Airworthiness Directives; Zodiac Seats France (Formerly Sicma Aero Seat) Passenger Seat Assemblies, 30349-30352 [2015-11392]
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Federal Register / Vol. 80, No. 102 / Thursday, May 28, 2015 / Rules and Regulations
(a) Effective Date
This AD is effective June 12, 2015.
(b) Affected ADs
This AD supersedes AD 2014–01–01,
Amendment 39–17724 (79 FR 3481, January
22, 2014).
devices, identifiable by serial number (S/N),
may have an incorrect bonding of the nozzle
on the ejector assembly. We are issuing this
AD to prevent failure of the ejector assembly
nozzle, which could lead to an in-flight
shutdown of the engine, damage to the
engine, and damage to the helicopter.
(e) Compliance
Comply with this AD within the
compliance times specified, unless already
done.
(1) For engines equipped with a lubricating
device having an S/N listed in Figure 1 to
paragraph (e) of this AD, within 30 days after
(c) Applicability
This AD applies to all Turbomeca S.A.
Arrius 2F turboshaft engines.
(d) Unsafe Condition
This AD was prompted by the
determination that additional lubricating
the effective date of this AD, inspect the
ejector assembly nozzle and the tightening
torque. Use paragraphs 4.4.2.1 through
4.4.2.3.4.2 of Turbomeca Mandatory Service
Bulletin (MSB) No. 319 79 4835, Version B,
dated February 12, 2015, to do the
inspection.
(2) For any part that fails the inspection
required by paragraph (e)(1) of this AD,
before further flight, remove and replace the
failed part with a part eligible for installation.
FIGURE 1 TO PARAGRAPH (e)—S/N’S OF AFFECTED LUBRICATING DEVICES
100
105M
106
107B
109M
112B
112M
114B
124B
125M
129M
135B
135M
140M
141M
142B
146M
147M
156M
159M
164M
178
178M
180
180M
181M
185M
190M
191M
195M
198M
202M
204M
207M
210M
213M
218M
222M
244M
247
255M
266M
278M
292M
304M
330M
334M
369M
384M
391M
392M
417M
(f) Credit for Previous Actions
(i) Material Incorporated by Reference
If you inspected the ejector assembly
nozzle of any lubricating device having an S/
N listed in Figure 1 to paragraph (e) of this
AD before the effective date of this AD, using
the instructions of Turbomeca S.A. MSB No.
319 79 4835, Version A, dated May 22, 2013,
you met the requirements of paragraph (e) of
this AD for that S/N lubricating device.
(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 June 12, 2015.
(i) Turbomeca S.A. Mandatory Service
Bulletin (MSB) No. 319 79 4835, Version B,
dated February 12, 2015.
(ii) Reserved.
(4) The following service information was
approved for IBR on February 6, 2014 (79 FR
3481, January 22, 2014).
(i) Turbomeca S.A. MSB No. 319 79 4835,
Version A, dated May 22, 2013.
(ii) Reserved.
(5) For Turbomeca S.A. service information
identified in this AD, contact Turbomeca
S.A., 40220 Tarnos, France; phone: 33 (0)5 59
74 40 00; telex: 570 042; fax: 33 (0)5 59 74
45 15.
(6) You may view this service information
at FAA, Engine & Propeller Directorate, 12
New England Executive Park, Burlington,
MA. For information on the availability of
this material at the FAA, call 781–238–7125.
(7) You may view this service information
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.
(g) Installation Prohibition
After the effective date of this AD, do not
return to service any engine having a
lubricating device with an S/N listed in
Figure 1 to paragraph (e) of this AD, unless
the engine has been inspected per the
requirements of paragraph (e) of this AD.
(h) Alternative Methods of Compliance
(AMOCs)
The Manager, Engine Certification Office,
FAA, may approve AMOCs for this AD. Use
the procedures found in 14 CFR 39.19 to
make your request. You may email your
request to: ANE-AD-AMOC@faa.gov.
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(i) Related Information
(1) For more information about this AD,
contact Philip Haberlen, Aerospace Engineer,
Engine Certification Office, FAA, Engine &
Propeller Directorate, 12 New England
Executive Park, Burlington, MA 01803;
phone: 781–238–7770; fax: 781–238–7199;
email: philip.haberlen@faa.gov.
(2) Refer to MCAI European Aviation
Safety Agency AD 2015–0057, dated April 1,
2015, for more information. You may
examine the MCAI in the AD docket on the
Internet at https://www.regulations.gov by
searching for and locating it in Docket No.
FAA–2013–1003.
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436M
443M
445M
451M
467M
477M
479M
483M
484M
512M
526M
563M
Issued in Burlington, Massachusetts, on
May 13, 2015.
Colleen M. D’Alessandro,
Assistant Directorate Manager, Engine &
Propeller Directorate, Aircraft Certification
Service.
[FR Doc. 2015–12654 Filed 5–27–15; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2015–1282; Directorate
Identifier 2015–NM–007–AD; Amendment
39–18157; AD 2015–10–02]
RIN 2120–AA64
Airworthiness Directives; Zodiac Seats
France (Formerly Sicma Aero Seat)
Passenger Seat Assemblies
Federal Aviation
Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule; request for
comments.
