Airworthiness Directives; Zodiac Aerotechnics Oxygen Mask Regulators, 4987-4991 [2019-02748]
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Federal Register / Vol. 84, No. 34 / Wednesday, February 20, 2019 / Rules and Regulations
in paragraphs (e)(1)(i) and (ii) of this
section.
(2) The first submission by any central
counterparty that is a covered reporter
as of the effective date of this Section
shall be submitted on the first business
day after the applicable compliance date
under paragraph (e)(1) of this section.
DEPARTMENT OF TRANSPORTATION
Note 1 to paragraph (e)(2): For example, if
this section became effective on March 20,
2019, a central counterparty that meets the
dollar threshold specified in paragraph (b)(2)
of this section for the calendar quarter ending
December 31, 2018, would be required to
submit its first report under paragraph
(e)(1)(i) of this section on the first business
day after September 16, 2019, its first report
under paragraph (e)(1)(ii) of this section on
November 15, 2019, and its first report with
data elements requiring an LEI (other than
that of the covered reporter) on May 13, 2020
(if the covered reporter effected the
rulemaking described in paragraph (e)(1)(iii)
of this section).
RIN 2120–AA64
(3) Any central counterparty that
becomes a covered reporter after the
effective date of this Section shall
comply with the reporting requirements
pursuant to this Section beginning on
the later of the schedule set forth in
paragraphs (e)(1)(i) through (iii) of this
section or the first business day of the
third calendar quarter following the
calendar quarter in which such central
counterparty meets the dollar threshold
specified in paragraph (b)(2) of this
section.
Note 2 to paragraph (e)(3): For example, if
this section became effective on March 20,
2019, a central counterparty that first meets
the dollar threshold specified in paragraph
(b)(2) of this section for the calendar quarter
ending June 30, 2019, would be required to
submit its first report under paragraphs
(e)(1)(i) and (ii) of this section on January 2,
2020, and its first report with data elements
requiring an LEI (other than that of the
covered reporter) on May 13, 2020 (if the
covered reporter effected the rulemaking
described in paragraph (e)(1)(iii) of this
section by May 13, 2020).
Note 3 to paragraph (e)(3): For example, if
this section became effective on March 20,
2019, a central counterparty that first met the
dollar threshold specified in paragraph (b)(2)
for the calendar quarter ending June 30, 2020,
would be required to comply with all of the
reporting requirements under this section on
January 2, 2021 (and would continue to be
required to report all data elements requiring
a legal name or internal identifier for at least
365 days after the effective date of the
covered reporter’s rulemaking described in
paragraph (e)(1)(iii) if such effective date
occurred after January 2, 2021).
Ryan D. Brady,
Executive Secretary, Department of the
Treasury.
[FR Doc. 2019–02639 Filed 2–19–19; 8:45 am]
BILLING CODE 4810–25–P
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Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2017–0505; Product
Identifier 2017–NE–15–AD; Amendment 39–
19472; AD 2018–21–14]
Airworthiness Directives; Zodiac
Aerotechnics Oxygen Mask Regulators
Federal Aviation
Administration (FAA), DOT.
ACTION: Final rule.
AGENCY:
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–2017–
0505; or in person at Docket Operations
between 9 a.m. and 5 p.m., Monday
through Friday, except Federal holidays.
The AD docket contains this final rule,
the mandatory continuing airworthiness
information (MCAI), the regulatory
evaluation, any comments received, and
Fmt 4700
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Erin
King, Aerospace Engineer, Boston ACO
Branch, FAA, 1200 District Avenue,
Burlington, MA 01803; phone 781–238–
7655; fax: 781–238–7199; email:
erin.king@faa.gov.
FOR FURTHER INFORMATION CONTACT:
Discussion
We are adopting a new
airworthiness directive (AD) for certain
Zodiac Aerotechnics (Zodiac) oxygen
mask regulators. This AD was prompted
by reports that certain silicon harness
inflation hoses installed on certain flight
crew quick donning mask harnesses
have shown an unusually high
premature rupture rate. This AD
requires inspection and replacement of
certain oxygen mask regulator harness
inflation hoses. We are issuing this AD
to address the unsafe condition on these
products.
DATES: This AD is effective March 27,
2019.
The Director of the Federal Register
approved the incorporation by reference
of a certain publication listed in this AD
as of March 27, 2019.
ADDRESSES: For service information
identified in this final rule, contact
Zodiac Aerotechnics, 61 rue Pierre
Curie BP 1, 78373 Plaisir, CEDEX,
France; phone: +33 1 6486 6964; email:
Christophe.besset@
zodiacaerospace.com or Yann.laine@
zodiacaerospace.com. You may view
this service information at the FAA,
Engine & Propeller Standards Branch,
1200 District Avenue, Burlington, MA
01803. For information on the
availability of this material at the FAA,
call 781–238–7759. It is also available
on the internet at https://
www.regulations.gov by searching for
and locating Docket No. FAA–2017–
0505.
Frm 00037
other information. The address for
Docket Operations (phone: 800–647–
5527) is U.S. Department of
Transportation, Docket Operations, M–
30, West Building Ground Floor, Room
W12–140, 1200 New Jersey Avenue SE,
Washington, DC 20590.
SUPPLEMENTARY INFORMATION:
SUMMARY:
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We issued a notice of proposed
rulemaking (NPRM) to amend 14 CFR
part 39 by adding an AD that would
apply to certain Zodiac oxygen mask
regulators. The NPRM published in the
Federal Register on September 25, 2017
(82 FR 44539). The NPRM was
prompted by reports that certain silicon
harness inflation hoses installed on
certain flight crew quick donning mask
harnesses have shown an unusually
high premature rupture rate. The NPRM
proposed to require an inspection and
replacement of oxygen mask regulator
harness inflation hoses. We are issuing
this AD to address the unsafe condition
on these products.
The European Union Aviation Safety
Agency (EASA), which is the Technical
Agent for the Member States of the
European Community, has issued EASA
AD 2014–0142, Revision 01, dated June
11, 2014 (referred to after this as ‘‘the
MCAI’’), to address the unsafe condition
on these products. The MCAI states:
Recent reported occurrences have shown
that for harness hoses P/N 445952, installed
on certain flight crew quick donning mask
harnesses (also known as ‘comfort’ harness)
having P/N MXH21–1, suspected silicon
batches may have been used during
manufacture, which have shown an
unusually high premature rupture rate. The
affected P/N MXH21–1 inflatable harness
assembly consists of two main parts that can
be disassembled; the harness itself and the
harness inflation hose, P/N 445952.
This condition, if not detected and
corrected, could lead, in case of a sudden
depressurization event, to a harness rupture,
thereby providing inadequate protection
against hypoxia of the affected flight crew
member, possibly resulting in
unconsciousness and consequent reduced
control of the aeroplane.
