.
    Description: Compliance filing: Freebird Gas Storage Notice of
Change in Circumstances to be effective N/A.
    Filed Date: 5/26/22.
    Accession Number: 20220526-5239.
    Comment Date: 5 p.m. ET 6/7/22.

    Docket Numbers: RP22-941-000.
    Applicants: Mississippi Hub, LLC.
    Description: Compliance filing: Mississippi Hub Notice of Change in
Circumstances to be effective N/A.
    Filed Date: 5/26/22.
    Accession Number: 20220526-5240.
    Comment Date: 5 p.m. ET 6/7/22.

    Any person desiring to intervene or protest in any of the above
proceedings must file in accordance with Rules 211 and 214 of the
Commission's Regulations (18 CFR 385.211 and 385.214) on or before 5:00
p.m. Eastern time on the specified comment date. Protests may be
considered, but intervention is necessary to become a party to the
proceeding.
    The filings are accessible in the Commission's eLibrary system
(https://elibrary.ferc.gov/idmws/search/fercgensearch.asp) by querying
the docket number.
    eFiling is encouraged. More detailed information relating to filing
requirements, interventions, protests, service, and qualifying
facilities filings can be found at: http://www.ferc.gov/docs-filing/efiling/filing-req.pdf. For other information, call<PHONE_NUMBER>
(toll free). For TTY, call<PHONE_NUMBER>.

    Dated: May 27, 2022.
Debbie-Anne A. Reese,
Deputy Secretary.
[FR Doc. 2022-11932 Filed 6-2-22; 8:45 am]
BILLING CODE 6717-01-P


[Federal Register Volume 80, Number 249 (Tuesday, December 29, 2015)]
[Proposed Rules]
[Pages 81233-81234]
[FR Doc No: 2015-32686]

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

DEPARTMENT OF HEALTH AND HUMAN SERVICES

Food and Drug Administration

21 CFR Part 1271

[Docket No. FDA-2015-D-3719]

Draft Guidances Relating to the Regulation of Human Cells,
Tissues, or Cellular or Tissue-Based Products; Public Hearing; Request
for Comments; Correction

AGENCY: Food and Drug Administration, HHS.

ACTION: Notification of public hearing; request for comments;
correction.

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

SUMMARY: The Food and Drug Administration (FDA or Agency) is correcting
a notification of a public hearing entitled ``Draft Guidances Relating
to the Regulation of Human Cells, Tissues, or Cellular or Tissue-Based
Products; Public Hearing; Request for Comments'' that appeared in the
Federal Register of October 30, 2015 (80 FR 66845). The document
announced a public hearing to obtain input on four recently issued
draft guidances relating to the regulation of human cells, tissues, or
cellular or tissue-based products (HCT/Ps). The document published with
conflicting information about who must register for the public hearing.
This document corrects that error.

FOR FURTHER INFORMATION CONTACT: Lori Jo Churchyard, Center for
Biologics Evaluation and Research, Food and Drug Administration, 10903
New Hampshire Ave., Bldg. 71, Rm. 7301, Silver Spring, MD 20993, 240-
402-7911.

SUPPLEMENTARY INFORMATION: In FR Doc. 2015-27703, appearing on pages
66845 and 66847 in the Federal Register of Friday, October 30, 2015,
the following corrections are made:
    1. On page 66845, in the third column under DATES, the third
sentence is revised to read: ``Persons seeking to attend (including FDA
employees) or to present at the public hearing must register by January
8, 2016.''
    2. On page 66847, in the first column under section IV. Attendance
and Registration, the third sentence is revised to read: ``Individuals
who wish to attend (including FDA employees) or present at the public
hearing must

register by sending an email to<EMAIL_ADDRESS>on or
before January 8, 2016, and provide complete contact information,
including name, title, affiliation, address, email, and phone number.''

    Dated: December 21, 2015.
Leslie Kux,
Associate Commissioner for Policy.
[FR Doc. 2015-32686 Filed 12-28-15; 8:45 am]
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[Federal Register Volume 76, Number 20 (Monday, January 31, 2011)]
[Notices]
[Pages 5411-5412]
[FR Doc No: 2011-2159]

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SECURITIES AND EXCHANGE COMMISSION

[File No. 500-1]

Clean Energy and Power, Inc., Order of Suspension of Trading

January 27, 2011.
    It appears to the Securities and Exchange Commission that there is
a lack of current and accurate information concerning the securities of
Clean Energy and Power, Inc. (``Clean Energy'') because it has not
filed any periodic reports since the period ended September 30, 2007.
Clean Energy is quoted on the Pink Sheets operated by OTC Markets Group
Inc. under the ticker symbol KEPI.
    The Commission is of the opinion that the public interest and the
protection of investors require a suspension of trading

in the securities of the above-listed company, and any equity
securities of any entity purporting to succeed to this issuer.
    Therefore, it is ordered, pursuant to Section 12(k) of the
Securities Exchange Act of 1934, that trading in the securities of the
above-listed company, and any equity securities of any entity
purporting to succeed to this issuer, is suspended for the period from
9:30 a.m. EST on January 27, 2011, through 11:59 p.m. EST on February
9, 2011.

    By the Commission.
Elizabeth M. Murphy,
Secretary.
[FR Doc. 2011-2159 Filed 1-27-11; 4:15 pm]
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