AGENCY:
We are superseding
Airworthiness Directive (AD) 2014–20–
11, for Zodiac Seats France 9140, 9166,
9173, 9174, 9184, 9188, 9196, 91B7,
91B8, 91C0, 91C2, 91C4, 91C5, 91C9,
9301, and 9501 series passenger seat
assemblies. AD 2014–20–11 required a
general visual inspection for cracking of
SUMMARY:
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Federal Register / Vol. 80, No. 102 / Thursday, May 28, 2015 / Rules and Regulations
backrest links; replacement with new
links if cracking is found; and eventual
replacement of all links with new links.
This AD was prompted by a
determination that a model designation
specified in paragraph (c)(1) of that AD
was incorrect. This new AD identifies
the correct model designation. We are
issuing this AD to detect and correct
cracks in the backrest links, which
could affect the structural integrity of
seat backrests. Failure of the backrest
links could result in injury to an
occupant during emergency landing
conditions.
This AD becomes effective June
12, 2015.
The Director of the Federal Register
approved the incorporation by reference
of a certain publication listed in this AD
as of October 22, 2014 (79 FR 60322,
October 7, 2014).
We must receive comments on this
AD by July 13, 2015.
ADDRESSES: You may send comments by
any of the following methods:
• Federal eRulemaking Portal: Go to
https://www.regulations.gov. Follow the
instructions for submitting comments.
• Fax: 202–493–2251.
• 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, between 9 a.m. and 5
p.m., Monday through Friday, except
Federal holidays.
For service information identified in
this AD, contact Zodiac Seats France, 7,
Rue Lucien Coupet, 36100 ISSOUDUN,
France; telephone +33 (0) 2 54 03 39 39;
fax +33 (0) 2 54 03 39 00; email
customerservices@sicma.zodiac.com;
Internet https://
www.sicma.zodiacaerospace.com/en/.
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.
DATES:
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Examining the AD Docket
You may examine the AD docket on
the Internet at https://
www.regulations.gov by searching for
and locating Docket No. FAA–2015–
1282; 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 this AD, the regulatory
evaluation, any comments received, and
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other information. The street address for
the Docket Operations office (telephone
800–647–5527) is in the ADDRESSES
section. Comments will be available in
the AD docket shortly after receipt.
FOR FURTHER INFORMATION CONTACT: Ian
Lucas, Aerospace Engineer, Boston
Aircraft Certification Office (ACO)
ANE–150, FAA, Engine and Propeller
Directorate, 12 New England Executive
Park, Burlington, MA 01803; phone:
781–238–7757; fax: 781–238–7170;
email: ian.lucas@faa.gov.
SUPPLEMENTARY INFORMATION:
Discussion
On September 23, 2014, we issued AD
2014–20–11, Amendment 39–17984 (79
FR 60322, October 7, 2014), to
supersede AD 2011–07–05, Amendment
39–16642 (76 FR 18020, April 1, 2011).
AD 2014–20–11 applied to certain
Zodiac Seats France 9140, 9166, 9173,
9174, 9184, 9188, 9196, 91B7, 91B8,
91C0, 91C2, 91C4, 91C5, 91C9, 9301,
and 9501 series passenger seat
assemblies; identified in Annex 1, Issue
3, dated January 25, 2012, of Sicma Aero
Seat Service Bulletin 90–25–012, Issue
6, dated January 25, 2012. AD 2014–20–
11 was prompted by a report that new
seat backrest links could be affected by
cracks similar to those identified on the
backrest links with the previous design.
AD 2014–20–11 required a general
visual inspection for cracking of
backrest links, which includes new seat
backrest links; replacement with new
links if cracking is found; and eventual
replacement of all links with new links.
We issued AD 2014–20–11 to detect and
correct cracking of backrest links, which
could affect the structural integrity of
seat backrests. Failure of the backrest
links could result in injury to an
occupant during emergency landing
conditions.
AD 2014–20–11, Amendment 39–
17984 (79 FR 60322, October 7, 2014),
corresponds to Mandatory Continuing
Airworthiness Information (MCAI)
European Aviation Safety Agency
Airworthiness Directive 2012–0038,
dated March 12, 2012. You may
examine the MCAI on the Internet at
https://www.regulations.gov by searching
for and locating Docket No. FAA–2015–
1282.
Since we issued AD 2014–20–11,
Amendment 39–17984 (79 FR 60322,
October 7, 2014), we have determined
that, in paragraph (c)(1) of AD 2014–20–
11, a model designation incorrectly
specified ‘‘A320–300’’ instead of
‘‘A330–300’’ as one of the models that
the affected passenger seats might be
installed on. Therefore, we have
determined that paragraph (c)(1) of this
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AD should read as follows: Airbus
Model A330–200, A330–200 Freighter,
and A330–300 series airplanes.
We have also re-designated paragraph
(l) of AD 2014–20–11, Amendment 39–
17984 (79 FR 60322, October 7, 2014),
as paragraph (l)(1) of this AD. We also
added a new paragraph (l)(2) to this AD
to provide information on the
availability of service information that is
not incorporated by reference in this
AD.
