Published 2017-09-11 · Federal Register document 2017-18855
Airworthiness Directives; B/E Aerospace Protective Breathing Equipment Part Number 119003-11 and Part Number 119003-21
Publication summary
We are superseding Airworthiness Directive (AD) 2016-11-20 for certain B/E Aerospace protective breathing equipment (PBE) that is installed on airplanes. AD 2016-11-20 required replacing part number (P/N) 119003-11 PBE units. Since we issued AD 2016-11-20, we received a report that PBE units, P/N 119003-21, within a certain serial number range are made with candle tube material determined to have a low yield strength and may be volatile upon use or disposal. This AD retains the actions required in AD 2016-11-20 and requires inspecting and replacing P/N 119003-11 and 119003-21 PBE units. We are issuing this AD to address the unsafe condition on these products.
Why this record is shown
Source: Federal Register annual FAA metadata. Acquired 2026-09-03T22:23:54.997910+00:00. The title, summary and date are source facts.
- Source revision
- federal_register_ad_metadata_2017-90ba553c3b802c53
- Source row
- results[265]
- Raw source SHA-256
- 90ba553c3b802c5316e8d18f30db5da9f7731a87f58278ec2965f199ef4375e9
Final-rule publication
Recorded publication clauses
- AD identifier printed in this edition
- 2017-18-12
- Effective date printed in this edition
- 2017-10-16
Read 15 complete recorded clauses
Effective Date
(a) Effective Date
This AD is effective October 16, 2017.
Exact source excerpt. Text positions 16295–16359, end exclusive, in the original decoded publication. SHA-256: d4b87debf0f0bbbe47ff5f42435183e4256d249e5808df24907a1a693537fa13
Affected ADs
(b) Affected ADs
This AD replaces AD 2016-11-20, Amendment 39-18547 (81 FR 37492,
June 10, 2016), (``AD 2016-11-20'').
Exact source excerpt. Text positions 16359–16485, end exclusive, in the original decoded publication. SHA-256: 33a8d1fe120eed3d73111d20dc945e5bdc08802fd0dc58d1bfaa7f7ef8a53f61
Applicability wording · Applicability
(c) Applicability
This AD applies to B/E Aerospace Protective Breathing Equipment
(PBE), part numbers (P/N) 119003-11 and 119003-21, that are
installed on airplanes.
Exact source excerpt. Text positions 16485–16659, end exclusive, in the original decoded publication. SHA-256: 71953d60eeedbd73099bdcffafd027c312e7d5175ac33a8821d2b0ddc59a9019
Subject
(d) Subject
Joint Aircraft System Component (JASC)/Air Transport Association
(ATA) of America Code 35; Oxygen.
Exact source excerpt. Text positions 16659–16777, end exclusive, in the original decoded publication. SHA-256: aa74c4ebc2833c24df4e42aca64d5edbae37fdbfcc71bda7c258d6a411c62ffa
Unsafe Condition
(e) Unsafe Condition
AD 2016-11-20 was prompted by a report of a PBE unit, P/N
119003-11, catching fire upon activation by a crewmember. This AD
was prompted by a report that PBE units, P/N 119003-21, within a
certain serial number range are made with candle tube material
determined to have a low yield strength and may be volatile upon use
or disposal. We are issuing this AD to correct the unsafe condition
on these products.
Exact source excerpt. Text positions 16777–17218, end exclusive, in the original decoded publication. SHA-256: bdea85ef1412764c970f2a97e368ee3b14019838206a27d56ab798c0980ba8e7
Compliance
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
Exact source excerpt. Text positions 17218–17320, end exclusive, in the original decoded publication. SHA-256: 00fbfa31932483f627d0ce0a11cbd2e35e15d9231842b91ac85623ce533912d3
Inspection Retained From AD 2016-11-20 for Airplanes With PBE, P/N 119003-11, Installed
(g) Inspection Retained From AD 2016-11-20 for Airplanes With PBE, P/N
119003-11, Installed
Within 3 months after July 15, 2016 (the effective date of AD
2016-11-20), while still in the stowage box, physically inspect the
PBE pouch to determine if it has an intact vacuum seal. Do this
inspection following paragraph III.A.(1) of the Accomplishment
Instructions in B/E Aerospace Service Bulletin (SB) No. 119003-35-
011, Rev. 000, dated February 4, 2015.