You may obtain further information
by examining the MCAI in the AD
docket on the internet at https://
www.regulations.gov by searching for
and locating Docket No. FAA–2017–
0505.
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Comments
We gave the public the opportunity to
participate in developing this final rule.
The following presents the comments
received on the NPRM and the FAA’s
response to each comment.
Comment To Figure Reference in
Service Information
NetJets Aviation, Inc. (NetJets)
commented that Accomplishment
Instructions, paragraph 3.A.(1) of Zodiac
Aerospace Service Bulletin (SB) MC10–
35–274, Revision 02, dated June 25,
2014, references Figure 3; however,
there are only Figures 1 and 2 in this
SB.
We agree that Zodiac Aerospace SB
MC10–35–274, Revision 02, dated June
25, 2014, references Figure 3 in error.
The FAA, however, is not responsible
for administrative errors in SBs. We did
not change this AD.
Request To Revise Part for Installation
Eligibility
American Airlines (AA) requested
that we revise the phrase in paragraph
(h)(2) of the NPRM from ‘‘inflatable
harness assembly’’ to ‘‘crew oxygen
mask regulator.’’ AA reasoned that
paragraph 1.A.(1) of Zodiac Aerospace
SB MC10–35–274, Revision 02, dated
June 25, 2014, includes both the
inflatable harness assembly part
numbers (P/Ns) as well as the crew
oxygen mask regulator P/Ns. The intent
is to check the crew oxygen mask
regulator for installation eligibility.
We agree. We revised the paragraphs
in this AD that refer to parts eligible for
installation as the ‘‘crew oxygen mask
regulator.’’
Request To Add Credit for Previous
Actions Paragraph
AA and NetJets requested that we add
a Credit For Previous Actions paragraph
to this AD. AA asked that we give credit
for actions required by this AD if those
actions were performed before the
effective date of this AD using Zodiac
Aerospace SB MC10–35–274, Revision
01, dated April 18, 2014, or Original
Issue, dated March 19, 2014. NetJets
asked that in addition to the SBs
mentioned above, we also give credit for
using EASA AD 2014–0142, Revision
01, dated June 11, 2014, to accomplish
the actions required by this AD. AA
reasoned that EASA AD 2014–0142,
Revision 01, dated June 11, 2014, allows
for compliance with earlier revisions of
the service information.
We partially agree. We agree to give
credit for accomplishing the required
actions if operators used Zodiac
Aerospace SB MC10–35–274, Revision
01, dated April 18, 2014, or Zodiac
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Aerospace SB MC10–35–274, Original
Issue, dated March 19, 2014, because
this meets the intended safety
requirements of this AD. We added a
Credit For Previous Actions paragraph
to this AD.
We disagree with revising the AD to
allow for previous credit for performing
EASA AD 2014–0142, Revision 01,
dated June 11, 2014, because this is not
necessary and is inconsistent with how
we draft ADs.
Request To Clarify the Oxygen Mask
Regulator Prohibition
AA, NetJets, and United Airlines
(United) requested clarification
regarding the oxygen mask regulator
prohibition in the Installation
Prohibition paragraph of this AD. The
commenters reasoned that paragraph
(h)(1), as proposed in the NPRM,
prohibited the installation of certain
oxygen mask regulators; whereas,
paragraphs (h)(2) and (3) in the NPRM
describe criteria that allow installation.
AA requested that we remove paragraph
(h)(1) of this AD. NetJets requested
clarification and possible rewording of
paragraph (h)(1) of this AD. United
suggested rewording and reformatting of
paragraph (h)(1) of this AD.
We partially agree. We agree that we
need to clarify this AD to more clearly
describe when a flight crew oxygen
mask regulator is eligible for
installation. We revised the Installation
Prohibition paragraph by moving
paragraphs (h)(2) and (3) into a
Definition paragraph. We also revised
paragraph (h)(1) of the NPRM, now
paragraph (h) in the final rule, to allow
the installation of certain oxygen mask
regulators when they meet the criteria
specified in paragraph (i)(1) of this AD.
We disagree with removing paragraph
(h)(1) from this AD (paragraph (h) in the
final rule) because oxygen mask
regulators with a P/N listed in
Paragraph 1.A.(1) of Zodiac Aerospace
SB MC10–35–274, Revision 02, dated
June 25, 2014, cannot be installed
unless they meet the criteria specified in
paragraph (i), Definition, of this AD.
Request To Remove Hose Part Numbers
United requested that we clarify
references to specific harness inflation
hose P/Ns in the Applicability
paragraph, paragraph (c), and the
Required Actions paragraph,
specifically paragraphs (g)(2) and (3), of
this AD. United noted that these P/Ns
are not identified on the inflation
harness assemblies after the hoses are
installed on a crew oxygen mask
assembly. United reasoned that
although detailed shop records would
likely itemize the hose P/Ns, they are
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unaware of any parts ‘data plate’ or ‘data
tag’ on the inflation harness assemblies
that identify the hose P/Ns after they are
installed on a crew oxygen mask
assembly.
We partially agree. We agree that the
hose P/Ns are not required in the
Applicability paragraph of this AD. We
revised the applicability, paragraph (c),
of this AD by removing the references to
the installation hose and its P/Ns.
We disagree with removing the hose
P/Ns from paragraphs (g)(2) and (3) of
this AD. Although the commenter
correctly points out that there is no data
tag or data plate affixed to the hose,
these P/Ns are useful to operators who
can determine the hose P/N.
Additionally, identifying the hose P/Ns
in this AD is consistent with EASA AD
2014–0142, Revision 01, dated June 11,
2014.
Request To Increase the Compliance
Time
United and AA requested,
respectively, that we increase the
compliance time from 24 months to 36
or to 48 months. The commenters
reasoned that operators experienced
supply issues when trying to comply
with AD 2015–08–07 and many
operators requested extensions to the
compliance time. The supply situation
was worsened because some oxygen
mask regulator harnesses needed to be
replaced because of illegible or nonexistent part marking.
We partially agree. We agree to
increase the compliance time to 36
months to ensure that suppliers can
provide the parts because of the
possibility there will be supply issues.
Zodiac has not been able to determine
inventory because they do not know the
number of parts in use by U.S.
operators. Increasing the compliance
time by 12 months still meets the safety
objectives of this AD. Our
understanding from Zodiac is that they
recommend hose replacement every 72
months, and given that all of the
affected hoses were manufactured
between 2008 and 2010, many of the
affected hoses likely have been removed
from service.
We disagree with increasing the
compliance time to 48 months because
36 months is sufficient to comply with
the required actions of this AD.
Additionally, we do not want to extend,
beyond a reasonable time, the period for
which suspect parts can remain on
aircraft. We revised paragraph (g)(1) of
this AD to increase the compliance time
to 36 months.