FAA’s Determination and Requirements
of This AD
This product has been approved by
the aviation authority of another
country, and is approved for operation
in the United States. Pursuant to our
bilateral agreement with the State of
Design Authority, we have been notified
of the unsafe condition described in the
MCAI and service information
referenced above. We are issuing this
AD because we evaluated all pertinent
information and determined the unsafe
condition exists and is likely to exist or
develop on other products of these same
type designs.
FAA’s Determination of the Effective
Date
Since there are currently no domestic
operators of airplanes that are equipped
with this product, notice and
opportunity for public comment before
issuing this AD are unnecessary.
Comments Invited
This AD is a final rule that involves
requirements affecting flight safety, and
we did not precede it by notice and
opportunity for public comment. We
invite you to send any written relevant
data, views, or arguments about this AD.
Send your comments to an address
listed under the ADDRESSES section.
Include ‘‘Docket No. FAA–2015–1282;
Directorate Identifier 2015–NM–007–
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 https://
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 0 seat
assemblies installed on, but not limited
to, transport airplanes of U.S. registry.
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Federal Register / Vol. 80, No. 102 / Thursday, May 28, 2015 / Rules and Regulations
The actions required by AD 2014–20–
11, Amendment 39–17984 (79 FR
60322, October 7, 2014), and retained in
this AD take about 1 work-hour per
product, at an average labor rate of $85
per work-hour. Required parts cost
about $227 per product. Based on these
figures, the estimated cost of the actions
that were required by AD 2014–20–11 is
$312 per product.
Since this AD only clarifies airplane
models on which the affected passenger
seat assemblies might be installed, this
AD adds no additional economic
burden.
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
1. The authority citation for part 39
continues to read as follows:
■
Authority for This Rulemaking
Authority: 49 U.S.C. 106(g), 40113, 44701.
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.
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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 that 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);
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.
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§ 39.13
[Amended]
2. The FAA amends § 39.13 by
removing airworthiness directive (AD)
2014–20–11, Amendment 39–17984 (79
FR 60322, October 7, 2014), and adding
the following new AD:
■
2015–10–02 Zodiac Seats France (formerly
Sicma Aero Seat): Amendment 39–
18157. Docket No. FAA–2015–1282;
Directorate Identifier 2015–NM–007–AD.
(a) Effective Date
This AD becomes effective June 12, 2015.
(b) Affected ADs
This AD replaces AD 2014–20–11,
Amendment 39–17984 (79 FR 60322, October
7, 2014).
(c) Applicability
This AD applies to Zodiac Seats France
9140, 9166, 9173, 9174, 9184, 9188, 9196,
91B7, 91B8, 91C0, 91C2, 91C4, 91C5, 91C9,
9301, and 9501 series passenger seat
assemblies; identified in Annex 1, Issue 3,
dated January 25, 2012, of Sicma Aero Seat
Service Bulletin 90–25–012, Issue 6, dated
January 25, 2012. These passenger seat
assemblies are installed on, but not limited
to, the airplanes identified in paragraphs
(c)(1), (c)(2), and (c)(3) of this AD, certificated
in any category.
(1) Airbus Model A330–200, A330–200
Freighter, and A330–300 series airplanes.
(2) Airbus Model A340–200, A340–300,
A340–500, and A340–600 series airplanes.
(3) The Boeing Company Model 777–200,
777–200LR, 777–300, 777–300ER, and 777F
series airplanes.
(d) Subject
Air Transport Association (ATA) of
America Code 25, Equipment/Furnishings.
(e) Reason
This AD was prompted by a report of
cracks in the backrest links on certain seats
and also by a determination that a model
designation specified in paragraph (c)(1) of
AD 2014–20–11, Amendment 39–17984 (79
FR 60322, October 7, 2014) was incorrect. We
are issuing this AD to detect and correct
cracks in the backrest links, which could
affect the structural integrity of seat
backrests. Failure of the backrest links could
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30351
result in injury to an occupant during
emergency landing conditions.
(f) Compliance
Comply with this AD within the
compliance times specified, unless already
done.
(g) Retained Repetitive Inspections, With No
Changes
This paragraph restates the requirements of
paragraph (g) of AD 2014–20–11,
Amendment 39–17984 (79 FR 60322, October
7, 2014), with no changes. At the later of the
times specified in paragraphs (g)(1) and (g)(2)
of this AD: Do a general visual inspection for
cracking of seat backrest links having part
number (P/N) 90–000200–104–1, P/N 90–
000200–104–2, P/N 90–000202–104–1, and
P/N 90–000202–104–2, in accordance with
the ‘‘PART ONE: GENERAL INTERMEDIATE
CHECKING PROCEDURE’’ of the
Accomplishment Instructions of Sicma Aero
Seat Service Bulletin 90–25–012, Issue 6,
dated January 25, 2012, including Annex 1,
Issue 3, dated January 25, 2012. If no
cracking is found on any link, repeat the
inspection thereafter at intervals not to
exceed 900 flight hours on the seat or 5
months since the most recent inspection,
whichever occurs later, until the replacement
specified in paragraph (i) of this AD is done.