Exact source excerpt. Text positions 17320–17786, end exclusive, in the original decoded publication. SHA-256: 12b4e0e3bf5d410d1d11c4d5d09fdd7343ce822596bb8aeded6b2be16cde0013
Replacement Retained From AD 2016-11-20 for Airplanes With PBE, P/N 119003-11, Installed
(h) Replacement Retained From AD 2016-11-20 for Airplanes With PBE, P/N
119003-11, Installed
(1) During the inspection required in paragraph (g) of this AD,
if a PBE pouch is found that does not have an intact vacuum seal,
before further flight, replace the PBE with a PBE unit, P/N 119003-
21 that is not within the serial number (S/N) range 004-14768M
through 004-21093M or 004-02393M through 004-03033M, following
paragraphs III.C., III.D.(4), III.D.(6), and III.D.(7) of the
Accomplishment Instructions in B/E Aerospace SB No. 119003-35-009,
Rev. 001, dated April 12, 2016, or replace it with another FAA-
approved PBE installation.
(2) During the inspection required in paragraph (g) of this AD,
if a PBE pouch is found where the vacuum seal is intact, within 18
months after July 15, 2016 (the effective date of AD 2016-11-20),
remove PBE, P/N 119003-11, and replace it with a PBE, P/N 119003-21
that is not within the S/N range 004-14768M through 004-21093M or
004-02393M through 004-03033M, following paragraphs III.C.,
III.D.(4), III.D.(6), and III.D.(7) of the Accomplishment
Instructions in B/E Aerospace SB No. 119003-35-009, Rev. 001, dated
April 12, 2016, or replace it with another FAA-approved PBE
installation.
(3) Once a discrepant PBE has been identified during an
inspection or review of records, the unit must be removed before
further flight. However, continued operation with fewer than
required PBE is permissible if allowed by your MEL.
Exact source excerpt. Text positions 17786–19281, end exclusive, in the original decoded publication. SHA-256: 7cdf82063c63119ff59b4b5d955598a6932f14b0a14e2a4ce47d90a0ebbb4e6c
New Inspection for Airplanes With PBE, P/N 119003-21, Installed
(i) New Inspection for Airplanes With PBE, P/N 119003-21, Installed
Within 6 months after October 16, 2017 (the effective date of
this AD), inspect to determine if the S/N of the installed PBE, P/N
119003-21, is within the range of 004-14768M through 004-21093M or
004-02393M through 004-03033M. Do the inspection following paragraph
III.A of the Accomplishment Instructions in B/E Aerospace SB No.
119003-35-013, Rev. 002, dated July 19, 2017.
(1) Instead of the inspection, you may do a maintenance records
review, to determine the S/N of the installed PBE, P/N 119003-21.
(2) If you choose to do the maintenance records review and you
can positively determine that the S/N of the installed PBE, P/N
119003-21, is within the range of 004-14768M through 004-21093M or
004-02393M through 004-03033M, continue to the replacement
requirement in paragraph (j) of this AD.
(3) If you choose to do the maintenance records review and you
cannot positively determine that the S/N of the installed PBE, P/N
119003-21, is within the range of 004-14768M through 004-21093M or
004-02393M through 004-03033M, then you must either go back and do
the inspection specified in paragraph (i) of this AD to determine if
the replacement in paragraph (j) of this AD is necessary or do the
replacement in paragraph (j) of this AD.
Exact source excerpt. Text positions 19281–20625, end exclusive, in the original decoded publication. SHA-256: 4acdb800e0c7e1b67943884bfe7127be2a0ee8cd604c7e13fe253b2006646e90
New Replacement for Airplanes With PBE, P/N 119003-21, Installed
(j) New Replacement for Airplanes With PBE, P/N 119003-21, Installed
During the inspection or the maintenance records review required
in paragraph (i) of
[[Page 42592]]
this AD, if it is found that the PBE, P/N 119003-21, is within the
S/N range specified in paragraph (i) of this AD, before further
flight, remove the PBE and replace it with a PBE, P/N 119003-21,
that does not have a S/N 004-14768M through 004-21093M or 004-02393M
through 004-03033M. Do this replacement following paragraphs III.C.,
III.D.(4), III.D.(6), and III.D.(7) of the Accomplishment
Instructions in B/E Aerospace SB No. 119003-35-013, Rev. 002, dated
July 19, 2017, or replace it with another FAA-approved PBE
installation. Once a discrepant PBE has been identified during an
inspection or review of records, the unit must be removed before
further flight. However, continued operation with fewer than
required PBE is permissible if allowed by your MEL.
