Airworthiness Directives; Airbus Airplanes, 51097-51100 [2016-18174]
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Federal Register / Vol. 81, No. 149 / Wednesday, August 3, 2016 / Rules and Regulations
deployment as a result of wear and tear,
or inertial loads resulting from in-flight
or ground maneuvers (including gusts
and hard landings), and other operating
and environmental conditions
(vibrations, moisture, etc.) likely to
occur in service.
3. Deployment of the leg-flail airbag
system must not introduce injury
mechanisms to the seated occupant, or
result in injuries that could impede
rapid egress.
4. Inadvertent deployment of the legflail airbag system, during the most
critical part of the flight, must either
meet the requirement of § 25.1309(b), or
not cause a hazard to the airplane or its
occupants. This also includes
preventing inadvertent airbag
deployment from a static discharge.
5. The leg-flail airbag system must not
impede rapid egress of occupants from
the airplane 10 seconds after airbag
deployment.
6. The leg-flail airbag system must be
protected from lightning and highintensity radiated fields (HIRF). The
threats to the airplane specified in
existing regulations regarding lightning
(§ 25.1316) and HIRF (§ 25.1317) are
incorporated by reference for the
purpose of measuring lightning and
HIRF protection.
7. The leg-flail airbag system must
function properly after loss of normal
airplane electrical power, and after a
transverse separation of the fuselage at
the most critical location. A separation
at the location of the leg-flail airbag
system does not have to be considered.
8. The leg-flail airbag system must not
release hazardous quantities of gas,
sharp injurious metal fragments, or
particulate matter into the cabin.
9. The leg-flail airbag system
installation must be protected from the
effects of fire such that no hazard to
occupants will result.
10. A means must be available to
verify the integrity of the leg-flail airbag
system’s activation system prior to each
flight, or the leg-flail airbag system’s
activation system must reliably operate
between inspection intervals. The FAA
considers that the loss of the leg-flail
airbag system’s deployment function
alone (i.e., independent of the
conditional event that requires the legflail airbag system’s deployment) is a
major-failure condition.
11. The airbag inflatable material may
not have an average burn rate of greater
than 2.5 inches per minute when tested
using the horizontal flammability test
defined in part 25, appendix F, part I,
paragraph (b)(5).
12. The leg-flail airbag system, once
deployed, must not adversely affect the
emergency-lighting system (i.e., block
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floor-proximity lights to the extent that
the lights no longer meet their intended
function).
Issued in Renton, Washington, on July 26,
2016.
Victor Wicklund,
Acting Manager, Transport Airplane
Directorate, Aircraft Certification Service.
[FR Doc. 2016–18398 Filed 8–2–16; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2016–3983; Directorate
Identifier 2015–NM–009–AD; Amendment
39–18582; AD 2016–14–01]
RIN 2120–AA64
Airworthiness Directives; Airbus
Airplanes
Federal Aviation
Administration (FAA), DOT.
ACTION: Final rule; correction.
AGENCY:
The FAA is correcting an
airworthiness directive (AD) that
published in the Federal Register. That
AD applies to certain Airbus Model
A330–200 Freighter series airplanes;
Model A330–200 and A330–300 series
airplanes; Model A340–200 and A340–
300 series airplanes; Model A340–500
series airplanes; and Model A340–600
series airplanes. Table 1 to paragraph (j)
of the regulatory text contains
typographical errors regarding certain
part numbers (P/Ns). This document
corrects those errors. In all other
respects, the original document remains
the same.
DATES: This final rule is effective August
16, 2016.
The Director of the Federal Register
approved the incorporation by reference
of certain publications listed in this AD
as of August 16, 2016 (81 FR 44983, July
12, 2016).
ADDRESSES: For Airbus service
information identified in this final rule,
contact Airbus SAS, Airworthiness
Office—EAL, 1 Rond Point Maurice
Bellonte, 31707 Blagnac Cedex, France;
telephone +33 5 61 93 36 96; fax +33 5
61 93 45 80; email airworthiness.A330A340@airbus.com; Internet https://
www.airbus.com.
For Hamilton Sundstrand service
information identified in this final rule,
contact Hamilton Sundstrand, Technical
Publications, Mail Stop 302–9, 4747
Harrison Avenue, P.O. Box 7002,
Rockford, IL 61125–7002; telephone
860–654–3575; fax 860–998–4564; email
SUMMARY:
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51097
tech.solutions@hs.utc.com; Internet
https://www.hamiltonsundstrand.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 425–227–1221. It is also
available on the Internet at https://
www.regulations.gov by searching for
and locating Docket No. FAA–2016–
3983.
Examining the AD Docket
You may examine the AD docket on
the Internet at https://
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 address for the
Docket Office (phone: 800–647–5527) is
Docket Management Facility, U.S.
Department of Transportation, Docket
Operations, M–30, West Building
Ground Floor, Room W12–140, 1200
New Jersey Avenue SE., Washington,
DC 20590.
FOR FURTHER INFORMATION CONTACT:
Vladimir Ulyanov, Aerospace Engineer,
International Branch, ANM–116,
Transport Airplane Directorate, FAA,
1601 Lind Avenue SW., Renton, WA
98057–3356; telephone 425–227–1138;
fax 425–227–1149.
SUPPLEMENTARY INFORMATION:
Airworthiness Directive 2016–14–01,
Amendment 39–18582 (81 FR 44983,
July 12, 2016) (‘‘AD 2016–14–01’’),
currently requires identification of the
manufacturer, part number, and serial
number of the ram air turbine (RAT),
and re-identification and modification
of the RAT if necessary, for certain
Airbus Model A330–200 Freighter series
airplanes; Model A330–200 and A330–
300 series airplanes; Model A340–200
and A340–300 series airplanes; Model
A340–500 series airplanes; and Model
A340–600 series airplanes.