(1) Within 6,000 flight hours on the seat or
2 years, whichever occurs later after the seat
manufacturing date or after the backrest link
replacement.
(2) Within 900 flight hours on the seat after
October 22, 2014 (the effective date AD
2014–20–11, Amendment 39–17984 (79 FR
60322, October 7, 2014)), but no later than 5
months after October 22, 2014.
(h) Retained Corrective Actions, With No
Changes
This paragraph restates the requirements of
paragraph (h) of AD 2014–20–11,
Amendment 39–17984 (79 FR 60322, October
7, 2014), with no changes.
(1) If, during any inspection required by
paragraph (g) of this AD, any cracking is
found on the link and no crack length
exceeds the lock-out pin-hole as specified in
Figure 2 or 4, as applicable, of Sicma Aero
Seat Service Bulletin 90–25–012, Issue 6,
dated January 25, 2012, including Annex 1,
Issue 3, dated January 25, 2012: Within 600
flight hours on the seat or 3 months,
whichever occurs later after crack
identification, replace the cracked link with
a new link, in accordance with ‘‘PART TWO:
ROUTINE REPLACEMENT PROCEDURE
(EXCEPT FOR SERIES 91B7, 91B8 & 91C5)’’
or ‘‘PART THREE: ROUTINE
REPLACEMENT PROCEDURE (FOR SERIES
91B7, 91B8 & 91C5)’’ of the Accomplishment
Instructions of Sicma Aero Seat Service
Bulletin 90–25–012, Issue 6, dated January
25, 2012, including Annex 1, Issue 3, dated
January 25, 2012.
(2) If, during any inspection required by
paragraph (g) of this AD, any cracking is
found on the link and any crack length
exceeds the lock-out pin-hole as specified in
Figure 2 or 4, as applicable, of Sicma Aero
Seat Service Bulletin 90–25–012, Issue 6,
dated January 25, 2012, including Annex 1,
Issue 3, dated January 25, 2012: Before
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further flight, replace the cracked link with
a new link, in accordance with ‘‘PART TWO:
ROUTINE REPLACEMENT PROCEDURE
(EXCEPT FOR SERIES 91B7, 91B8 & 91C5)’’
or ‘‘PART THREE: ROUTINE
REPLACEMENT PROCEDURE (FOR SERIES
91B7, 91B8 & 91C5)’’ of the Accomplishment
Instructions of Sicma Aero Seat Service
Bulletin 90–25–012, Issue 6, dated January
25, 2012, including Annex 1, Issue 3, dated
January 25, 2012.
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(i) Retained Replacement, With No Changes
This paragraph restates the requirements of
paragraph (i) of AD 2014–20–11, Amendment
39–17984 (79 FR 60322, October 7, 2014),
with no changes. At the later of the times
specified in paragraphs (i)(1) and (i)(2) of this
AD: Replace all seat backrest links, having P/
N 90–000200–104–1, P/N 90–000200–104–2,
P/N 90–000202–104–1, and P/N 90–000202–
104–2, with new links, in accordance with
‘‘PART TWO: ROUTINE REPLACEMENT
PROCEDURE (EXCEPT FOR SERIES 91B7,
91B8 & 91C5)’’ or ‘‘PART THREE: ROUTINE
REPLACEMENT PROCEDURE (FOR SERIES
91B7, 91B8 & 91C5)’’ of the Accomplishment
Instructions of Sicma Aero Seat Service
Bulletin 90–25–012, Issue 6, dated January
25, 2012, including Annex 1, Issue 3, dated
January 25, 2012.
(1) Within 12,000 flight hours on the seat
or 4 years, whichever occurs later after the
seat manufacturing date or after the backrest
link replacement.
(2) Within 3,500 flight hours on the seat
after October 22, 2014 (the effective date AD
2014–20–11, Amendment 39–17984 (79 FR
60322, October 7, 2014), but no later than 18
months after October 22, 2014.
(j) Retained Credit for Previous Actions,
With No Changes
This paragraph restates the credit provided
in paragraph (j) of AD 2014–20–11,
Amendment 39–17984 (79 FR 60322, October
7, 2014), with no changes. This paragraph
provides credit for actions required by
paragraphs (g), (h), and (i) of this AD, if those
actions were performed before October 22,
2014 (the effective date AD 2014–20–11,
Amendment 39–17984 (79 FR 60322, October
7, 2014), using the service information
specified in paragraph (j)(1), (j)(2), or (j)(3) of
this AD.
(1) Sicma Aero Seat Service Bulletin 90–
25–012, Issue 3, dated October 3, 2001,
which is not incorporated by reference in this
AD.
(2) Sicma Aero Seat Service Bulletin 90–
25–012, Issue 4, dated December 19, 2001,
which is not incorporated by reference in this
AD.
(3) Sicma Aero Seat Service Bulletin 90–
25–012, Issue 5, dated March 19, 2004,
including Annex 1, Issue 2, dated March 19,
2004, which was incorporated by reference in
AD 2011–07–05, Amendment 39–16642 (76
FR 18020, April 1, 2011).
