Published 2018-11-27 · Federal Register document 2018-25394
Airworthiness Directives; The Boeing Company Airplanes
Publication summary
We are adopting a new airworthiness directive (AD) for all The Boeing Company Model 747-8 and 747-8F series airplanes. This AD was prompted by a report that flightcrew oxygen masks did not function as designed during flight testing. This AD requires an inspection to determine if certain oxygen masks/regulators are installed, and replacement if necessary. 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 2026-09-03T22:23:58.123663+00:00. The title, summary and date are source facts.
- Source revision
- federal_register_ad_metadata_2018-258c65fa72d503e0
- Source row
- results[362]
- Raw source SHA-256
- 258c65fa72d503e0b0dfb928a28beb1793ddc7dd9218bce0413e53dfe11d78fb
Final-rule publication
Recorded publication clauses
- AD identifier printed in this edition
- 2018-23-13
- Effective date printed in this edition
- 2019-01-02
Read 12 complete recorded clauses
Effective Date
(a) Effective Date
This AD is effective January 2, 2019.
Exact source excerpt. Text positions 12339–12402, end exclusive, in the original decoded publication. SHA-256: 771f68383990615dcc9d8ee7b58af805b718e175e7d45be9b48223db09c5acda
Affected ADs
(b) Affected ADs
None.
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Applicability wording · Applicability
(c) Applicability
This AD applies to all The Boeing Company Model 747-8 and 747-8F
series airplanes, certificated in any category.
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Subject
(d) Subject
Air Transport Association (ATA) of America Code 35, Oxygen.
[[Page 60761]]
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Unsafe Condition
(e) Unsafe Condition
This AD was prompted by a report that flightcrew oxygen masks
did not function as designed during flight testing. We are issuing
this AD to address flightcrew oxygen masks/regulators that do not
deploy correctly, which could result in a delay for the flightcrew
to put on the masks, which may lead to hypoxia and loss of useful
consciousness, potentially resulting in loss of control of the
airplane.
Exact source excerpt. Text positions 12663–13097, end exclusive, in the original decoded publication. SHA-256: d1ad6f58dc33c32e1e25e463815c42e5062ebb55e712a44c9e69d35c0dcb4ea6
Compliance
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
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Required Actions
(g) Required Actions
For airplanes with an original certificate of airworthiness, or
an original export certificate of airworthiness, issued on or before
the effective date of this AD: Within 72 months after the effective
date of this AD, inspect for oxygen mask/regulator part number (P/N)
MLD20-626-1. A review of airplane maintenance records is acceptable
in lieu of the part number inspection if the part number of the
oxygen mask/regulator can be conclusively determined from that
review. If any oxygen mask/regulator P/N MLD20-626-1 is found,
within 72 months after the effective date of this AD, do the actions
identified in paragraph (g)(1), (g)(2), or (g)(3) of this AD.
(1) Do all applicable actions identified as ``RC'' (required for
compliance) in, and in accordance with, the Accomplishment
Instructions of Boeing Special Attention Service Bulletin 747-35-
2133, Revision 1, dated November 1, 2017, except as provided by
paragraph (h) of this AD.
(2) Except as specified in paragraph (i)(3) of this AD: Remove
oxygen mask/regulator P/N MLD20-626-1 and install any new or
serviceable oxygen mask/regulator that is not P/N MLD20-626-1 and
that is FAA approved for installation on the airplane.
Note 1 to paragraphs (g)(2) and (g)(3) of this AD: Guidance for
the installation procedures can be found in Boeing Model 747
Aircraft Maintenance Manual (AMM) 35-11-18.
(3) Except as specified in paragraph (i)(3) of this AD: Remove
the oxygen mask/regulator P/N MLD20-626-1 and the installed oxygen
mask stowage box combination, and install any new or serviceable
oxygen mask/regulator and stowage box combination that does not
include oxygen mask/regulator P/N MLD20-626-1, and that is FAA
approved for installation on the airplane.
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Exceptions to Service Information Specifications
(h) Exceptions to Service Information Specifications
Where Boeing Special Attention Service Bulletin 747-35-2133,
Revision 1, dated November 1, 2017, refers to or specifies
installing a new (or changed) part, for this AD, a new or
serviceable (or changed) part is acceptable.