Need for the Correction
As published, table 1 to paragraph (j)
of the regulatory text contains
typographical errors in two part
numbers. Table 1 to paragraph (j) of the
AD incorrectly refers to RAT P/Ns
1720934C and 1720934D. Those part
numbers should have been 1702934C
and 1702934D.
Related Service Information Under 1
CFR Part 51
Airbus has issued the following
service information, which describes
procedures for identifying the supplier,
part number, and serial number of the
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Federal Register / Vol. 81, No. 149 / Wednesday, August 3, 2016 / Rules and Regulations
installed RAT actuator; modifying the
RAT; and re-identifying the RAT
actuator and RAT.
• Service Bulletin A330–29–3126,
dated June 12, 2014.
• Service Bulletin A340–29–4097,
dated June 12, 2014.
• Service Bulletin A340–29–5025,
dated June 16, 2014.
Hamilton Sundstrand has issued
Service Bulletins ERPS06M–29–21,
Revision 1, dated April 14, 2015; and
ERPS33T–29–7, dated June 6, 2014.
This service information describes
procedures for identifying the affected
RAT actuator and RAT part numbers
and serial numbers, modifying affected
actuators, and re-identifying affected
RAT actuators and RATs.
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.
Correction of Publication
This document corrects an error and
correctly adds the AD as an amendment
to 14 CFR 39.13. Although no other part
of the preamble or regulatory
information has been corrected, we are
publishing the entire rule in the Federal
Register.
The effective date of this AD remains
August 16, 2016.
Since this action only corrects
typographical errors, it has no adverse
economic impact and imposes no
additional burden on any person.
Therefore, we have determined that
notice and public procedures are
unnecessary.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation
safety, Incorporation by reference,
Safety.
Adoption of the Correction
Accordingly, pursuant to the
authority delegated to me by the
Administrator, the Federal Aviation
Administration amends part 39 of the
Federal Aviation Regulations (14 CFR
part 39) as follows:
1. The authority citation for part 39
continues to read as follows:
■
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Authority: 49 U.S.C. 106(g), 40113, 44701.
[Corrected]
2. The FAA amends § 39.13 by adding
the following new airworthiness
directive (AD):
■
2016–14–01 Airbus: Amendment 39–18582;
Docket No. FAA–2016–3983; Directorate
Identifier 2015–NM–009–AD.
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(b) Affected ADs
This AD affects the ADs specified in
paragraphs (b)(1), (b)(2), and (b)(3) of this AD.
(1) AD 2012–21–19, Amendment 39–17235
(77 FR 65812, October 31, 2012) (‘‘AD 2012–
21–19’’).
(2) AD 2012–21–20, Amendment 39–17236
(77 FR 65799, October 31, 2012) (‘‘AD 2012–
21–20’’).
(3) AD 2016–04–01, Amendment 39–18395
(81 FR 8134, February 18, 2016) (‘‘AD 2016–
04–01’’).
(c) Applicability
This AD applies to the airplanes identified
in paragraphs (c)(1) through (c)(7) of this AD,
certificated in any category.
(1) Airbus Model A330–223F and –243F
airplanes, all manufacturer serial numbers;
except those on which Airbus Modification
204067 has been embodied in production.
(2) Airbus Model A330–201, –202, –203,
–223, and –243 airplanes, all manufacturer
serial numbers; except those on which
Airbus Modification 204067 has been
embodied in production.
(3) Airbus Model A330–301, –302, –303,
–321, –322, –323, –341, –342, and –343
airplanes, all manufacturer serial numbers;
except those on which Airbus Modification
204067 has been embodied in production.
(4) Airbus Model A340–211, –212, and
–213, airplanes, all manufacturer serial
numbers.
(5) Airbus Model A340–311, –312, and
–313 airplanes, all manufacturer serial
numbers.
(6) Airbus Model A340–541 airplanes, all
manufacturer serial numbers.
(7) Airbus Model A340–642 airplanes, all
manufacturer serial numbers.
(d) Subject
Air Transport Association (ATA) of
America Code 29, Hydraulic Power.
(e) Reason
This AD was prompted by a report
indicating that, during an operational test of
a ram air turbine (RAT), the RAT did not
deploy in automatic mode. We are issuing
this AD to prevent non-deployment of the
RAT, which, if preceded by a total engine
flame-out, or during a total loss of normal
electrical power generation, could result in
reduced control of the airplane.
(f) Compliance
Comply with this AD within the
compliance times specified, unless already
done.
PART 39—AIRWORTHINESS
DIRECTIVES
§ 39.13
(a) Effective Date
This AD becomes effective on August 16,
2016.
(g) Identification and Replacement for
Certain Airbus Model A330, and A340–200
and –300 Airplanes
For Airbus Model A330–200 Freighter
series airplanes, Model A330–200 and –300
series airplanes, and Model A340–200 and
–300 series airplanes: Within 30 months after
the effective date of this AD, identify the
supplier, part number, and serial number of
the installed RAT actuator, in accordance
with the Accomplishment Instructions of
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Airbus Service Bulletin A330–29–3126,
dated June 12, 2014; or Airbus Service
Bulletin A340–29–4097, dated June 12, 2014;
as applicable.
(1) If the supplier identified is Arkwin
Industries, and the identified RAT actuator
part number and serial number are listed in
Hamilton Sundstrand Service Bulletin
ERPS06M–29–21, Revision 1, dated April 14,
2015, and the serial number is included in
table 2 of Hamilton Sundstrand Service
Bulletin ERPS06M–29–21, Revision 1, dated
April 14, 2015, with a description of
‘‘correctly shimmed’’: Within 30 months after
the effective date of this AD, re-identify the
actuator and the RAT, in accordance with the
Accomplishment Instructions of Airbus
Service Bulletin A330–29–3126, dated June
12, 2014; or Airbus Service Bulletin A340–
29–4097, dated June 12, 2014; as applicable.