Exact source excerpt. Text positions 20625–21577, end exclusive, in the original decoded publication. SHA-256: bcb21dc8ffa98ace8142c4acb15739794dee22b5f95d0a57b24dac9e16a270cb
Prohibited Installation
(k) Prohibited Installation
As of October 16, 2017 (the effective date of this AD), do not
install a PBE, P/N 119003-21, that has a S/N within the range of
004-14768M through 004-21093M or 004-02393M through 004-03033M.
Exact source excerpt. Text positions 21577–21805, end exclusive, in the original decoded publication. SHA-256: 9215b5db353fb69cb5140d800ec2a108e26b0488e18915106f5991a98a61dd76
Credit for Actions Done Following Previous Service Information
(l) Credit for Actions Done Following Previous Service Information
If you performed the inspection and replacement action required
in paragraphs (i) and (j) of this AD before October 16, 2017 (the
effective date of this AD) using B/E Aerospace SB No. 119003-35-013,
Rev. 000, dated January 9, 2017, or B/E Aerospace SB No. 119003-35-
013, Rev. 001, dated February 24, 2017, you have met the
requirements of those paragraphs of this AD.
Exact source excerpt. Text positions 21805–22251, end exclusive, in the original decoded publication. SHA-256: c8fc807a5af287715bacbe485fdd5006c209b9bb55fead065afeaedf9af8cd75
Alternative Methods of Compliance (AMOCs)
(m) Alternative Methods of Compliance (AMOCs)
(1) The Manager, Wichita ACO Branch, FAA, has the authority to
approve AMOCs for this AD, if requested using the procedures found
in 14 CFR 39.19. In accordance with 14 CFR 39.19, send your request
to your principal inspector or local Flight Standards District
Office, as appropriate. If sending information directly to the
manager of the ACO, send it to the attention of the person
identified in paragraph (n)(1) of this AD.
(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.
Exact source excerpt. Text positions 22251–22952, end exclusive, in the original decoded publication. SHA-256: 1375152911ae072c5f454f57882ae4a1ee9e013983cbcc3a0f539092439f803e
Related Information
(n) Related Information
For more information about this AD, contact David Enns,
Aerospace Engineer, Wichita ACO Branch, FAA, 1801 S. Airport Road,
Room 100, Wichita, Kansas 67209; phone: (316) 946-4147; fax: (316)
946-4107; email: [email protected].
Exact source excerpt. Text positions 22952–23211, end exclusive, in the original decoded publication. SHA-256: a665d7a14739071cf3b1bc179ab74d8702bc850b92b2ab2e85dd8f03274a3696
Material Incorporated by Reference
(o) Material Incorporated by Reference
(1) The Director of the Federal Register approved the
incorporation by reference (IBR) of the service information listed
in this paragraph under 5 U.S.C. 552(a) and 1 CFR part 51.
(2) You must use this service information as applicable to do
the actions required by this AD, unless this AD specifies otherwise.
(3) The following service information was approved for IBR on
October 16, 2017.
(i) B/E Aerospace Service Bulletin No. 119003-35-013, Rev. 002,
dated July 19, 2017.
(ii) Reserved
(4) The following service information was approved for IBR on
July 15, 2016 (81 FR 37492, June 10, 2016).
(i) B/E Aerospace Service Bulletin No. 119003-35-009, Rev. 001,
dated April 12, 2016.
(ii) B/E Aerospace Service Bulletin No. 119003-35-011, Rev. 000,
dated February 4, 2015.
(5) For service information identified in this AD, contact B/E
Aerospace, Inc. service information identified in this AD, contact
B/E Aerospace, Inc., 10800 Pflumm Road, Commercial Aircraft Products
Group, Lenexa, Kansas 66215; phone: (913) 338-9800; fax: (913) 338-
8419; Internet: www.beaerospace.com.