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Request To Decrease the Compliance
Time
remarking P/Ns MXH20–1 and MXH21–
1 with a ‘‘W.’’
The Airline Pilots Association
International (ALPA) requested that the
compliance time decrease from 24
months to 12 months. ALPA reasoned
that greater than 40 months have passed
since EASA AD 2014–0142, Revision
01, dated June 11, 2014, became
effective. ALPA also noted that the
required time to comply with the AD is
one work-hour. Based on these factors
the compliance time of this AD should
be decreased to minimize risk.
We disagree. We note that operators
may have difficulty obtaining
replacement parts within a shortened
compliance time. Also, the compliance
time of 36 months after the effective
date of this AD meets the safety
objectives of this AD. We did not change
this AD.
Request To Include Inflatable Harness
Assemblies Marked With an ‘‘I’’
Request To Remove the P/Ns That Are
Not Eligible for the ‘‘W’’ Marking
AA and United requested that we
remove the reference to inflatable
harness assembly P/Ns that have been
re-marked with a ‘‘W’’ from the
Installation Prohibition, of this AD. The
commenters reasoned that adding a ‘‘W’’
applies only to oxygen mask regulator
assemblies that have inflation harness
assemblies, P/N MXH21–31, installed
per Zodiac Aerospace SB MA_B_C_F10–
35–260, dated October 19, 2012, or later
revisions.
We agree. When an oxygen mask is
modified per Zodiac SB MA_B_C_F10–
35–260 and marked with a ‘‘W,’’ the P/
N also changes to MXH21–31.
Therefore, only P/N MXH21–31 is
marked with a ‘‘W.’’ Paragraph (h)(3) of
the NPRM incorrectly implied that P/N
MXH20–1 and P/N MXH21–1 might
also be marked with a ‘‘W.’’ We revised
this AD by removing the reference to
AA requested that we include
inflatable harness assembly marked
with an ‘‘I’’ on the metal bushing to
Required Actions, paragraph (g)(3), of
this AD. AA reasoned that inflatable
harness assemblies with an ‘‘I’’ on the
metal bushings have been inspected and
are not affected by this AD.
We agree. Based on paragraph 2.E. of
Zodiac SB MC10–35–274, Revision 02,
dated June 25, 2014, marking an ‘‘I’’ on
the metal bushing of the inflatable
harness indicates accomplishment of
the SB. We have revised paragraph (g)(3)
of this AD to note that inflatable harness
assemblies with metal bushings marked
with an ‘‘I’’ are not affected by this AD.
Request To Delay the Installation
Prohibition Start Time
United requested that we add ‘‘within
60 days of the effective date of this AD’’
to the Installation Prohibition of this AD
to provide more time before prohibiting
the installation of the affected flight
crew oxygen mask regulators. United
reasoned that immediately restricting
the installation of the affected regulators
after the effective date of this AD is a
logistical challenge and can be
counterproductive. United is also
concerned that material orders will be
over abundantly placed to compensate
for not knowing the modification status
of their mask inventory. United believes
that offsetting the start of a parts
installation prohibition period would
not significantly increase the risk.
We disagree. Given the increased
compliance time allowed in paragraph
(g)(1) of this AD, operators should have
time to assess their inventory and make
accurate purchases to replace affected
4989
parts. It would not be in the interest of
safety to allow the period for which
suspect parts could remain on the
aircraft to continue for any period after
this AD is published. We did not change
this AD.
Conclusion
We reviewed the relevant data,
considered the comments received, and
determined that air safety and the
public interest require adopting this
final rule with the changes described
previously and minor editorial changes.
We have determined that these minor
changes:
• Are consistent with the intent that
was proposed in the NPRM for
addressing the unsafe condition; and
• Do not add any additional burden
upon the public than was already
proposed in the NPRM.
We also determined that these
changes will not increase the economic
burden on any operator or increase the
scope of this final rule.
Related Service Information Under 1
CFR Part 51
We reviewed Zodiac Aerospace SB
MC10–35–274, Revision 02, dated June
25, 2014. The SB describes procedures
for inspecting and replacing, if
necessary, oxygen mask regulator
inflatable harnesses. 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.
Costs of Compliance
We estimate that this AD affects an
unknown number of oxygen mask
regulators installed on, but not limited
to, various aircraft of U.S. registry.
We estimate the following costs to
comply with this AD:
ESTIMATED COSTS
Action
Labor cost
Date of manufacturing code review .............................
Hose replacement ........................................................
0.1 work-hours × $85 per hour = $8.50 .......................
0.3 work-hours × $85 per hour = $25.50 .....................
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.
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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
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Parts cost
$0
1,465.00
Cost per
product
$8.50
1,490.50
because it addresses an unsafe condition
that is likely to exist or develop on
products identified in this rulemaking
action.
This AD is issued in accordance with
authority delegated by the Executive
Director, Aircraft Certification Service,
as authorized by FAA Order 8000.51C.
In accordance with that order, issuance
of ADs is normally a function of the
Compliance and Airworthiness
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Division, but during this transition
period, the Executive Director has
delegated the authority to issue ADs
applicable to engines, propellers, and
associated appliances to the Manager,
Engine and Propeller Standards Branch,
Policy and Innovation Division.
Regulatory Findings
This AD will not have federalism
implications under Executive Order
13132. This AD will not have a
substantial direct effect on the States, on
the relationship between the national
government and the States, or on the
distribution of power and
responsibilities among the various
levels of government.
For the reasons discussed above, I
certify 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
1. The authority citation for part 39
continues to read as follows:
■
Authority: 49 U.S.C. 106(g), 40113, 44701.
§ 39.13
[Amended]
2. The FAA amends § 39.13 by adding
the following new airworthiness
directive (AD):
■
2018–21–14 Zodiac Aerotechnics (formerly
Intertechnique): Amendment 39–19472;
Docket No. FAA–2017–0505; Product
Identifier 2017–NE–15–AD.
(a) Effective Date
This AD is effective March 27, 2019.
(b) Affected ADs
None.
(c) Applicability
This AD applies to Zodiac Aerotechnics
(Zodiac) MC10 series crew oxygen mask
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regulators fitted with an inflatable harness
assembly, part number (P/N) MXH20–1 or
MXH21–1.
is acceptable to make the determination,
provided those records can be relied upon for
that purpose.
(d) Subject
Joint Aircraft System Component (JASC)
Code 3510, Crew Oxygen System.
(h) Installation Prohibition
(e) Unsafe Condition
This AD was prompted by reports that
certain silicon harness inflation hoses
installed on certain flight crew quick
donning mask harnesses (also known as
‘comfort’ harness) have shown an unusually
high premature rupture rate. We are issuing
this AD to prevent a harness rupture during
a sudden depressurization event. The unsafe
condition, if not addressed, could result in
hypoxia and subsequent unconsciousness of
the affected flight crew member, and
consequent reduced control of the aircraft.