(2) If the supplier identified is Arkwin
Industries, and the identified actuator RAT
part number and serial number are listed in
Hamilton Sundstrand Service Bulletin
ERPS06M–29–21, Revision 1, dated April 14,
2015, and the serial number is included in
table 2 of Hamilton Sundstrand Service
Bulletin ERPS06M–29–21, Revision 1, dated
April 14, 2015, with a description of
‘‘incorrectly shimmed’’: Within 30 months
after the effective date of this AD, remove the
actuator from the RAT, install a modified
actuator, and re-identify the RAT, in
accordance with the Accomplishment
Instructions of Airbus Service Bulletin A330–
29–3126, dated June 12, 2014; or Airbus
Service Bulletin A340–29–4097, dated June
12, 2014; as applicable.
(3) If the supplier identified is Arkwin
Industries, and the identification plate for the
RAT actuator is missing, or the part number
and serial number are not listed in Hamilton
Sundstrand Service Bulletin ERPS06M–29–
21, Revision 1, dated April 14, 2015: Within
30 months after the effective date of this AD,
remove the actuator from the RAT, install a
modified actuator, and re-identify the RAT,
in accordance with the Accomplishment
Instructions of Airbus Service Bulletin A330–
29–3126, dated June 12, 2014; or Airbus
Service Bulletin A340–29–4097, dated June
12, 2014; as applicable.
(h) Identification and Replacement for
Certain Airbus Model A340–500 and –600
Airplanes
For Airbus Model A340–500 and –600
airplanes: Within 30 months after the
effective date of this AD, identify the part
number and serial number of the installed
RAT actuator, in accordance with the
Accomplishment Instructions of Airbus
Service Bulletin A340–29–5025, dated June
16, 2014.
(1) If the identified RAT actuator part
number and serial number are listed in
Hamilton Sundstrand Service Bulletin
ERPS33T–29–7, dated June 6, 2014, and the
serial number is included in table 2 of
Hamilton Sundstrand Service Bulletin
ERPS33T–29–7, dated June 6, 2014, with a
description of ‘‘correctly shimmed’’: Within
30 months after the effective date of this AD,
re-identify the actuator and the RAT, in
accordance with the Accomplishment
Instructions of Airbus Service Bulletin A340–
29–5025, dated June 16, 2014.
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(2) If the identified RAT actuator part
number and serial number are listed in
Hamilton Sundstrand Service Bulletin
ERPS33T–29–7, dated June 6, 2014, and the
serial number is included in table 2 of
Hamilton Sundstrand Service Bulletin
ERPS33T–29–7, dated June 6, 2014, with a
description of ‘‘incorrectly shimmed’’:
Within 30 months after the effective date of
this AD, remove the actuator from the RAT,
install a modified actuator, and re-identify
the RAT, in accordance with the
Accomplishment Instructions of Airbus
Service Bulletin A340–29–5025, dated June
16, 2014.
(3) If the identification plate for the RAT
actuator is missing, or the part number and
serial number are not listed in Hamilton
Sundstrand Service Bulletin ERPS33T–29–7,
dated June 6, 2014: Within 30 months after
the effective date of this AD, remove the
actuator from the RAT, install a modified
actuator, and re-identify the RAT, in
accordance with the Accomplishment
Instructions of Airbus Service Bulletin A340–
29–5025, dated June 16, 2014.
(i) Terminating Action for Certain
Requirements of Other ADs
(1) For Airbus Model A330–200 Freighter,
A330–200, and A330–300 series airplanes;
and Model A340–200 and –300 series
airplanes: Accomplishment of the actions
required by paragraph (g)(1), (g)(2), or (g)(3)
of this AD constitutes compliance with the
requirements of paragraph (g)(1) of AD 2012–
21–19, paragraph (g) of AD 2012–21–20, and
51099
paragraphs (g), (h), and (i) of AD 2016–04–
01, for that airplane only.
(2) For Airbus Model A340–500 and –600
series airplanes: Accomplishment of the
actions required by paragraphs (h)(1), (h)(2),
and (h)(3) of this AD constitutes compliance
with the requirements of paragraphs (h)(1)
and (h)(2) of AD 2012–21–20, and paragraph
(j) of 2016–04–01, for that airplane only.
(j) Parts Installation Limitations
As of the effective date of this AD, no
person may install any RAT actuator or any
RAT having a part number identified in table
1 to paragraph (j) of this AD on any airplane,
unless it meets the conditions specified in
paragraph (j)(1) or (j)(2) of this AD, as
applicable.
TABLE 1 TO PARAGRAPH (j) OF THIS AD—AFFECTED PART NUMBERS
Affected Airbus airplane models
Model A330–200
planes.
Model A330–200
planes.
Model A340–200
planes.
Model A340–500
planes.
and –300 series airFreighter series airand –300 series airand –600 series air-
1702934C, 1702934D, 766351A, 768084A, 770379A, 770952C, 770952D,
770952E.
1702934C, 1702934D, 766351A, 768084A, 770379A, 770952C, 770952D,
770952E.
1702934C, 1702934D, 766351A, 768084A, 770379A, 770952C, 770952D,
770952E.
772722H, 772722J, 772722L ................................................................................
(1) For Airbus Model A330–200 Freighter
series airplanes; Model A330–200, and
A330–300 series airplanes; and Model A340–
200 and –300 series airplanes: The RAT
actuator or RAT has a serial number listed as
affected and modified in Hamilton
Sundstrand Service Bulletin ERPS06M–29–
21, Revision 1, dated April 14, 2015, and the
RAT has been re-identified in accordance
with the Accomplishment Instructions of
Airbus Service Bulletin A330–29–3126,
dated June 12, 2014; or Airbus Service
Bulletin A340–29–4097, dated June 12, 2014.