(k) Other FAA AD Provisions
The following provisions also apply to this
AD:
(1) Alternative Methods of Compliance
(AMOCs): The Manager, Boston Aircraft
Certification Office (ACO), FAA, has the
authority to approve AMOCs for this AD, if
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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 ACO, send it to ATTN: Ian Lucas,
Aerospace Engineer, Boston ACO, ANE–150,
FAA, Engine and Propeller Directorate, 12
New England Executive Park, Burlington,
MA 01803; phone: 781–238–7757; fax: 781–
238–7170; email: ian.lucas@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, Boston ACO, FAA; or the
European Aviation Safety Agency (EASA).
(l) Related Information
(1) Refer to Mandatory Continuing
Airworthiness Information (MCAI) EASA
Airworthiness Directive 2012–0038, dated
March 12, 2012, for related information. You
may examine the MCAI on the Internet at
https://www.regulations.gov by searching for
and locating Docket No. FAA–2015–1282.
(2) Service information identified in this
AD that is not incorporated by reference is
available at the addresses specified in
paragraphs (m)(4) and (m)(5) of this AD.
(m) 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 October 22, 2014 (79 FR
60322, October 7, 2014).
(i) Sicma Aero Seat Service Bulletin 90–
25–012, Issue 6, dated January 25, 2012,
including Annex 1, Issue 3, dated January 25,
2012.
(ii) Reserved.
(4) For service information identified in
this AD, contact Zodiac Seats France, 7, Rue
Lucien Coupet, 36100 ISSOUDUN, France;
telephone +33 (0) 2 54 03 39 39; fax +33 (0)
2 54 03 39 00; email customerservices@
sicma.zodiac.com; Internet https://
www.sicma.zodiacaerospace.com/en/.
(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
202–741–6030, or go to: https://
www.archives.gov/federal-register/cfr/ibrlocations.html.
PO 00000
Frm 00020
Fmt 4700
Sfmt 4700
Issued in Renton, Washington, on May 4,
2015.
Jeffrey E. Duven,
Manager, Transport Airplane Directorate,
Aircraft Certification Service.
[FR Doc. 2015–11392 Filed 5–27–15; 8:45 am]
BILLING CODE 4910–13–P
NATIONAL AERONAUTICS AND
SPACE ADMINISTRATION
14 CFR Part 1216
RIN 2700–AE20
[Docket No. NASA–2015–0002]
Removal of Obsolete Regulations
National Aeronautics and
Space Administration.
ACTION: Direct final rule.
AGENCY:
This direct final rule makes
non-substantive changes by removing
regulations that are captured in NASA
internal requirements. The revisions to
this rule are part of NASA’s
retrospective plan completed in August
2011 under Executive Order (E.O.)
13563. NASA’s full plan can be
accessed on the Agency’s open
Government Web site at https://
www.nasa.gov/open/.
DATES: This direct final rule is effective
on July 27, 2015. Comments due on or
before June 29, 2015. If adverse
comments are received, NASA will
publish a timely withdrawal of the rule
in the Federal Register.
ADDRESSES: Comments must be
identified with RIN 2700–AE20 and
may be sent to NASA via the Federal ERulemaking Portal: https://
www.regulations.gov. Follow the online
instructions for submitting comments.
Please note that NASA will post all
comments on the Internet with changes,
including any personal information
provided.
SUMMARY:
FOR FURTHER INFORMATION CONTACT:
Nanette Jennings, 202–358–0819.
SUPPLEMENTARY INFORMATION:
Direct Final Rule Adverse Comments
NASA has determined this
rulemaking meets the criteria for a
direct final rule because it involves nonsubstantive changes to remove a section
from 14 CFR part 1216 that is captured
in internal NASA requirements. No
opposition to the changes and no
significant adverse comments are
expected. However, if the Agency
receives a significant adverse comment,
it will withdraw this direct final rule by
publishing a notice in the Federal
Register. A significant adverse comment
E:\FR\FM\28MYR1.SGM
28MYR1
]]>Agencies
[Federal Register Volume 80, Number 102 (Thursday, May 28, 2015)]
[Rules and Regulations]
[Pages 30349-30352]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2015-11392]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2015-1282; Directorate Identifier 2015-NM-007-AD;
Amendment 39-18157; AD 2015-10-02]
RIN 2120-AA64
Airworthiness Directives; Zodiac Seats France (Formerly Sicma
Aero Seat) Passenger Seat Assemblies
AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule; request for comments.
-----------------------------------------------------------------------
SUMMARY: We are superseding Airworthiness Directive (AD) 2014-20-11,
for Zodiac Seats France 9140, 9166, 9173, 9174, 9184, 9188, 9196, 91B7,
91B8, 91C0, 91C2, 91C4, 91C5, 91C9, 9301, and 9501 series passenger
seat assemblies. AD 2014-20-11 required a general visual inspection for
cracking of
[[Page 30350]]
backrest links; replacement with new links if cracking is found; and
eventual replacement of all links with new links. This AD was prompted
by a determination that a model designation specified in paragraph
(c)(1) of that AD was incorrect. This new AD identifies the correct
model designation. We are issuing this AD to detect and correct cracks
in the backrest links, which could affect the structural integrity of
seat backrests. Failure of the backrest links could result in injury to
an occupant during emergency landing conditions.