(f) Compliance
Comply with this AD within the
compliance times specified, unless already
done.
(g) Required Actions
(1) Within 36 months after the effective
date of this AD, determine the date of
manufacturing (DMF) code of each inflatable
harness assembly, P/N MXH20–1 and P/N
MXH21–1, fitted to a flight crew oxygen
mask regulator, having a P/N listed in
Planning Information, paragraph 1.A.(1), of
Zodiac Aerospace Service Bulletin (SB)
MC10–35–274, Revision 02, dated June 25,
2014. A review of airplane delivery or
maintenance records is acceptable to make
the determination as specified in this
paragraph, provided those records can be
relied upon for that purpose, and the DMF
of the inflatable harness assembly, P/N
MXH20–1 or P/N MXH21–1, as applicable,
can be conclusively identified from that
review.
(2) If during the review required by
paragraph (g)(1) of this AD, the DMF code of
the inflatable harness assembly, P/N
MXH20–1 or P/N MXH21–1, is found to be
between 0850–S and 1051–S (inclusive):
Within 36 months after the effective date of
this AD, replace the harness inflation hose,
P/N 445186 or P/N 445952, as applicable,
with a part eligible for installation, or remove
the inflatable harness assembly from the
mask regulator and replace it with an
inflatable harness assembly eligible for
installation.
(3) An oxygen mask regulator equipped
with an inflatable harness assembly, P/N
MXH20–1 or P/N MXH21–1, having a DMF
code of November 2008 (0845–S or 08/45–S)
or earlier, and those with a DMF code of
January 2011 (1101–S or 11/01–S) or later,
are excluded from the requirements of this
AD, provided it can be demonstrated that
neither the inflatable harness assembly, nor
the harness inflation hose, P/N 445186 or P/
N 445952, as applicable, was replaced on that
mask. An oxygen mask regulator with an
inflatable harness assembly, P/N MXH20–1
or P/N MXH21–1, and with an inflatatable
harness assembly with a metal bushing that
has been marked with an ‘‘I’’ is also excluded
from the requirements of this AD. A review
of airplane delivery or maintenance records
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After the effective date of this AD, do not
install on any airplane a flight crew oxygen
mask regulator with a P/N listed in Planning
Information, paragraph 1.A.(1), of Zodiac SB
MC10–35–274, Revision 02, dated June 25,
2014, unless it meets the definition of a part
eligible for installation in paragraph (i) of this
AD.
(i) Definition
(1) After the effective date of this AD, a
part eligible for installation is a crew oxygen
mask regulator with:
(i) A P/N identified in Planning
Information, paragraph 1.A.(1), of Zodiac
Aerospace SB MC10–35–274, Revision 02,
dated June 25, 2014, provided it has been
determined that a P/N MXH20–1 or P/N
MXH21–1 inflatable harness installed on that
crew oxygen mask regulator has been
inspected, and re-marked with an ‘‘I’’ as
required by Material Information, paragraph
2.E. of Zodiac Aerospace SB MC10–35–274,
Revision 02, dated June 25, 2014; or
(ii) a P/N identified in Planning
Information, paragraph 1.A.(1), of Zodiac
Aerospace SB MC10–35–274, Revision 02,
dated June 25, 2014, provided it has been
determined that an inflatable harness, P/N
MXH21–31, is installed.
(2) [Reserved]
(j) Credit for Previous Actions
You may take credit for the inspection and
replacement of the oxygen mask regulator
harness inflation hose required by paragraphs
(g)(1) and (2) of this AD, if you performed the
inspection and replacement using the
Accomplishment Instructions, paragraph 3,
of Zodiac Aerospace SB MC10–35–274,
Initial Issue, dated March 19, 2014, or
Revision 01, dated April 18, 2014.
(k) Alternative Methods of Compliance
(AMOCs)
(1) The Manager, FAA, Boston ACO
Branch, Compliance and Airworthiness
Division, has the authority to approve
AMOCs for this AD, if requested using the
procedures found in 14 CFR 39.19. In
accordance with 14 CFR 39.19, send your
request to your principal inspector or local
Flight Standards District Office, as
appropriate. If sending information directly
to the manager of the ACO Branch, send it
to the attention of the person identified in
paragraph (l)(1) of this AD. You may email
your request to: ANE-AD-AMOC@faa.gov.
(2) Before using any approved AMOC,
notify your appropriate principal inspector,
or lacking a principal inspector, the manager
of the local flight standards district office/
certificate holding district office.
(l) Related Information
(1) For more information about this AD,
contact Erin King, Aerospace Engineer,
Boston ACO Branch, FAA, 1200 District
Avenue, Burlington, MA 01803; phone 781–
238–7655; fax: 781–238–7199; email:
erin.king@faa.gov.
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20FER1
Federal Register / Vol. 84, No. 34 / Wednesday, February 20, 2019 / Rules and Regulations
(2) Refer to European Union Aviation
Safety Agency AD 2014–0142, Revision 01,
dated June 11, 2014, for more information.
You may examine the EASA AD in the AD
docket on the internet at https://
www.regulations.gov by searching for and
locating Docket No. FAA–2017–0505.
(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 the AD specifies otherwise.
(i) Zodiac Aerospace Service Bulletin
MC10–35–274, Revision 02, dated June 25,
2014.
(ii) [Reserved]
(3) For service information identified in
this AD, contact Zodiac Aerotechnics, 61 rue
Pierre Curie BP 1, 78373 Plaisir, CEDEX,
France; phone: +33 1 6486 6964; email:
Christophe.besset@zodiacaerospace.com or
Yann.laine@zodiacaerospace.com.
(4) You may view this service information
at FAA, Engine & Propeller Standards
Branch, 1200 District Avenue, Burlington,
MA 01803. For information on the
availability of this material at the FAA, call
781–238–7759.
(5) 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 Burlington, Massachusetts, on
February 13, 2019.
Robert J. Ganley,
Manager, Engine and Propeller Standards
Branch, Aircraft Certification Service.
[FR Doc. 2019–02748 Filed 2–19–19; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 71
[Docket No. FAA–2018–0256; Airspace
Docket No. 18–AEA–11]
RIN 2120–AA66
Amendment of Class D Airspace and
Class E Airspace; Schenectady, NY,
Ithaca, NY, and Albany, NY
Federal Aviation
Administration (FAA), DOT.
ACTION: Final rule.