(6) You may view this service information at FAA, Policy and
Innovation Division, 901 Locust, Kansas City, Missouri 64106. For
information on the availability of this material at the FAA, call
(816) 329-4148. It is also available on the internet at http://www.regulations.gov by searching for and locating Docket No. FAA-
2017-0439.
(7) You may view this service information that is incorporated
by reference at the National Archives and Records Administration
(NARA). For information on the availability of this material at
NARA, call 202-741-6030, or go to: http://www.archives.gov/federal-register/cfr/ibr-locations.html.
Exact source excerpt. Text positions 23211–25013, end exclusive, in the original decoded publication. SHA-256: 263920536e66fc4ffdcd42579f89e36885a3e6b19123b26c8fb592755e742493
No replacement link has been established from this edition. The complete historical rule chain and current legal effect remain unknown.
Find all recorded historical references to AD 2017-18-12 · 0 printed reference observations in this pinned collection.
These are observations from one dated publication. Current legal status is unknown; aircraft applicability, installed configuration, compliance and burden require separate evidence. Missing or unparsed conditions remain unknown.
Why these observations are shown
They were extracted offline from the same immutable official HTML source as the complete recorded text. The dated source wording, original text coordinates and exact quote digests are retained. PDF/text agreement and current regulatory effect have not been qualified.
Observation revision: whole-ad-publication-clause-observations-1.0.1. Text SHA-256: f7e0e5edea28df6960ab754f9e1b06a9303c0fc16ff7c409e923961788b4c78e. Source manifest: 5f7962406788f553f5094e43db67934a505d2689cf3fa5a02896a7312cb17b5a.
Official source · 2017-09-11
Publication text
This is the complete recorded text of this dated publication.
Current legal effect is unknown. Aircraft applicability, installed configuration and compliance require separate evidence. PDF/text agreement has not been evaluated.
Read the complete official publication text
[Federal Register Volume 82, Number 174 (Monday, September 11, 2017)]
[Rules and Regulations]
[Pages 42589-42592]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2017-18855]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2017-0439; Product Identifier 2017-CE-010-AD; Amendment
39-19021; AD 2017-18-12]
RIN 2120-AA64
Airworthiness Directives; B/E Aerospace Protective Breathing
Equipment Part Number 119003-11 and Part Number 119003-21
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Final rule.
-----------------------------------------------------------------------
SUMMARY: We are superseding Airworthiness Directive (AD) 2016-11-20 for
certain B/E Aerospace protective breathing equipment (PBE) that is
installed on airplanes. AD 2016-11-20 required replacing part number
(P/N) 119003-11 PBE units. Since we issued AD 2016-11-20, we received a
report that PBE units, P/N 119003-21, within a certain serial number
range are made with candle tube material determined to have a low yield
strength and may be volatile upon use or disposal. This AD retains the
actions required in AD 2016-11-20 and requires inspecting and replacing
P/N 119003-11 and 119003-21 PBE units. We are issuing this AD to
address the unsafe condition on these products.
DATES: This AD is effective October 16, 2017.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in this AD as of October 16,
2017.
The Director of the Federal Register approved the incorporation by
reference of certain other publication listed in this AD as of July 15,
2016 (81 FR 37492, June 10, 2016).
ADDRESSES: For service information identified in this final rule,
contact B/E Aerospace, Inc., Commercial Aircraft Products Group, 10800
Pflumm Road, Lenexa, Kansas 66215; phone: (913) 338-9800; fax: (913)
338-8419; Internet: www.beaerospace.com. You may view this service
information at the FAA, Policy and Innovation Division, 901 Locust,
Kansas City, Missouri 64106. For information on the availability of
this material at the FAA, call (816) 329-4148. It is also available on
the internet at http://www.regulations.gov by searching for and
locating Docket No. FAA-2017-0439.
Examining the AD Docket
You may examine the AD docket on the Internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2017-
0439; or in person at the Docket Management Facility between 9 a.m. and
5 p.m., Monday through Friday, except Federal holidays. The AD docket
contains this final rule, the regulatory evaluation, any comments
received, and other information. The address for the Docket Office
(phone: 800-647-5527) is Document Management Facility, U.S. Department
of Transportation, Docket Operations, M-30, West Building Ground Floor,
Room W12-140, 1200 New Jersey Avenue SE., Washington, DC 20590.