(2) For Airbus Model A340–500 and –600
series airplanes: The RAT actuator or the
RAT has a serial number listed as affected
and modified in Hamilton Sundstrand
Service Bulletin ERPS33T–29–7, dated June
6, 2014, and the RAT has been re-identified
in accordance with the Accomplishment
Instructions of Airbus Service Bulletin A340–
29–5025, dated June 16, 2014.
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(k) Credit for Previous Actions
(1) This paragraph provides credit for the
RAT and RAT actuator identification
specified in paragraphs (g)(1), (g)(2), and
(g)(3) of this AD if that identification was
performed before the effective date of this AD
using Hamilton Sundstrand Service Bulletin
ERPS06M–29–21, dated May 27, 2014, which
is not incorporated by reference in this AD.
(2) This paragraph provides credit for the
RAT or RAT actuator identification and
modification specified in paragraph (j)(1) of
this AD, if those actions were performed
before the effective date of this AD using
Hamilton Sundstrand Service Bulletin
ERPS06M–29–21, dated May 27, 2014, which
is not incorporated by reference in this AD.
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RAT actuator
part No.
RAT part No.
(l) Other FAA AD Provisions
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:
Vladimir Ulyanov, Aerospace Engineer,
International Branch, ANM–116, Transport
Airplane Directorate, FAA, 1601 Lind
Avenue SW., Renton, WA 98057–3356;
telephone 425–227–1138; fax 425–227–1149.
Information may be emailed to: 9-ANM-116AMOC-REQUESTS@faa.gov. 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.
(2) Contacting the Manufacturer: For any
requirement in this AD to obtain corrective
actions from a manufacturer, the action must
be accomplished using a method approved
by the Manager, International Branch, ANM–
116, Transport Airplane Directorate, FAA; or
the European Aviation Safety Agency
(EASA); or Airbus’s EASA Design
Organization Approval (DOA). If approved by
the DOA, the approval must include the
DOA-authorized signature.
(3) Required for Compliance (RC): If any
Airbus service information contains
procedures or tests that are identified as RC,
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5912958, 5915768
5912958, 5915768
5912958, 5915768
5912536, 5915769
those procedures and tests must be done to
comply with this AD; any procedures or tests
that are not identified as RC are
recommended. Those procedures and tests
that are not identified as RC may be deviated
from using accepted methods in accordance
with the operator’s maintenance or
inspection program without obtaining
approval of an AMOC, provided the
procedures and tests identified as RC can be
done and the airplane can be put back in an
airworthy condition. Any substitutions or
changes to procedures or tests identified as
RC require approval of an AMOC.
(m) Related Information
(1) Refer to Mandatory Continuing
Airworthiness Information (MCAI) EASA
Airworthiness Directive 2015–0008, dated
January 15, 2015, for related information.
This MCAI may be found in the AD docket
on the Internet at https://www.regulations.gov
by searching for and locating Docket No.
FAA–2016–3983.
(2) Service information identified in this
AD that is not incorporated by reference is
available at the addresses specified in
paragraphs (n)(4) and (n)(5) of this AD.
(n) 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 this AD specifies otherwise.
(3) The following service information was
approved for IBR on August 16, 2016 (81 FR
44983, July 12, 2016).
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Federal Register / Vol. 81, No. 149 / Wednesday, August 3, 2016 / Rules and Regulations
(i) Airbus Service Bulletin A330–29–3126,
dated June 12, 2014.
(ii) Airbus Service Bulletin A340–29–4097,
dated June 12, 2014.
(iii) Airbus Service Bulletin A340–29–
5025, dated June 16, 2014.
(iv) Hamilton Sundstrand Service Bulletin
ERPS06M–29–21, Revision 1, dated April 14,
2015.
(v) Hamilton Sundstrand Service Bulletin
ERPS33T–29–7, dated June 6, 2014.
(4) For Airbus service information
identified in this AD, contact Airbus SAS,
Airworthiness Office—EAL, 1 Rond Point
Maurice Bellonte, 31707 Blagnac Cedex,
France; telephone +33 5 61 93 36 96; fax +33
5 61 93 45 80; email airworthiness.A330A340@airbus.com; Internet https://
www.airbus.com.
(5) For Hamilton Sundstrand service
information identified in this AD, contact
Hamilton Sundstrand, Technical
Publications, Mail Stop 302–9, 4747 Harrison
Avenue, P.O. Box 7002, Rockford, IL 61125–
7002; telephone 860–654–3575; fax 860–998–
4564; email tech.solutions@hs.utc.com;
Internet https://
www.hamiltonsundstrand.com.
(6) 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.
(7) 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
202–741–6030, or go to: https://
www.archives.gov/federal-register/cfr/ibrlocations.html.
Issued in Renton, Washington, on July 25,
2016.
Victor Wicklund,
Acting Manager, Transport Airplane
Directorate, Aircraft Certification Service.
DATES:
Effective date: August 3, 2016.
FOR FURTHER INFORMATION CONTACT:
Richard Wartchow, Office of the General
Counsel, Federal Energy Regulatory
Commission, 888 First Street NE.,
Washington, DC 20426, Telephone:
202–502–6000.
SUPPLEMENTARY INFORMATION: The
Commission amended 18 CFR
154.112(a), addressing the filing of
‘‘special rate schedules,’’ reflecting
special operating arrangements
previously certificated pursuant to part
157 of the Commission’s regulations
(such as for the exchange of natural
gas).1
As published in the 2015 edition of
the Code of Federal Regulations, the
final regulations (effective November 3,
2008) contained an error. Order No. 714
revised the fourth, fifth and sixth
sentences to reflect new filing
requirements. However, the published
version of 18 CFR 154.112(a) incorrectly
retained language from the earlier
version that should have been
superseded. The Commission did not
intend to retain the superseded
sentences. This correcting amendment
removes the incorrectly-retained
language. This correction does not affect
18 CFR 154.112(b) which remains
unchanged.