AGENCY:
This action amends Class D
airspace, Class E airspace designated as
an extension to a Class D surface area,
and Class E airspace extending upward
from 700 feet or more above the surface
SUMMARY:
VerDate Sep<11>2014
17:42 Feb 19, 2019
Jkt 247001
at Schenectady County Airport,
Schenectady, NY, and Albany, NY by
updating the geographic coordinates of
this airport, Saratoga County Airport,
Hunter NDB, and Cambridge VOR/DME.
Controlled airspace is necessary for the
safety and management of instrument
flight rules (IFR) operations at this
airport. This action also replaces the
outdated term Airport/Facility Directory
with the term Chart Supplement in the
legal descriptions of associated Class D
and E airspace of Schenectady County
Airport, Schenectady, NY, and Ithaca
Tompkins Regional Airport, Ithaca, NY.
In addition, subsequent to publication,
it was noted that the Cambridge VOR/
DME was identified as VORTAC. This
action corrects the error.
DATES: Effective 0901 UTC, April 25,
2019. The Director of the Federal
Register approves this incorporation by
reference action under Title 1 Code of
Federal Regulations part 51, subject to
the annual revision of FAA Order
7400.11 and publication of conforming
amendments.
ADDRESSES: FAA Order 7400.11C,
Airspace Designations and Reporting
Points, and subsequent amendments can
be viewed online at https://www.faa.gov/
air_traffic/publications/. For further
information, you can contact the
Airspace Policy Group, Federal Aviation
Administration, 800 Independence
Avenue SW, Washington, DC, 20591;
telephone: (202) 267–8783. The Order is
also available for inspection at the
National Archives and Records
Administration (NARA). For
information on the availability of FAA
Order 7400.11C at NARA, call (202)
741–6030, or go to https://
www.archives.gov/federal-register/cfr/
ibr-locations.html.
FAA Order 7400.11, Airspace
Designations and Reporting Points, is
published yearly and effective on
September 15.
FOR FURTHER INFORMATION CONTACT: John
Fornito, Operations Support Group,
Eastern Service Center, Federal Aviation
Administration, 1701 Columbia Avenue,
College Park, GA 30337; telephone (404)
305–6364.
SUPPLEMENTARY INFORMATION:
Authority for This Rulemaking
The FAA’s authority to issue rules
regarding aviation safety is found in
Title 49 of the United States Code.
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. This rulemaking is
promulgated under the authority
described in Subtitle VII, Part A,
PO 00000
Frm 00041
Fmt 4700
Sfmt 4700
4991
Subpart I, Section 40103. Under that
section, the FAA is charged with
prescribing regulations to assign the use
of airspace necessary to ensure the
safety of aircraft and the efficient use of
airspace. This regulation is within the
scope of that authority as it amends
Class D airspace and Class E airspace at
Schenectady County Airport,
Schenectady, NY, Ithaca Tompkins
Regional Airport, Ithaca, NY, and
Saratoga County Airport, Albany, NY to
support IFR operations at these airports.
History
The FAA published a notice of
proposed rulemaking in the Federal
Register (83 FR 60378, November 26,
2018) for Docket No. FAA–2018–0256 to
amend Class D airspace and Class E
airspace at Schenectady County Airport,
Schenectady, NY, Ithaca Tompkins
Regional Airport, Ithaca, NY, and
Saratoga County Airport, Albany, NY to
support IFR operations at these airports.
Interested parties were invited to
participate in this rulemaking effort by
submitting written comments on the
proposal to the FAA. No comments
were received.
Class D and Class E airspace
designations are published in
paragraphs 5000, 6002, 6004, and 6005,
respectively, of FAA Order 7400.11C
dated August 13, 2018, and effective
September 15, 2018, which is
incorporated by reference in 14 CFR
part 71.1. The Class D and Class E
airspace designation listed in this
document will be published
subsequently in the Order.
Availability and Summary of
Documents for Incorporation by
Reference
This document amends FAA Order
7400.11C, Airspace Designations and
Reporting Points, dated August 13,
2018, and effective September 15, 2018.
FAA Order 7400.11C is publicly
available as listed in the ADDRESSES
section of this document. FAA Order
7400.11C lists Class A, B, C, D, and E
airspace areas, air traffic service routes,
and reporting points.
The Rule
This amendment to Title 14 Code of
Federal Regulations (14 CFR) part 71
amends Class D airspace, Class E
airspace designated as an extension to a
Class D surface area, at Schenectady
County Airport, Schenectady, NY and
Class E airspace area extending upward
from 700 feet or more above the surface
at Albany, NY, by updating the
geographic coordinates of Saratoga
County Airport, Hunter NDB, and
Cambridge VOR/DME to be in concert
E:\FR\FM\20FER1.SGM
20FER1
Agencies
[Federal Register Volume 84, Number 34 (Wednesday, February 20, 2019)]
[Rules and Regulations]
[Pages 4987-4991]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2019-02748]
=======================================================================
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2017-0505; Product Identifier 2017-NE-15-AD; Amendment
39-19472; AD 2018-21-14]
RIN 2120-AA64
Airworthiness Directives; Zodiac Aerotechnics Oxygen Mask
Regulators
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Final rule.
-----------------------------------------------------------------------
SUMMARY: We are adopting a new airworthiness directive (AD) for certain
Zodiac Aerotechnics (Zodiac) oxygen mask regulators. This AD was
prompted by reports that certain silicon harness inflation hoses
installed on certain flight crew quick donning mask harnesses have
shown an unusually high premature rupture rate. This AD requires
inspection and replacement of certain oxygen mask regulator harness
inflation hoses. We are issuing this AD to address the unsafe condition
on these products.
DATES: This AD is effective March 27, 2019.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in this AD as of March 27,
2019.
ADDRESSES: For service information identified in this final rule,
contact Zodiac Aerotechnics, 61 rue Pierre Curie BP 1, 78373 Plaisir,
CEDEX, France; phone: +33 1 6486 6964; email:
Christophe.besset@zodiacaerospace.com or
Yann.laine@zodiacaerospace.com. You may view this service information
at the FAA, Engine & Propeller Standards Branch, 1200 District Avenue,
Burlington, MA 01803. For information on the availability of this
material at the FAA, call 781-238-7759. It is also available on the
internet at https://www.regulations.gov by searching for and locating
Docket No. FAA-2017-0505.
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-2017-
0505; or in person at Docket Operations between 9 a.m. and 5 p.m.,
Monday through Friday, except Federal holidays. The AD docket contains
this final rule, the mandatory continuing airworthiness information
(MCAI), the regulatory evaluation, any comments received, and other
information. The address for Docket Operations (phone: 800-647-5527) is
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: Erin King, Aerospace Engineer, Boston
ACO Branch, FAA, 1200 District Avenue, Burlington, MA 01803; phone 781-
238-7655; fax: 781-238-7199; email: erin.king@faa.gov.