FOR FURTHER INFORMATION CONTACT: David Enns, Aerospace Engineer,
Wichita ACO Branch, FAA, 1801 S. Airport Road, Room 100, Wichita,
Kansas 67209; phone: (316) 946-4147; fax: (316) 946-4107; email:
[email protected].
SUPPLEMENTARY INFORMATION:
Discussion
We issued a notice of proposed rulemaking (NPRM) to amend 14 CFR
part 39 to supersede AD 2016-11-20, Amendment 39-18547 (81 FR 37492,
June 10, 2016), (``AD 2016-11-20''), for B/E Aerospace protective
breathing equipment (PBE), part number (P/N) 119003-11, that is
installed on airplanes. The NPRM published in the Federal Register on
May 26, 2017 (82 FR 24260). The NPRM was prompted by a report that PBE
units, P/N 119003-21, within a certain serial number range are made
with candle tube material determined to have a low yield strength and
may be volatile upon use or disposal. The NPRM proposed to retain the
actions required in AD 2016-11-20 and would require inspecting and
replacing P/N 119003-11 and 119003-21 PBE units. We are issuing this AD
to correct the unsafe condition on these products.
Comments
We gave the public the opportunity to participate in developing
this AD. The following presents the comments received on the NPRM and
the FAA's response to each comment.
Request To Include Additional Compliance Method for Paragraph (i) of
This AD
David White, of NetJets Aviation, requested that the action
required in paragraph (i) of this AD for determining the serial number
of the installed PBE, P/N 119003-21, also include a maintenance records
review.
The commenter stated that if the maintenance records are available
and the determination can positively be made, this review will save the
owners/operators time and money.
We agree with the commenter and have changed this AD based on this
comment.
Request for Clarification of Compliance Time for Paragraph (j) of This
AD
David White, of NetJets Aviation, requested that the compliance
time in paragraph (j) of this AD to be clarified.
The commenter stated that paragraph (j) of this AD requires
replacement of an affected mask before further flight or following
existing minimum equipment list (MEL) procedures, but it does not
identify if compliance is required at the earlier or the later of the
two thresholds.
We do not agree with commenter. The MEL is a document and method
airplane operators use to obtain relief from Federal Aviation
Regulations that requires all equipment installed on the airplane be
operative at the time of flight. It is airplane-specific and spells out
which pieces of equipment may be inoperable along with any procedures
that are required for an airplane to operate under specific conditions
while maintaining airworthiness. The reference to MEL is a reminder
that, depending on the airplane and its MEL, it may be acceptable to
remove the affected units and continue to operate with a reduced number
of PBEs as stated in the specific MEL. The affected units must be
removed upon discovery.
We have changed this AD based on this comment to make this more
clear.
Request To Change the Compliance Time in Paragraph (j) of This AD
David White, of NetJets Aviation, requested we change the
replacement compliance time in paragraph (j) of this AD to match the
compliance time in paragraph (i) of this AD, which would allow six
months to replace the affected PBE after it is identified by inspection
or maintenance records review.
The commenter stated that if the request to allow a records review
for paragraph (i) of this AD is accepted, then the maintenance records
review could be accomplished without access to the airplane and could
result in
[[Page 42590]]
unnecessarily grounding the airplane if a discrepant mask is found
during the records review. However, if the compliance time for
replacing the affected PBE matches the compliance time for the
inspection/maintenance records review, the operators will have
flexibility for compliance with paragraph (j).
We do not agree with the commenter. Once an airplane has been
identified to have an affected PBE installed, it must be removed and
replaced before further flight. Once a discrepant PBE has been
identified during an inspection or review of records, the unit must be
removed before further flight. However, continued operation with fewer
than required PBE is permissible if allowed by your MEL.
We have not changed this AD based on this comment.
Request To Include Revised Service Bulletin
B/E Aerospace, Inc. requested that Service Bulletin (SB) 119003-35-
013, Rev. 002, dated July 19, 2017, be incorporated into this AD.
The commenter stated that the only change in the B/E Aerospace SB
119003-35-013, Rev. 002, dated July 19, 2017, is the addition of
warranty credit. All other information and instructions are the same as
those contained in B/E Aerospace SB 119003-35-013, Rev. 001, dated
February 24, 2017.