List of Subjects in 18 CFR Part 154
Natural gas, Pipelines, Reporting and
record-keeping requirements, Natural
gas companies, Rate schedules and
tariffs.
Accordingly, 18 CFR part 154 is
corrected by making the following
correcting amendments:
[FR Doc. 2016–18174 Filed 8–2–16; 8:45 am]
PART 154—RATE SCHEDULES AND
TARIFFS
BILLING CODE 4910–13–P
1. The authority citation for part 154
continues to read as follows:
DEPARTMENT OF ENERGY
■
Federal Energy Regulatory
Commission
Authority: 15 U.S.C. 717–717w; 31 U.S.C.
9701; 42 U.S.C. 7102–7352.
18 CFR Part 154
■
2. Section 154.112 is corrected by
revising paragraph (a) to read as follows:
[Docket No. RM01–5–000]
§ 154.112 Exception to form and
composition of tariff.
Electronic Tariff Filings
Federal Energy Regulatory
Commission, DOE.
ACTION: Correcting amendment.
AGENCY:
This document contains
corrections to the final regulations that
became effective November 3, 2008
(with implementation of the
requirements beginning April 1, 2010),
as published in the subsequent editions
of the Code of Federal Regulations,
including the 2015 edition.
rmajette on DSK2TPTVN1PROD with RULES
SUMMARY:
VerDate Sep<11>2014
14:12 Aug 02, 2016
Jkt 238001
the date of the agreement, a brief
description of services to be rendered,
and the designation: ‘‘Rate Schedule X[number].’’ Special rate schedules may
not contain any supplements.
Modifications must be made by
inserting revised sheets, sections or the
entire document as appropriate. Special
rate schedules must be included in a
separate volume of the tariff. Each such
separate volume must contain a table of
contents which is incorporated as a
sheet or section in the open access
transmission tariff.
*
*
*
*
*
Dated: July 28, 2016.
Kimberly D. Bose,
Secretary.
[FR Doc. 2016–18360 Filed 8–2–16; 8:45 am]
BILLING CODE 6717–01–P
SOCIAL SECURITY ADMINISTRATION
20 CFR Part 404
[Docket No. SSA–2016–0023]
RIN 0960–AI03
Extension of Expiration Dates for Four
Body System Listings
Social Security Administration.
Final rule.
AGENCY:
ACTION:
We are extending the
expiration dates of the following body
systems in the Listing of Impairments
(listings) in our regulations:
Musculoskeletal System, Cardiovascular
System, Digestive System, and Skin
Disorders. We are making no other
revisions to these body systems in this
final rule. This extension ensures that
we will continue to have the criteria we
need to evaluate impairments in the
affected body systems at step three of
the sequential evaluation processes for
initial claims and continuing disability
reviews.
DATES: This final rule is effective on
August 3, 2016.
FOR FURTHER INFORMATION CONTACT:
Cheryl A. Williams, Director, Office of
Medical Policy, 6401 Security
Boulevard, Baltimore, MD 21235–6401,
(410) 965–1020. For information on
eligibility or filing for benefits, call our
national toll-free number, 1–800–772–
1213, or TTY 1–800–325–0778, or visit
our Internet site, Social Security Online,
at https://www.socialsecurity.gov.
SUPPLEMENTARY INFORMATION:
SUMMARY:
(a) The Commission may permit a
special rate schedule to be filed in the
form of an agreement in the case of a
special operating arrangement,
previously certificated pursuant to part
157 of this chapter, such as for the
exchange of natural gas. The special rate
schedule must contain a title page
showing the parties to the agreement,
Background
1 Electronic Tariff Filings, Order No. 714, FERC
Stats. & Regs. ¶ 31,276, 73 FR 57515 (2008) (Order
No. 714).
We use the listings in appendix 1 to
subpart P of part 404 of 20 CFR at the
third step of the sequential evaluation
PO 00000
Frm 00026
Fmt 4700
Sfmt 4700
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]]>Agencies
[Federal Register Volume 81, Number 149 (Wednesday, August 3, 2016)]
[Rules and Regulations]
[Pages 51097-51100]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2016-18174]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2016-3983; Directorate Identifier 2015-NM-009-AD;
Amendment 39-18582; AD 2016-14-01]
RIN 2120-AA64
Airworthiness Directives; Airbus Airplanes
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Final rule; correction.
-----------------------------------------------------------------------
SUMMARY: The FAA is correcting an airworthiness directive (AD) that
published in the Federal Register. That AD applies to certain Airbus
Model A330-200 Freighter series airplanes; Model A330-200 and A330-300
series airplanes; Model A340-200 and A340-300 series airplanes; Model
A340-500 series airplanes; and Model A340-600 series airplanes. Table 1
to paragraph (j) of the regulatory text contains typographical errors
regarding certain part numbers (P/Ns). This document corrects those
errors. In all other respects, the original document remains the same.
DATES: This final rule is effective August 16, 2016.
The Director of the Federal Register approved the incorporation by
reference of certain publications listed in this AD as of August 16,
2016 (81 FR 44983, July 12, 2016).
ADDRESSES: For Airbus service information identified in this final
rule, contact Airbus SAS, Airworthiness Office--EAL, 1 Rond Point
Maurice Bellonte, 31707 Blagnac Cedex, France; telephone +33 5 61 93 36
96; fax +33 5 61 93 45 80; email airworthiness.A330-A340@airbus.com;
Internet https://www.airbus.com.