SUPPLEMENTARY INFORMATION:
Discussion
We issued a notice of proposed rulemaking (NPRM) to amend 14 CFR
part 39 by adding an AD that would apply to certain Zodiac oxygen mask
regulators. The NPRM published in the Federal Register on September 25,
2017 (82 FR 44539). The NPRM was prompted by reports that certain
silicon harness inflation hoses installed on certain flight crew quick
donning mask harnesses have shown an unusually high premature rupture
rate. The NPRM proposed to require an inspection and replacement of
oxygen mask regulator harness inflation hoses. We are issuing this AD
to address the unsafe condition on these products.
The European Union Aviation Safety Agency (EASA), which is the
Technical Agent for the Member States of the European Community, has
issued EASA AD 2014-0142, Revision 01, dated June 11, 2014 (referred to
after this as ``the MCAI''), to address the unsafe condition on these
products. The MCAI states:
Recent reported occurrences have shown that for harness hoses P/
N 445952, installed on certain flight crew quick donning mask
harnesses (also known as `comfort' harness) having P/N MXH21-1,
suspected silicon batches may have been used during manufacture,
which have shown an unusually high premature rupture rate. The
affected P/N MXH21-1 inflatable harness assembly consists of two
main parts that can be disassembled; the harness itself and the
harness inflation hose, P/N 445952.
This condition, if not detected and corrected, could lead, in
case of a sudden depressurization event, to a harness rupture,
thereby providing inadequate protection against hypoxia of the
affected flight crew member, possibly resulting in unconsciousness
and consequent reduced control of the aeroplane.
You may obtain further information by examining the MCAI in the AD
docket on the internet at https://www.regulations.gov by searching for
and locating Docket No. FAA-2017-0505.
[[Page 4988]]
Comments
We gave the public the opportunity to participate in developing
this final rule. The following presents the comments received on the
NPRM and the FAA's response to each comment.
Comment To Figure Reference in Service Information
NetJets Aviation, Inc. (NetJets) commented that Accomplishment
Instructions, paragraph 3.A.(1) of Zodiac Aerospace Service Bulletin
(SB) MC10-35-274, Revision 02, dated June 25, 2014, references Figure
3; however, there are only Figures 1 and 2 in this SB.
We agree that Zodiac Aerospace SB MC10-35-274, Revision 02, dated
June 25, 2014, references Figure 3 in error. The FAA, however, is not
responsible for administrative errors in SBs. We did not change this
AD.
Request To Revise Part for Installation Eligibility
American Airlines (AA) requested that we revise the phrase in
paragraph (h)(2) of the NPRM from ``inflatable harness assembly'' to
``crew oxygen mask regulator.'' AA reasoned that paragraph 1.A.(1) of
Zodiac Aerospace SB MC10-35-274, Revision 02, dated June 25, 2014,
includes both the inflatable harness assembly part numbers (P/Ns) as
well as the crew oxygen mask regulator P/Ns. The intent is to check the
crew oxygen mask regulator for installation eligibility.
We agree. We revised the paragraphs in this AD that refer to parts
eligible for installation as the ``crew oxygen mask regulator.''
Request To Add Credit for Previous Actions Paragraph
AA and NetJets requested that we add a Credit For Previous Actions
paragraph to this AD. AA asked that we give credit for actions required
by this AD if those actions were performed before the effective date of
this AD using Zodiac Aerospace SB MC10-35-274, Revision 01, dated April
18, 2014, or Original Issue, dated March 19, 2014. NetJets asked that
in addition to the SBs mentioned above, we also give credit for using
EASA AD 2014-0142, Revision 01, dated June 11, 2014, to accomplish the
actions required by this AD. AA reasoned that EASA AD 2014-0142,
Revision 01, dated June 11, 2014, allows for compliance with earlier
revisions of the service information.
We partially agree. We agree to give credit for accomplishing the
required actions if operators used Zodiac Aerospace SB MC10-35-274,
Revision 01, dated April 18, 2014, or Zodiac Aerospace SB MC10-35-274,
Original Issue, dated March 19, 2014, because this meets the intended
safety requirements of this AD. We added a Credit For Previous Actions
paragraph to this AD.
We disagree with revising the AD to allow for previous credit for
performing EASA AD 2014-0142, Revision 01, dated June 11, 2014, because
this is not necessary and is inconsistent with how we draft ADs.
Request To Clarify the Oxygen Mask Regulator Prohibition
AA, NetJets, and United Airlines (United) requested clarification
regarding the oxygen mask regulator prohibition in the Installation
Prohibition paragraph of this AD. The commenters reasoned that
paragraph (h)(1), as proposed in the NPRM, prohibited the installation
of certain oxygen mask regulators; whereas, paragraphs (h)(2) and (3)
in the NPRM describe criteria that allow installation. AA requested
that we remove paragraph (h)(1) of this AD. NetJets requested
clarification and possible rewording of paragraph (h)(1) of this AD.
United suggested rewording and reformatting of paragraph (h)(1) of this
AD.
We partially agree. We agree that we need to clarify this AD to
more clearly describe when a flight crew oxygen mask regulator is
eligible for installation. We revised the Installation Prohibition
paragraph by moving paragraphs (h)(2) and (3) into a Definition
paragraph. We also revised paragraph (h)(1) of the NPRM, now paragraph
(h) in the final rule, to allow the installation of certain oxygen mask
regulators when they meet the criteria specified in paragraph (i)(1) of
this AD.
We disagree with removing paragraph (h)(1) from this AD (paragraph
(h) in the final rule) because oxygen mask regulators with a P/N listed
in Paragraph 1.A.(1) of Zodiac Aerospace SB MC10-35-274, Revision 02,
dated June 25, 2014, cannot be installed unless they meet the criteria
specified in paragraph (i), Definition, of this AD.
Request To Remove Hose Part Numbers
United requested that we clarify references to specific harness
inflation hose P/Ns in the Applicability paragraph, paragraph (c), and
the Required Actions paragraph, specifically paragraphs (g)(2) and (3),
of this AD. United noted that these P/Ns are not identified on the
inflation harness assemblies after the hoses are installed on a crew
oxygen mask assembly. United reasoned that although detailed shop
records would likely itemize the hose P/Ns, they are unaware of any
parts `data plate' or `data tag' on the inflation harness assemblies
that identify the hose P/Ns after they are installed on a crew oxygen
mask assembly.
We partially agree. We agree that the hose P/Ns are not required in
the Applicability paragraph of this AD. We revised the applicability,
paragraph (c), of this AD by removing the references to the
installation hose and its P/Ns.
We disagree with removing the hose P/Ns from paragraphs (g)(2) and
(3) of this AD. Although the commenter correctly points out that there
is no data tag or data plate affixed to the hose, these P/Ns are useful
to operators who can determine the hose P/N. Additionally, identifying
the hose P/Ns in this AD is consistent with EASA AD 2014-0142, Revision
01, dated June 11, 2014.