We agree with the commenter and have changed this AD based on this
comment.
Conclusion
We reviewed the relevant data, considered the comments received,
and determined that air safety and the public interest require adopting
this AD with the change described previously. We have determined that
these minor changes:
<bullet> Are consistent with the intent that was proposed in the
NPRM for correcting the unsafe condition; and
<bullet> 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 AD.
Related Service Information Under 1 CFR Part 51
We reviewed B/E Aerospace SB No. 119003-35-011, Rev. 000, dated
February 4, 2015; SB 119003-35-009, Rev. 001, dated April 12, 2016; and
SB No. 119003-35-013, Rev. 002, dated July 19, 2017. B/E Aerospace SB
No. 119003-35-011, Rev. 000, dated February 4, 2015, describes
procedures for inspecting PBE, P/N 119003-11, to determine if the
vacuum seal of the pouch containing the PBE is compromised; B/E
Aerospace SB No. 119003-35-009, Rev. 001, dated April 12, 2016,
describes procedures for replacing PBE, P/N 119003-11 with P/N 119003-
21; and B/E Aerospace SB No. 119003-35-013, Rev. 002, dated July 19,
2017, describes procedures for inspecting PBE P/N 119003-21 to
determine the serial number and replacing any within the specified
serial number range. 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.
Differences Between This AD and the Service Information
We are not requiring the disposal of the PBE as specified in the
related service information because we have determined that owner/
operators use various methods for disposal, which includes returning
the PBE to the manufacturer. Therefore, we have not required the use of
only one method of disposal. However, given the potential concern with
activation of certain PBE units during disposal, we encourage
coordination with the manufacturer and awareness of the disposal
methods.
Costs of Compliance
We estimate that this AD affects 9,000 products installed on
airplanes of U.S. registry.
We estimate the following costs to comply with this AD:
Estimated Costs
----------------------------------------------------------------------------------------------------------------
Cost per Cost on U.S.
Action Labor cost Parts cost product operators
----------------------------------------------------------------------------------------------------------------
Inspecting the pouch containing .5 work-hour x $85 Not applicable............. $42.50 $382,500
the PBE for proper vacuum seal. per hour = $42.50.
Replace PBE P/N 119003-11 with .5 work-hour x $85 1,510...................... 1,552.50 13,972,500
PBE P/N 119003-21. per hour = $42.50.
Inspecting the PBE to determine .5 work-hour x $85 Not applicable............. 42.50 382,500
whether an affected PBE P/N per hour = $42.50.
119003-21 is installed.
Maintenance records review to .5 work-hour x $85 Not applicable............. 42.50 382,500
determine whether an affected per hour = $42.50.
PBE P/N 119003-21 is installed.
----------------------------------------------------------------------------------------------------------------
We estimate the following costs to replace any affected PBE P/N
119003-21 units that fall within the affected serial number range. We
have no way of determining the number of aircraft that might need these
repairs/replacements:
On-Condition Costs
----------------------------------------------------------------------------------------------------------------
Cost per
Action Labor cost Parts cost product
----------------------------------------------------------------------------------------------------------------
Replacement of PBE P/N 119003-21........... .5 work-hour x $85 per hour = $1,510 $1,552.50
$42.50.
----------------------------------------------------------------------------------------------------------------
The cost difference between AD 2016-11-20 and this AD is the cost
of inspecting for serial number determination and replacing the
affected serial numbers. This part of the AD could potentially affect
2,070 PBE units.
According to the manufacturer, some of the costs of this AD may be
covered under warranty, thereby reducing the cost impact on affected
individuals. We do not control warranty coverage for affected
individuals. As a result, we have included all costs in our cost
estimate.
[[Page 42591]]
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 Division, but
during this transition period, the Executive Director has delegated the
authority to issue ADs applicable to small airplanes and domestic
business jet transport airplanes to the Director of the Policy and
Innovation Division.
Regulatory Findings
We have 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 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)
2016-11-20, Amendment 39-18547 (81 FR 37492, June 10, 2016), and adding
the following new AD:
2017-18-12 B/E Aerospace: Amendment 39-19021; Docket No. FAA-2017-
0439; Product Identifier 2017-CE-010-AD.