For Hamilton Sundstrand service information identified in this
final rule, contact Hamilton Sundstrand, Technical Publications, Mail
Stop 302-9, 4747 Harrison Avenue, P.O. Box 7002, Rockford, IL 61125-
7002; telephone 860-654-3575; fax 860-998-4564; email
tech.solutions@hs.utc.com; Internet https://www.hamiltonsundstrand.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 425-
227-1221. It is also available on the Internet at https://www.regulations.gov by searching for and locating Docket No. FAA-2016-
3983.
Examining the AD Docket
You may examine the AD docket on the Internet at https://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 address for the
Docket Office (phone: 800-647-5527) is Docket Management Facility, U.S.
Department of Transportation, Docket Operations, M-30, West Building
Ground Floor, Room W12-140, 1200 New Jersey Avenue SE., Washington, DC
20590.
FOR FURTHER INFORMATION CONTACT: Vladimir Ulyanov, Aerospace Engineer,
International Branch, ANM-116, Transport Airplane Directorate, FAA,
1601 Lind Avenue SW., Renton, WA 98057-3356; telephone 425-227-1138;
fax 425-227-1149.
SUPPLEMENTARY INFORMATION: Airworthiness Directive 2016-14-01,
Amendment 39-18582 (81 FR 44983, July 12, 2016) (``AD 2016-14-01''),
currently requires identification of the manufacturer, part number, and
serial number of the ram air turbine (RAT), and re-identification and
modification of the RAT if necessary, for certain Airbus Model A330-200
Freighter series airplanes; Model A330-200 and A330-300 series
airplanes; Model A340-200 and A340-300 series airplanes; Model A340-500
series airplanes; and Model A340-600 series airplanes.
Need for the Correction
As published, table 1 to paragraph (j) of the regulatory text
contains typographical errors in two part numbers. Table 1 to paragraph
(j) of the AD incorrectly refers to RAT P/Ns 1720934C and 1720934D.
Those part numbers should have been 1702934C and 1702934D.
Related Service Information Under 1 CFR Part 51
Airbus has issued the following service information, which
describes procedures for identifying the supplier, part number, and
serial number of the
[[Page 51098]]
installed RAT actuator; modifying the RAT; and re-identifying the RAT
actuator and RAT.
Service Bulletin A330-29-3126, dated June 12, 2014.
Service Bulletin A340-29-4097, dated June 12, 2014.
Service Bulletin A340-29-5025, dated June 16, 2014.
Hamilton Sundstrand has issued Service Bulletins ERPS06M-29-21,
Revision 1, dated April 14, 2015; and ERPS33T-29-7, dated June 6, 2014.
This service information describes procedures for identifying the
affected RAT actuator and RAT part numbers and serial numbers,
modifying affected actuators, and re-identifying affected RAT actuators
and RATs.
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.
Correction of Publication
This document corrects an error and correctly adds the AD as an
amendment to 14 CFR 39.13. Although no other part of the preamble or
regulatory information has been corrected, we are publishing the entire
rule in the Federal Register.
The effective date of this AD remains August 16, 2016.
Since this action only corrects typographical errors, it has no
adverse economic impact and imposes no additional burden on any person.
Therefore, we have determined that notice and public procedures are
unnecessary.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation safety, Incorporation by
reference, Safety.
Adoption of the Correction
Accordingly, pursuant to the authority delegated to me by the
Administrator, the Federal Aviation Administration amends part 39 of
the Federal Aviation Regulations (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 [Corrected]
0
2. The FAA amends Sec. 39.13 by adding the following new airworthiness
directive (AD):
2016-14-01 Airbus: Amendment 39-18582; Docket No. FAA-2016-3983;
Directorate Identifier 2015-NM-009-AD.
(a) Effective Date
This AD becomes effective on August 16, 2016.
(b) Affected ADs
This AD affects the ADs specified in paragraphs (b)(1), (b)(2),
and (b)(3) of this AD.
(1) AD 2012-21-19, Amendment 39-17235 (77 FR 65812, October 31,
2012) (``AD 2012-21-19'').
(2) AD 2012-21-20, Amendment 39-17236 (77 FR 65799, October 31,
2012) (``AD 2012-21-20'').
(3) AD 2016-04-01, Amendment 39-18395 (81 FR 8134, February 18,
2016) (``AD 2016-04-01'').
(c) Applicability
This AD applies to the airplanes identified in paragraphs (c)(1)
through (c)(7) of this AD, certificated in any category.
(1) Airbus Model A330-223F and -243F airplanes, all manufacturer
serial numbers; except those on which Airbus Modification 204067 has
been embodied in production.
(2) Airbus Model A330-201, -202, -203, -223, and -243 airplanes,
all manufacturer serial numbers; except those on which Airbus
Modification 204067 has been embodied in production.
(3) Airbus Model A330-301, -302, -303, -321, -322, -323, -341, -
342, and -343 airplanes, all manufacturer serial numbers; except
those on which Airbus Modification 204067 has been embodied in
production.
(4) Airbus Model A340-211, -212, and -213, airplanes, all
manufacturer serial numbers.
(5) Airbus Model A340-311, -312, and -313 airplanes, all
manufacturer serial numbers.
(6) Airbus Model A340-541 airplanes, all manufacturer serial
numbers.
(7) Airbus Model A340-642 airplanes, all manufacturer serial
numbers.
(d) Subject
Air Transport Association (ATA) of America Code 29, Hydraulic
Power.
(e) Reason
This AD was prompted by a report indicating that, during an
operational test of a ram air turbine (RAT), the RAT did not deploy
in automatic mode. We are issuing this AD to prevent non-deployment
of the RAT, which, if preceded by a total engine flame-out, or
during a total loss of normal electrical power generation, could
result in reduced control of the airplane.