Request To Increase the Compliance Time
United and AA requested, respectively, that we increase the
compliance time from 24 months to 36 or to 48 months. The commenters
reasoned that operators experienced supply issues when trying to comply
with AD 2015-08-07 and many operators requested extensions to the
compliance time. The supply situation was worsened because some oxygen
mask regulator harnesses needed to be replaced because of illegible or
non-existent part marking.
We partially agree. We agree to increase the compliance time to 36
months to ensure that suppliers can provide the parts because of the
possibility there will be supply issues. Zodiac has not been able to
determine inventory because they do not know the number of parts in use
by U.S. operators. Increasing the compliance time by 12 months still
meets the safety objectives of this AD. Our understanding from Zodiac
is that they recommend hose replacement every 72 months, and given that
all of the affected hoses were manufactured between 2008 and 2010, many
of the affected hoses likely have been removed from service.
We disagree with increasing the compliance time to 48 months
because 36 months is sufficient to comply with the required actions of
this AD. Additionally, we do not want to extend, beyond a reasonable
time, the period for which suspect parts can remain on aircraft. We
revised paragraph (g)(1) of this AD to increase the compliance time to
36 months.
[[Page 4989]]
Request To Decrease the Compliance Time
The Airline Pilots Association International (ALPA) requested that
the compliance time decrease from 24 months to 12 months. ALPA reasoned
that greater than 40 months have passed since EASA AD 2014-0142,
Revision 01, dated June 11, 2014, became effective. ALPA also noted
that the required time to comply with the AD is one work-hour. Based on
these factors the compliance time of this AD should be decreased to
minimize risk.
We disagree. We note that operators may have difficulty obtaining
replacement parts within a shortened compliance time. Also, the
compliance time of 36 months after the effective date of this AD meets
the safety objectives of this AD. We did not change this AD.
Request To Remove the P/Ns That Are Not Eligible for the ``W'' Marking
AA and United requested that we remove the reference to inflatable
harness assembly P/Ns that have been re-marked with a ``W'' from the
Installation Prohibition, of this AD. The commenters reasoned that
adding a ``W'' applies only to oxygen mask regulator assemblies that
have inflation harness assemblies, P/N MXH21-31, installed per Zodiac
Aerospace SB MA_B_C_F10-35-260, dated October 19, 2012, or later
revisions.
We agree. When an oxygen mask is modified per Zodiac SB MA_B_C_F10-
35-260 and marked with a ``W,'' the P/N also changes to MXH21-31.
Therefore, only P/N MXH21-31 is marked with a ``W.'' Paragraph (h)(3)
of the NPRM incorrectly implied that P/N MXH20-1 and P/N MXH21-1 might
also be marked with a ``W.'' We revised this AD by removing the
reference to remarking P/Ns MXH20-1 and MXH21-1 with a ``W.''
Request To Include Inflatable Harness Assemblies Marked With an ``I''
AA requested that we include inflatable harness assembly marked
with an ``I'' on the metal bushing to Required Actions, paragraph
(g)(3), of this AD. AA reasoned that inflatable harness assemblies with
an ``I'' on the metal bushings have been inspected and are not affected
by this AD.
We agree. Based on paragraph 2.E. of Zodiac SB MC10-35-274,
Revision 02, dated June 25, 2014, marking an ``I'' on the metal bushing
of the inflatable harness indicates accomplishment of the SB. We have
revised paragraph (g)(3) of this AD to note that inflatable harness
assemblies with metal bushings marked with an ``I'' are not affected by
this AD.
Request To Delay the Installation Prohibition Start Time
United requested that we add ``within 60 days of the effective date
of this AD'' to the Installation Prohibition of this AD to provide more
time before prohibiting the installation of the affected flight crew
oxygen mask regulators. United reasoned that immediately restricting
the installation of the affected regulators after the effective date of
this AD is a logistical challenge and can be counterproductive. United
is also concerned that material orders will be over abundantly placed
to compensate for not knowing the modification status of their mask
inventory. United believes that offsetting the start of a parts
installation prohibition period would not significantly increase the
risk.
We disagree. Given the increased compliance time allowed in
paragraph (g)(1) of this AD, operators should have time to assess their
inventory and make accurate purchases to replace affected parts. It
would not be in the interest of safety to allow the period for which
suspect parts could remain on the aircraft to continue for any period
after this AD is published. We did not change this AD.
Conclusion
We reviewed the relevant data, considered the comments received,
and determined that air safety and the public interest require adopting
this final rule with the changes described previously and minor
editorial changes. We have determined that these minor changes:
[Agr]re consistent with the intent that was proposed in
the NPRM for addressing the unsafe condition; and
Do not add any additional burden upon the public than was
already proposed in the NPRM.
We also determined that these changes will not increase the
economic burden on any operator or increase the scope of this final
rule.
Related Service Information Under 1 CFR Part 51
We reviewed Zodiac Aerospace SB MC10-35-274, Revision 02, dated
June 25, 2014. The SB describes procedures for inspecting and
replacing, if necessary, oxygen mask regulator inflatable harnesses.
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.
Costs of Compliance
We estimate that this AD affects an unknown number of oxygen mask
regulators installed on, but not limited to, various aircraft of U.S.
registry.
We estimate the following costs to comply with this AD:
Estimated Costs
----------------------------------------------------------------------------------------------------------------
Cost per
Action Labor cost Parts cost product
----------------------------------------------------------------------------------------------------------------
Date of manufacturing code review............. 0.1 work-hours x $85 per hour = $0 $8.50
$8.50.
Hose replacement.............................. 0.3 work-hours x $85 per hour = 1,465.00 1,490.50
$25.50.
----------------------------------------------------------------------------------------------------------------
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.
This AD is issued in accordance with authority delegated by the
Executive Director, Aircraft Certification Service, as authorized by
FAA Order 8000.51C. In accordance with that order, issuance of ADs is
normally a function of the Compliance and Airworthiness
[[Page 4990]]
Division, but during this transition period, the Executive Director has
delegated the authority to issue ADs applicable to engines, propellers,
and associated appliances to the Manager, Engine and Propeller
Standards Branch, Policy and Innovation Division.
Regulatory Findings
This AD will not have federalism implications under Executive Order
13132. This AD will not have a substantial direct effect on the States,
on the relationship between the national government and the States, or
on the distribution of power and responsibilities among the various
levels of government.
For the reasons discussed above, I certify 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 adding the following new airworthiness
directive (AD):
2018-21-14 Zodiac Aerotechnics (formerly Intertechnique): Amendment
39-19472; Docket No. FAA-2017-0505; Product Identifier 2017-NE-15-
AD.