DATES: This AD becomes effective June 12, 2015.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in this AD as of October 22,
2014 (79 FR 60322, October 7, 2014).
We must receive comments on this AD by July 13, 2015.
ADDRESSES: You may send comments by any of the following methods:
Federal eRulemaking Portal: Go to https://www.regulations.gov. Follow the instructions for submitting comments.
Fax: 202-493-2251.
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, between 9 a.m. and 5 p.m., Monday
through Friday, except Federal holidays.
For service information identified in this AD, contact Zodiac Seats
France, 7, Rue Lucien Coupet, 36100 ISSOUDUN, France; telephone +33 (0)
2 54 03 39 39; fax +33 (0) 2 54 03 39 00; email
customerservices@sicma.zodiac.com; Internet https://www.sicma.zodiacaerospace.com/en/. 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.
Examining the AD Docket
You may examine the AD docket on the Internet at https://www.regulations.gov by searching for and locating Docket No. FAA-2015-
1282; 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 this AD, the regulatory evaluation, any comments received, and
other information. The street address for the Docket Operations office
(telephone 800-647-5527) is in the ADDRESSES section. Comments will be
available in the AD docket shortly after receipt.
FOR FURTHER INFORMATION CONTACT: Ian Lucas, Aerospace Engineer, Boston
Aircraft Certification Office (ACO) ANE-150, FAA, Engine and Propeller
Directorate, 12 New England Executive Park, Burlington, MA 01803;
phone: 781-238-7757; fax: 781-238-7170; email: ian.lucas@faa.gov.
SUPPLEMENTARY INFORMATION:
Discussion
On September 23, 2014, we issued AD 2014-20-11, Amendment 39-17984
(79 FR 60322, October 7, 2014), to supersede AD 2011-07-05, Amendment
39-16642 (76 FR 18020, April 1, 2011). AD 2014-20-11 applied to certain
Zodiac Seats France 9140, 9166, 9173, 9174, 9184, 9188, 9196, 91B7,
91B8, 91C0, 91C2, 91C4, 91C5, 91C9, 9301, and 9501 series passenger
seat assemblies; identified in Annex 1, Issue 3, dated January 25,
2012, of Sicma Aero Seat Service Bulletin 90-25-012, Issue 6, dated
January 25, 2012. AD 2014-20-11 was prompted by a report that new seat
backrest links could be affected by cracks similar to those identified
on the backrest links with the previous design. AD 2014-20-11 required
a general visual inspection for cracking of backrest links, which
includes new seat backrest links; replacement with new links if
cracking is found; and eventual replacement of all links with new
links. We issued AD 2014-20-11 to detect and correct cracking of
backrest links, which could affect the structural integrity of seat
backrests. Failure of the backrest links could result in injury to an
occupant during emergency landing conditions.
AD 2014-20-11, Amendment 39-17984 (79 FR 60322, October 7, 2014),
corresponds to Mandatory Continuing Airworthiness Information (MCAI)
European Aviation Safety Agency Airworthiness Directive 2012-0038,
dated March 12, 2012. You may examine the MCAI on the Internet at
https://www.regulations.gov by searching for and locating Docket No.
FAA-2015-1282.
Since we issued AD 2014-20-11, Amendment 39-17984 (79 FR 60322,
October 7, 2014), we have determined that, in paragraph (c)(1) of AD
2014-20-11, a model designation incorrectly specified ``A320-300''
instead of ``A330-300'' as one of the models that the affected
passenger seats might be installed on. Therefore, we have determined
that paragraph (c)(1) of this AD should read as follows: Airbus Model
A330-200, A330-200 Freighter, and A330-300 series airplanes.
We have also re-designated paragraph (l) of AD 2014-20-11,
Amendment 39-17984 (79 FR 60322, October 7, 2014), as paragraph (l)(1)
of this AD. We also added a new paragraph (l)(2) to this AD to provide
information on the availability of service information that is not
incorporated by reference in this AD.
FAA's Determination and Requirements of This AD
This product has been approved by the aviation authority of another
country, and is approved for operation in the United States. Pursuant
to our bilateral agreement with the State of Design Authority, we have
been notified of the unsafe condition described in the MCAI and service
information referenced above. We are issuing this AD because we
evaluated all pertinent information and determined the unsafe condition
exists and is likely to exist or develop on other products of these
same type designs.
FAA's Determination of the Effective Date
Since there are currently no domestic operators of airplanes that
are equipped with this product, notice and opportunity for public
comment before issuing this AD are unnecessary.
Comments Invited
This AD is a final rule that involves requirements affecting flight
safety, and we did not precede it by notice and opportunity for public
comment. We invite you to send any written relevant data, views, or
arguments about this AD. Send your comments to an address listed under
the ADDRESSES section. Include ``Docket No. FAA-2015-1282; Directorate
Identifier 2015-NM-007-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 https://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 0 seat assemblies installed on,
but not limited to, transport airplanes of U.S. registry.