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
(g) Identification and Replacement for Certain Airbus Model A330, and
A340-200 and -300 Airplanes
For Airbus Model A330-200 Freighter series airplanes, Model
A330-200 and -300 series airplanes, and Model A340-200 and -300
series airplanes: Within 30 months after the effective date of this
AD, identify the supplier, part number, and serial number of the
installed RAT actuator, in accordance with the Accomplishment
Instructions of Airbus Service Bulletin A330-29-3126, dated June 12,
2014; or Airbus Service Bulletin A340-29-4097, dated June 12, 2014;
as applicable.
(1) If the supplier identified is Arkwin Industries, and the
identified RAT actuator part number and serial number are listed in
Hamilton Sundstrand Service Bulletin ERPS06M-29-21, Revision 1,
dated April 14, 2015, and the serial number is included in table 2
of Hamilton Sundstrand Service Bulletin ERPS06M-29-21, Revision 1,
dated April 14, 2015, with a description of ``correctly shimmed'':
Within 30 months after the effective date of this AD, re-identify
the actuator and the RAT, in accordance with the Accomplishment
Instructions of Airbus Service Bulletin A330-29-3126, dated June 12,
2014; or Airbus Service Bulletin A340-29-4097, dated June 12, 2014;
as applicable.
(2) If the supplier identified is Arkwin Industries, and the
identified actuator RAT part number and serial number are listed in
Hamilton Sundstrand Service Bulletin ERPS06M-29-21, Revision 1,
dated April 14, 2015, and the serial number is included in table 2
of Hamilton Sundstrand Service Bulletin ERPS06M-29-21, Revision 1,
dated April 14, 2015, with a description of ``incorrectly shimmed'':
Within 30 months after the effective date of this AD, remove the
actuator from the RAT, install a modified actuator, and re-identify
the RAT, in accordance with the Accomplishment Instructions of
Airbus Service Bulletin A330-29-3126, dated June 12, 2014; or Airbus
Service Bulletin A340-29-4097, dated June 12, 2014; as applicable.
(3) If the supplier identified is Arkwin Industries, and the
identification plate for the RAT actuator is missing, or the part
number and serial number are not listed in Hamilton Sundstrand
Service Bulletin ERPS06M-29-21, Revision 1, dated April 14, 2015:
Within 30 months after the effective date of this AD, remove the
actuator from the RAT, install a modified actuator, and re-identify
the RAT, in accordance with the Accomplishment Instructions of
Airbus Service Bulletin A330-29-3126, dated June 12, 2014; or Airbus
Service Bulletin A340-29-4097, dated June 12, 2014; as applicable.
(h) Identification and Replacement for Certain Airbus Model A340-500
and -600 Airplanes
For Airbus Model A340-500 and -600 airplanes: Within 30 months
after the effective date of this AD, identify the part number and
serial number of the installed RAT actuator, in accordance with the
Accomplishment Instructions of Airbus Service Bulletin A340-29-5025,
dated June 16, 2014.
(1) If the identified RAT actuator part number and serial number
are listed in Hamilton Sundstrand Service Bulletin ERPS33T-29-7,
dated June 6, 2014, and the serial number is included in table 2 of
Hamilton Sundstrand Service Bulletin ERPS33T-29-7, dated June 6,
2014, with a description of ``correctly shimmed'': Within 30 months
after the effective date of this AD, re-identify the actuator and
the RAT, in accordance with the Accomplishment Instructions of
Airbus Service Bulletin A340-29-5025, dated June 16, 2014.
[[Page 51099]]
(2) If the identified RAT actuator part number and serial number
are listed in Hamilton Sundstrand Service Bulletin ERPS33T-29-7,
dated June 6, 2014, and the serial number is included in table 2 of
Hamilton Sundstrand Service Bulletin ERPS33T-29-7, dated June 6,
2014, with a description of ``incorrectly shimmed'': Within 30
months after the effective date of this AD, remove the actuator from
the RAT, install a modified actuator, and re-identify the RAT, in
accordance with the Accomplishment Instructions of Airbus Service
Bulletin A340-29-5025, dated June 16, 2014.
(3) If the identification plate for the RAT actuator is missing,
or the part number and serial number are not listed in Hamilton
Sundstrand Service Bulletin ERPS33T-29-7, dated June 6, 2014: Within
30 months after the effective date of this AD, remove the actuator
from the RAT, install a modified actuator, and re-identify the RAT,
in accordance with the Accomplishment Instructions of Airbus Service
Bulletin A340-29-5025, dated June 16, 2014.
(i) Terminating Action for Certain Requirements of Other ADs
(1) For Airbus Model A330-200 Freighter, A330-200, and A330-300
series airplanes; and Model A340-200 and -300 series airplanes:
Accomplishment of the actions required by paragraph (g)(1), (g)(2),
or (g)(3) of this AD constitutes compliance with the requirements of
paragraph (g)(1) of AD 2012-21-19, paragraph (g) of AD 2012-21-20,
and paragraphs (g), (h), and (i) of AD 2016-04-01, for that airplane
only.
(2) For Airbus Model A340-500 and -600 series airplanes:
Accomplishment of the actions required by paragraphs (h)(1), (h)(2),
and (h)(3) of this AD constitutes compliance with the requirements
of paragraphs (h)(1) and (h)(2) of AD 2012-21-20, and paragraph (j)
of 2016-04-01, for that airplane only.
(j) Parts Installation Limitations
As of the effective date of this AD, no person may install any
RAT actuator or any RAT having a part number identified in table 1
to paragraph (j) of this AD on any airplane, unless it meets the
conditions specified in paragraph (j)(1) or (j)(2) of this AD, as
applicable.
Table 1 to Paragraph (j) of This AD--Affected Part Numbers
----------------------------------------------------------------------------------------------------------------
Affected Airbus airplane models RAT part No. RAT actuator part No.