(a) Effective Date
This AD is effective March 27, 2019.
(b) Affected ADs
None.
(c) Applicability
This AD applies to Zodiac Aerotechnics (Zodiac) MC10 series crew
oxygen mask regulators fitted with an inflatable harness assembly,
part number (P/N) MXH20-1 or MXH21-1.
(d) Subject
Joint Aircraft System Component (JASC) Code 3510, Crew Oxygen
System.
(e) Unsafe Condition
This AD was prompted by reports that certain silicon harness
inflation hoses installed on certain flight crew quick donning mask
harnesses (also known as `comfort' harness) have shown an unusually
high premature rupture rate. We are issuing this AD to prevent a
harness rupture during a sudden depressurization event. The unsafe
condition, if not addressed, could result in hypoxia and subsequent
unconsciousness of the affected flight crew member, and consequent
reduced control of the aircraft.
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
(g) Required Actions
(1) Within 36 months after the effective date of this AD,
determine the date of manufacturing (DMF) code of each inflatable
harness assembly, P/N MXH20-1 and P/N MXH21-1, fitted to a flight
crew oxygen mask regulator, having a P/N listed in Planning
Information, paragraph 1.A.(1), of Zodiac Aerospace Service Bulletin
(SB) MC10-35-274, Revision 02, dated June 25, 2014. A review of
airplane delivery or maintenance records is acceptable to make the
determination as specified in this paragraph, provided those records
can be relied upon for that purpose, and the DMF of the inflatable
harness assembly, P/N MXH20-1 or P/N MXH21-1, as applicable, can be
conclusively identified from that review.
(2) If during the review required by paragraph (g)(1) of this
AD, the DMF code of the inflatable harness assembly, P/N MXH20-1 or
P/N MXH21-1, is found to be between 0850-S and 1051-S (inclusive):
Within 36 months after the effective date of this AD, replace the
harness inflation hose, P/N 445186 or P/N 445952, as applicable,
with a part eligible for installation, or remove the inflatable
harness assembly from the mask regulator and replace it with an
inflatable harness assembly eligible for installation.
(3) An oxygen mask regulator equipped with an inflatable harness
assembly, P/N MXH20-1 or P/N MXH21-1, having a DMF code of November
2008 (0845-S or 08/45-S) or earlier, and those with a DMF code of
January 2011 (1101-S or 11/01-S) or later, are excluded from the
requirements of this AD, provided it can be demonstrated that
neither the inflatable harness assembly, nor the harness inflation
hose, P/N 445186 or P/N 445952, as applicable, was replaced on that
mask. An oxygen mask regulator with an inflatable harness assembly,
P/N MXH20-1 or P/N MXH21-1, and with an inflatatable harness
assembly with a metal bushing that has been marked with an ``I'' is
also excluded from the requirements of this AD. A review of airplane
delivery or maintenance records is acceptable to make the
determination, provided those records can be relied upon for that
purpose.
(h) Installation Prohibition
After the effective date of this AD, do not install on any
airplane a flight crew oxygen mask regulator with a P/N listed in
Planning Information, paragraph 1.A.(1), of Zodiac SB MC10-35-274,
Revision 02, dated June 25, 2014, unless it meets the definition of
a part eligible for installation in paragraph (i) of this AD.
(i) Definition
(1) After the effective date of this AD, a part eligible for
installation is a crew oxygen mask regulator with:
(i) A P/N identified in Planning Information, paragraph 1.A.(1),
of Zodiac Aerospace SB MC10-35-274, Revision 02, dated June 25,
2014, provided it has been determined that a P/N MXH20-1 or P/N
MXH21-1 inflatable harness installed on that crew oxygen mask
regulator has been inspected, and re-marked with an ``I'' as
required by Material Information, paragraph 2.E. of Zodiac Aerospace
SB MC10-35-274, Revision 02, dated June 25, 2014; or
(ii) a P/N identified in Planning Information, paragraph
1.A.(1), of Zodiac Aerospace SB MC10-35-274, Revision 02, dated June
25, 2014, provided it has been determined that an inflatable
harness, P/N MXH21-31, is installed.
(2) [Reserved]
(j) Credit for Previous Actions
You may take credit for the inspection and replacement of the
oxygen mask regulator harness inflation hose required by paragraphs
(g)(1) and (2) of this AD, if you performed the inspection and
replacement using the Accomplishment Instructions, paragraph 3, of
Zodiac Aerospace SB MC10-35-274, Initial Issue, dated March 19,
2014, or Revision 01, dated April 18, 2014.
(k) Alternative Methods of Compliance (AMOCs)
(1) The Manager, FAA, Boston ACO Branch, Compliance and
Airworthiness Division, has the authority to approve AMOCs for this
AD, if requested using the procedures found in 14 CFR 39.19. In
accordance with 14 CFR 39.19, send your request to your principal
inspector or local Flight Standards District Office, as appropriate.
If sending information directly to the manager of the ACO Branch,
send it to the attention of the person identified in paragraph
(l)(1) of this AD. You may email your request to: ANE-AD-AMOC@faa.gov.
(2) Before using any approved AMOC, notify your appropriate
principal inspector, or lacking a principal inspector, the manager
of the local flight standards district office/certificate holding
district office.
(l) Related Information
(1) For more information about this AD, contact Erin King,
Aerospace Engineer, Boston ACO Branch, FAA, 1200 District Avenue,
Burlington, MA 01803; phone 781-238-7655; fax: 781-238-7199; email:
erin.king@faa.gov.
[[Page 4991]]
(2) Refer to European Union Aviation Safety Agency AD 2014-0142,
Revision 01, dated June 11, 2014, for more information. You may
examine the EASA AD in the AD docket on the internet at https://www.regulations.gov by searching for and locating Docket No. FAA-
2017-0505.
(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 the AD specifies otherwise.
(i) Zodiac Aerospace Service Bulletin MC10-35-274, Revision 02,
dated June 25, 2014.
(ii) [Reserved]
(3) For service information identified in this AD, contact
Zodiac Aerotechnics, 61 rue Pierre Curie BP 1, 78373 Plaisir, CEDEX,
France; phone: +33 1 6486 6964; email:
Christophe.besset@zodiacaerospace.com or
Yann.laine@zodiacaerospace.com.
(4) You may view this service information at FAA, Engine &
Propeller Standards Branch, 1200 District Avenue, Burlington, MA
01803. For information on the availability of this material at the
FAA, call 781-238-7759.
(5) 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 Burlington, Massachusetts, on February 13, 2019.
Robert J. Ganley,
Manager, Engine and Propeller Standards Branch, Aircraft Certification
Service.
[FR Doc. 2019-02748 Filed 2-19-19; 8:45 am]
BILLING CODE 4910-13-P