(a) Effective Date
This AD is effective October 16, 2017.
(b) Affected ADs
This AD replaces AD 2016-11-20, Amendment 39-18547 (81 FR 37492,
June 10, 2016), (``AD 2016-11-20'').
(c) Applicability
This AD applies to B/E Aerospace Protective Breathing Equipment
(PBE), part numbers (P/N) 119003-11 and 119003-21, that are
installed on airplanes.
(d) Subject
Joint Aircraft System Component (JASC)/Air Transport Association
(ATA) of America Code 35; Oxygen.
(e) Unsafe Condition
AD 2016-11-20 was prompted by a report of a PBE unit, P/N
119003-11, catching fire upon activation by a crewmember. This AD
was prompted by a report that PBE units, P/N 119003-21, within a
certain serial number range are made with candle tube material
determined to have a low yield strength and may be volatile upon use
or disposal. We are issuing this AD to correct the unsafe condition
on these products.
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
(g) Inspection Retained From AD 2016-11-20 for Airplanes With PBE, P/N
119003-11, Installed
Within 3 months after July 15, 2016 (the effective date of AD
2016-11-20), while still in the stowage box, physically inspect the
PBE pouch to determine if it has an intact vacuum seal. Do this
inspection following paragraph III.A.(1) of the Accomplishment
Instructions in B/E Aerospace Service Bulletin (SB) No. 119003-35-
011, Rev. 000, dated February 4, 2015.
(h) Replacement Retained From AD 2016-11-20 for Airplanes With PBE, P/N
119003-11, Installed
(1) During the inspection required in paragraph (g) of this AD,
if a PBE pouch is found that does not have an intact vacuum seal,
before further flight, replace the PBE with a PBE unit, P/N 119003-
21 that is not within the serial number (S/N) range 004-14768M
through 004-21093M or 004-02393M through 004-03033M, following
paragraphs III.C., III.D.(4), III.D.(6), and III.D.(7) of the
Accomplishment Instructions in B/E Aerospace SB No. 119003-35-009,
Rev. 001, dated April 12, 2016, or replace it with another FAA-
approved PBE installation.
(2) During the inspection required in paragraph (g) of this AD,
if a PBE pouch is found where the vacuum seal is intact, within 18
months after July 15, 2016 (the effective date of AD 2016-11-20),
remove PBE, P/N 119003-11, and replace it with a PBE, P/N 119003-21
that is not within the S/N range 004-14768M through 004-21093M or
004-02393M through 004-03033M, following paragraphs III.C.,
III.D.(4), III.D.(6), and III.D.(7) of the Accomplishment
Instructions in B/E Aerospace SB No. 119003-35-009, Rev. 001, dated
April 12, 2016, or replace it with another FAA-approved PBE
installation.
(3) Once a discrepant PBE has been identified during an
inspection or review of records, the unit must be removed before
further flight. However, continued operation with fewer than
required PBE is permissible if allowed by your MEL.
(i) New Inspection for Airplanes With PBE, P/N 119003-21, Installed
Within 6 months after October 16, 2017 (the effective date of
this AD), inspect to determine if the S/N of the installed PBE, P/N
119003-21, is within the range of 004-14768M through 004-21093M or
004-02393M through 004-03033M. Do the inspection following paragraph
III.A of the Accomplishment Instructions in B/E Aerospace SB No.
119003-35-013, Rev. 002, dated July 19, 2017.
(1) Instead of the inspection, you may do a maintenance records
review, to determine the S/N of the installed PBE, P/N 119003-21.
(2) If you choose to do the maintenance records review and you
can positively determine that the S/N of the installed PBE, P/N
119003-21, is within the range of 004-14768M through 004-21093M or
004-02393M through 004-03033M, continue to the replacement
requirement in paragraph (j) of this AD.
(3) If you choose to do the maintenance records review and you
cannot positively determine that the S/N of the installed PBE, P/N
119003-21, is within the range of 004-14768M through 004-21093M or
004-02393M through 004-03033M, then you must either go back and do
the inspection specified in paragraph (i) of this AD to determine if
the replacement in paragraph (j) of this AD is necessary or do the
replacement in paragraph (j) of this AD.