----------------------------------------------------------------------------------------------------------------
Model A330-200 and -300 series airplanes 1702934C, 1702934D, 766351A, 5912958, 5915768
768084A, 770379A, 770952C,
770952D, 770952E.
Model A330-200 Freighter series 1702934C, 1702934D, 766351A, 5912958, 5915768
airplanes. 768084A, 770379A, 770952C,
770952D, 770952E.
Model A340-200 and -300 series airplanes 1702934C, 1702934D, 766351A, 5912958, 5915768
768084A, 770379A, 770952C,
770952D, 770952E.
Model A340-500 and -600 series airplanes 772722H, 772722J, 772722L....... 5912536, 5915769
----------------------------------------------------------------------------------------------------------------
(1) For Airbus Model A330-200 Freighter series airplanes; Model
A330-200, and A330-300 series airplanes; and Model A340-200 and -300
series airplanes: The RAT actuator or RAT has a serial number listed
as affected and modified in Hamilton Sundstrand Service Bulletin
ERPS06M-29-21, Revision 1, dated April 14, 2015, and the RAT has
been re-identified in accordance with the Accomplishment
Instructions of Airbus Service Bulletin A330-29-3126, dated June 12,
2014; or Airbus Service Bulletin A340-29-4097, dated June 12, 2014.
(2) For Airbus Model A340-500 and -600 series airplanes: The RAT
actuator or the RAT has a serial number listed as affected and
modified in Hamilton Sundstrand Service Bulletin ERPS33T-29-7, dated
June 6, 2014, and the RAT has been re-identified in accordance with
the Accomplishment Instructions of Airbus Service Bulletin A340-29-
5025, dated June 16, 2014.
(k) Credit for Previous Actions
(1) This paragraph provides credit for the RAT and RAT actuator
identification specified in paragraphs (g)(1), (g)(2), and (g)(3) of
this AD if that identification was performed before the effective
date of this AD using Hamilton Sundstrand Service Bulletin ERPS06M-
29-21, dated May 27, 2014, which is not incorporated by reference in
this AD.
(2) This paragraph provides credit for the RAT or RAT actuator
identification and modification specified in paragraph (j)(1) of
this AD, if those actions were performed before the effective date
of this AD using Hamilton Sundstrand Service Bulletin ERPS06M-29-21,
dated May 27, 2014, which is not incorporated by reference in this
AD.
(l) Other FAA AD Provisions
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: Vladimir
Ulyanov, Aerospace Engineer, International Branch, ANM-116,
Transport Airplane Directorate, FAA, 1601 Lind Avenue SW., Renton,
WA 98057-3356; telephone 425-227-1138; fax 425-227-1149. Information
may be emailed to: 9-ANM-116-AMOC-REQUESTS@faa.gov. 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.
(2) Contacting the Manufacturer: For any requirement in this AD
to obtain corrective actions from a manufacturer, the action must be
accomplished using a method approved by the Manager, International
Branch, ANM-116, Transport Airplane Directorate, FAA; or the
European Aviation Safety Agency (EASA); or Airbus's EASA Design
Organization Approval (DOA). If approved by the DOA, the approval
must include the DOA-authorized signature.
(3) Required for Compliance (RC): If any Airbus service
information contains procedures or tests that are identified as RC,
those procedures and tests must be done to comply with this AD; any
procedures or tests that are not identified as RC are recommended.
Those procedures and tests that are not identified as RC may be
deviated from using accepted methods in accordance with the
operator's maintenance or inspection program without obtaining
approval of an AMOC, provided the procedures and tests identified as
RC can be done and the airplane can be put back in an airworthy
condition. Any substitutions or changes to procedures or tests
identified as RC require approval of an AMOC.
(m) Related Information
(1) Refer to Mandatory Continuing Airworthiness Information
(MCAI) EASA Airworthiness Directive 2015-0008, dated January 15,
2015, for related information. This MCAI may be found in the AD
docket on the Internet at https://www.regulations.gov by searching
for and locating Docket No. FAA-2016-3983.
(2) Service information identified in this AD that is not
incorporated by reference is available at the addresses specified in
paragraphs (n)(4) and (n)(5) of this AD.
(n) 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 this AD specifies otherwise.
(3) The following service information was approved for IBR on
August 16, 2016 (81 FR 44983, July 12, 2016).
[[Page 51100]]
(i) Airbus Service Bulletin A330-29-3126, dated June 12, 2014.
(ii) Airbus Service Bulletin A340-29-4097, dated June 12, 2014.
(iii) Airbus Service Bulletin A340-29-5025, dated June 16, 2014.
(iv) Hamilton Sundstrand Service Bulletin ERPS06M-29-21,
Revision 1, dated April 14, 2015.
(v) Hamilton Sundstrand Service Bulletin ERPS33T-29-7, dated
June 6, 2014.
(4) For Airbus service information identified in this AD,
contact Airbus SAS, Airworthiness Office--EAL, 1 Rond Point Maurice
Bellonte, 31707 Blagnac Cedex, France; telephone +33 5 61 93 36 96;
fax +33 5 61 93 45 80; email airworthiness.A330-A340@airbus.com;
Internet https://www.airbus.com.
(5) For Hamilton Sundstrand service information identified in
this AD, contact Hamilton Sundstrand, Technical Publications, Mail
Stop 302-9, 4747 Harrison Avenue, P.O. Box 7002, Rockford, IL 61125-
7002; telephone 860-654-3575; fax 860-998-4564; email
tech.solutions@hs.utc.com; Internet https://www.hamiltonsundstrand.com.
(6) 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.
(7) 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 202-741-6030, or go to: https://www.archives.gov/federal-register/cfr/ibr-locations.html.
Issued in Renton, Washington, on July 25, 2016.
Victor Wicklund,
Acting Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 2016-18174 Filed 8-2-16; 8:45 am]
BILLING CODE 4910-13-P