[[Page 30351]]
The actions required by AD 2014-20-11, Amendment 39-17984 (79 FR
60322, October 7, 2014), and retained in this AD take about 1 work-hour
per product, at an average labor rate of $85 per work-hour. Required
parts cost about $227 per product. Based on these figures, the
estimated cost of the actions that were required by AD 2014-20-11 is
$312 per product.
Since this AD only clarifies airplane models on which the affected
passenger seat assemblies might be installed, this AD adds no
additional economic burden.
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 that 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);
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)
2014-20-11, Amendment 39-17984 (79 FR 60322, October 7, 2014), and
adding the following new AD:
2015-10-02 Zodiac Seats France (formerly Sicma Aero Seat): Amendment
39-18157. Docket No. FAA-2015-1282; Directorate Identifier 2015-NM-
007-AD.
(a) Effective Date
This AD becomes effective June 12, 2015.
(b) Affected ADs
This AD replaces AD 2014-20-11, Amendment 39-17984 (79 FR 60322,
October 7, 2014).
(c) Applicability
This AD applies to Zodiac Seats France 9140, 9166, 9173, 9174,
9184, 9188, 9196, 91B7, 91B8, 91C0, 91C2, 91C4, 91C5, 91C9, 9301,
and 9501 series passenger seat assemblies; identified in Annex 1,
Issue 3, dated January 25, 2012, of Sicma Aero Seat Service Bulletin
90-25-012, Issue 6, dated January 25, 2012. These passenger seat
assemblies are installed on, but not limited to, the airplanes
identified in paragraphs (c)(1), (c)(2), and (c)(3) of this AD,
certificated in any category.
(1) Airbus Model A330-200, A330-200 Freighter, and A330-300
series airplanes.
(2) Airbus Model A340-200, A340-300, A340-500, and A340-600
series airplanes.
(3) The Boeing Company Model 777-200, 777-200LR, 777-300, 777-
300ER, and 777F series airplanes.
(d) Subject
Air Transport Association (ATA) of America Code 25, Equipment/
Furnishings.
(e) Reason
This AD was prompted by a report of cracks in the backrest links
on certain seats and also by a determination that a model
designation specified in paragraph (c)(1) of AD 2014-20-11,
Amendment 39-17984 (79 FR 60322, October 7, 2014) was incorrect. We
are issuing this AD to detect and correct cracks in the backrest
links, which could affect the structural integrity of seat
backrests. Failure of the backrest links could result in injury to
an occupant during emergency landing conditions.
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
(g) Retained Repetitive Inspections, With No Changes
This paragraph restates the requirements of paragraph (g) of AD
2014-20-11, Amendment 39-17984 (79 FR 60322, October 7, 2014), with
no changes. At the later of the times specified in paragraphs (g)(1)
and (g)(2) of this AD: Do a general visual inspection for cracking
of seat backrest links having part number (P/N) 90-000200-104-1, P/N
90-000200-104-2, P/N 90-000202-104-1, and P/N 90-000202-104-2, in
accordance with the ``PART ONE: GENERAL INTERMEDIATE CHECKING
PROCEDURE'' of the Accomplishment Instructions of Sicma Aero Seat
Service Bulletin 90-25-012, Issue 6, dated January 25, 2012,
including Annex 1, Issue 3, dated January 25, 2012. If no cracking
is found on any link, repeat the inspection thereafter at intervals
not to exceed 900 flight hours on the seat or 5 months since the
most recent inspection, whichever occurs later, until the
replacement specified in paragraph (i) of this AD is done.
(1) Within 6,000 flight hours on the seat or 2 years, whichever
occurs later after the seat manufacturing date or after the backrest
link replacement.
(2) Within 900 flight hours on the seat after October 22, 2014
(the effective date AD 2014-20-11, Amendment 39-17984 (79 FR 60322,
October 7, 2014)), but no later than 5 months after October 22,
2014.
(h) Retained Corrective Actions, With No Changes
This paragraph restates the requirements of paragraph (h) of AD
2014-20-11, Amendment 39-17984 (79 FR 60322, October 7, 2014), with
no changes.
(1) If, during any inspection required by paragraph (g) of this
AD, any cracking is found on the link and no crack length exceeds
the lock-out pin-hole as specified in Figure 2 or 4, as applicable,
of Sicma Aero Seat Service Bulletin 90-25-012, Issue 6, dated
January 25, 2012, including Annex 1, Issue 3, dated January 25,
2012: Within 600 flight hours on the seat or 3 months, whichever
occurs later after crack identification, replace the cracked link
with a new link, in accordance with ``PART TWO: ROUTINE REPLACEMENT
PROCEDURE (EXCEPT FOR SERIES 91B7, 91B8 & 91C5)'' or ``PART THREE:
ROUTINE REPLACEMENT PROCEDURE (FOR SERIES 91B7, 91B8 & 91C5)'' of
the Accomplishment Instructions of Sicma Aero Seat Service Bulletin
90-25-012, Issue 6, dated January 25, 2012, including Annex 1, Issue
3, dated January 25, 2012.