(j) New Replacement for Airplanes With PBE, P/N 119003-21, Installed
During the inspection or the maintenance records review required
in paragraph (i) of
[[Page 42592]]
this AD, if it is found that the PBE, P/N 119003-21, is within the
S/N range specified in paragraph (i) of this AD, before further
flight, remove the PBE and replace it with a PBE, P/N 119003-21,
that does not have a S/N 004-14768M through 004-21093M or 004-02393M
through 004-03033M. Do this replacement following paragraphs III.C.,
III.D.(4), III.D.(6), and III.D.(7) of the Accomplishment
Instructions in B/E Aerospace SB No. 119003-35-013, Rev. 002, dated
July 19, 2017, or replace it with another FAA-approved PBE
installation. Once a discrepant PBE has been identified during an
inspection or review of records, the unit must be removed before
further flight. However, continued operation with fewer than
required PBE is permissible if allowed by your MEL.
(k) Prohibited Installation
As of October 16, 2017 (the effective date of this AD), do not
install a PBE, P/N 119003-21, that has a S/N within the range of
004-14768M through 004-21093M or 004-02393M through 004-03033M.
(l) Credit for Actions Done Following Previous Service Information
If you performed the inspection and replacement action required
in paragraphs (i) and (j) of this AD before October 16, 2017 (the
effective date of this AD) using B/E Aerospace SB No. 119003-35-013,
Rev. 000, dated January 9, 2017, or B/E Aerospace SB No. 119003-35-
013, Rev. 001, dated February 24, 2017, you have met the
requirements of those paragraphs of this AD.
(m) Alternative Methods of Compliance (AMOCs)
(1) The Manager, Wichita ACO Branch, FAA, has the authority to
approve AMOCs for this AD, if requested using the procedures found
in 14 CFR 39.19. In accordance with 14 CFR 39.19, send your request
to your principal inspector or local Flight Standards District
Office, as appropriate. If sending information directly to the
manager of the ACO, send it to the attention of the person
identified in paragraph (n)(1) of this AD.
(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.
(n) Related Information
For more information about this AD, contact David Enns,
Aerospace Engineer, Wichita ACO Branch, FAA, 1801 S. Airport Road,
Room 100, Wichita, Kansas 67209; phone: (316) 946-4147; fax: (316)
946-4107; email: [email protected].
(o) Material Incorporated by Reference
(1) The Director of the Federal Register approved the
incorporation by reference (IBR) of the service information listed
in this paragraph under 5 U.S.C. 552(a) and 1 CFR part 51.
(2) You must use this service information as applicable to do
the actions required by this AD, unless this AD specifies otherwise.
(3) The following service information was approved for IBR on
October 16, 2017.
(i) B/E Aerospace Service Bulletin No. 119003-35-013, Rev. 002,
dated July 19, 2017.
(ii) Reserved
(4) The following service information was approved for IBR on
July 15, 2016 (81 FR 37492, June 10, 2016).
(i) B/E Aerospace Service Bulletin No. 119003-35-009, Rev. 001,
dated April 12, 2016.
(ii) B/E Aerospace Service Bulletin No. 119003-35-011, Rev. 000,
dated February 4, 2015.
(5) For service information identified in this AD, contact B/E
Aerospace, Inc. service information identified in this AD, contact
B/E Aerospace, Inc., 10800 Pflumm Road, Commercial Aircraft Products
Group, Lenexa, Kansas 66215; phone: (913) 338-9800; fax: (913) 338-
8419; Internet: www.beaerospace.com.
(6) You may view this service information at FAA, Policy and
Innovation Division, 901 Locust, Kansas City, Missouri 64106. For
information on the availability of this material at the FAA, call
(816) 329-4148. It is also available on the internet at http://www.regulations.gov by searching for and locating Docket No. FAA-
2017-0439.
(7) You may view this service information that is incorporated
by reference at the National Archives and Records Administration
(NARA). For information on the availability of this material at
NARA, call 202-741-6030, or go to: http://www.archives.gov/federal-register/cfr/ibr-locations.html.
Issued in Kansas City, Missouri, on August 30, 2017.
Melvin Johnson,
Deputy Director, Policy and Innovation Division, Aircraft Certification
Service.
[FR Doc. 2017-18855 Filed 9-8-17; 8:45 am]
BILLING CODE 4910-13-P
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