(2) If, during any inspection required by paragraph (g) of this
AD, any cracking is found on the link and any crack length exceeds
the lock-out pin-hole as specified in Figure 2 or 4, as applicable,
of Sicma Aero Seat Service Bulletin 90-25-012, Issue 6, dated
January 25, 2012, including Annex 1, Issue 3, dated January 25,
2012: Before
[[Page 30352]]
further flight, replace the cracked link with a new link, in
accordance with ``PART TWO: ROUTINE REPLACEMENT PROCEDURE (EXCEPT
FOR SERIES 91B7, 91B8 & 91C5)'' or ``PART THREE: ROUTINE REPLACEMENT
PROCEDURE (FOR SERIES 91B7, 91B8 & 91C5)'' of the Accomplishment
Instructions of Sicma Aero Seat Service Bulletin 90-25-012, Issue 6,
dated January 25, 2012, including Annex 1, Issue 3, dated January
25, 2012.
(i) Retained Replacement, With No Changes
This paragraph restates the requirements of paragraph (i) of AD
2014-20-11, Amendment 39-17984 (79 FR 60322, October 7, 2014), with
no changes. At the later of the times specified in paragraphs (i)(1)
and (i)(2) of this AD: Replace all seat backrest links, having P/N
90-000200-104-1, P/N 90-000200-104-2, P/N 90-000202-104-1, and P/N
90-000202-104-2, with new links, in accordance with ``PART TWO:
ROUTINE REPLACEMENT PROCEDURE (EXCEPT FOR SERIES 91B7, 91B8 &
91C5)'' or ``PART THREE: ROUTINE REPLACEMENT PROCEDURE (FOR SERIES
91B7, 91B8 & 91C5)'' of the Accomplishment Instructions of Sicma
Aero Seat Service Bulletin 90-25-012, Issue 6, dated January 25,
2012, including Annex 1, Issue 3, dated January 25, 2012.
(1) Within 12,000 flight hours on the seat or 4 years, whichever
occurs later after the seat manufacturing date or after the backrest
link replacement.
(2) Within 3,500 flight hours on the seat after October 22, 2014
(the effective date AD 2014-20-11, Amendment 39-17984 (79 FR 60322,
October 7, 2014), but no later than 18 months after October 22,
2014.
(j) Retained Credit for Previous Actions, With No Changes
This paragraph restates the credit provided in paragraph (j) of
AD 2014-20-11, Amendment 39-17984 (79 FR 60322, October 7, 2014),
with no changes. This paragraph provides credit for actions required
by paragraphs (g), (h), and (i) of this AD, if those actions were
performed before October 22, 2014 (the effective date AD 2014-20-11,
Amendment 39-17984 (79 FR 60322, October 7, 2014), using the service
information specified in paragraph (j)(1), (j)(2), or (j)(3) of this
AD.
(1) Sicma Aero Seat Service Bulletin 90-25-012, Issue 3, dated
October 3, 2001, which is not incorporated by reference in this AD.
(2) Sicma Aero Seat Service Bulletin 90-25-012, Issue 4, dated
December 19, 2001, which is not incorporated by reference in this
AD.
(3) Sicma Aero Seat Service Bulletin 90-25-012, Issue 5, dated
March 19, 2004, including Annex 1, Issue 2, dated March 19, 2004,
which was incorporated by reference in AD 2011-07-05, Amendment 39-
16642 (76 FR 18020, April 1, 2011).
(k) Other FAA AD Provisions
The following provisions also apply to this AD:
(1) Alternative Methods of Compliance (AMOCs): The Manager,
Boston 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 ACO, send it to ATTN: Ian Lucas, Aerospace Engineer, Boston ACO,
ANE-150, FAA, Engine and Propeller Directorate, 12 New England
Executive Park, Burlington, MA 01803; phone: 781-238-7757; fax: 781-
238-7170; email: ian.lucas@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, Boston ACO,
FAA; or the European Aviation Safety Agency (EASA).
(l) Related Information
(1) Refer to Mandatory Continuing Airworthiness Information
(MCAI) EASA Airworthiness Directive 2012-0038, dated March 12, 2012,
for related information. You may examine the MCAI on the Internet at
https://www.regulations.gov by searching for and locating Docket No.
FAA-2015-1282.
(2) Service information identified in this AD that is not
incorporated by reference is available at the addresses specified in
paragraphs (m)(4) and (m)(5) of this AD.
(m) 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
October 22, 2014 (79 FR 60322, October 7, 2014).
(i) Sicma Aero Seat Service Bulletin 90-25-012, Issue 6, dated
January 25, 2012, including Annex 1, Issue 3, dated January 25,
2012.
(ii) Reserved.
(4) For service information identified in this AD, contact
Zodiac Seats France, 7, Rue Lucien Coupet, 36100 ISSOUDUN, France;
telephone +33 (0) 2 54 03 39 39; fax +33 (0) 2 54 03 39 00; email
customerservices@sicma.zodiac.com; Internet https://www.sicma.zodiacaerospace.com/en/.
(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 202-741-6030, or go to: https://www.archives.gov/federal-register/cfr/ibr-locations.html.
Issued in Renton, Washington, on May 4, 2015.
Jeffrey E. Duven,
Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 2015-11392 Filed 5-27-15; 8:45 am]
BILLING CODE 4910-13-P