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Parts Installation Limitations
(i) Parts Installation Limitations
(1) For airplanes with an original certificate of airworthiness,
or an original export certificate of airworthiness, issued on or
before the effective date of this AD: As of the effective date of
this AD, no person may install an oxygen mask/regulator P/N MLD20-
626-1 on any airplane, except that prior to 72 months after the
effective date of this AD, installation of P/N MLD20-626-1 is
acceptable for unscheduled maintenance as a replacement only for
another P/N MLD20-626-1, and only into a stowage box having P/N
MXP806-1. If an oxygen mask/regulator having a part number other
than P/N MLD20-626-1 is installed, it may not be replaced with P/N
MLD20-626-1. For the purposes of this AD, unscheduled maintenance is
defined as maintenance that was not planned for or scheduled in
advance, such as changing a defective or unserviceable oxygen mask
at dispatch.
(2) For airplanes with an original certificate of airworthiness
or an original export certificate of airworthiness issued after the
effective date of this AD: As of the effective date of this AD, no
person may install oxygen mask/regulator P/N MLD20-626-1 on any
airplane.
(3) For all airplanes: As of the effective date of this AD, no
person may install oxygen mask/regulator P/N MLD20-726-1 in
combination with any stowage box part number that is not P/N MXP806-
7 on any airplane.
Exact source excerpt. Text positions 15269–16683, end exclusive, in the original decoded publication. SHA-256: 53ea482408b2cf6e6f494f205f428a89ab2b414985ebc5bfdbdfb8c2010c9461
Alternative Methods of Compliance (AMOCs)
(j) Alternative Methods of Compliance (AMOCs)
(1) The Manager, Seattle 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 certification office, send it to the attention of the
person identified in paragraph (k)(1) of this AD. Information may be
emailed to: [email protected].
(2) Before using any approved AMOC, notify your appropriate
principal inspector, or lacking a principal inspector, the manager
of the local flight standards district office/certificate holding
district office.
(3) An AMOC that provides an acceptable level of safety may be
used for any repair, modification, or alteration required by this AD
if it is approved by the Boeing Commercial Airplanes Organization
Designation Authorization (ODA) that has been authorized by the
Manager, Seattle ACO Branch, FAA, to make those findings. To be
approved, the repair method, modification deviation, or alteration
deviation must meet the certification basis of the airplane, and the
approval must specifically refer to this AD.
(4) Except as required by paragraph (h) of this AD: For service
information that contains steps that are labeled as RC, the
provisions of paragraphs (j)(4)(i) and (j)(4)(ii) of this AD apply.
(i) The steps labeled as RC, including substeps under an RC step
and any figures identified in an RC step, must be done to comply
with the AD. If a step or substep is labeled ``RC Exempt,'' then the
RC requirement is removed from that step or substep. An AMOC is
required for any deviations to RC steps, including substeps and
identified figures.
(ii) Steps not labeled as RC may be deviated from using accepted
methods in accordance with the operator's maintenance or inspection
program without obtaining approval of an AMOC, provided the RC
steps, including substeps and identified figures, can still be done
as specified, and the airplane can be put back in an airworthy
condition.
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Related Information
(k) Related Information
(1) For more information about this AD, contact Susan L. Monroe,
Aerospace Engineer, Cabin Safety and Environmental Systems Section,
FAA, Seattle ACO Branch, 2200 South 216th St., Des Moines, WA 98198;
phone and fax: 206-231-3570; email: [email protected].
(2) Service information identified in this AD that is not
incorporated by reference is available at the addresses specified in
paragraphs (k)(3) and (k)(4) of this AD.
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Material Incorporated by Reference
(l) 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) Boeing Special Attention Service Bulletin 747-35-2133,
Revision 1, dated November 1, 2017.
(ii) [Reserved]
(3) For service information identified in this AD, contact
Boeing Commercial Airplanes, Attention: Contractual & Data Services
(C&DS), 2600 Westminster Blvd., MC 110-SK57, Seal Beach, CA 90740-
5600; telephone 562-797-1717; internet https://www.myboeingfleet.com.
(4) You may view this service information at the FAA, Transport
Standards Branch, 2200 South 216th St., Des Moines, WA. For
information on the availability of this material at the FAA, call
206-231-3195.
(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: http://www.archives.gov/federal-register/cfr/ibr-locations.html.
Exact source excerpt. Text positions 19335–20597, end exclusive, in the original decoded publication. SHA-256: 34bafb958fef9405c700fbd1edf74e61ee267fa779b5e9a21f335cac4ee95aa7
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 2018-23-13 · 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: 9bf04b8a4307dc7d36e90fc94aa04ab01a2c52ba527e8790002383d431a46c39. Source manifest: 4224355ab2805dd6f9aa888d2fc8f5719b8e947d73943df1fa10b52502d8f71d.
Official source · 2018-11-27
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 83, Number 228 (Tuesday, November 27, 2018)]
[Rules and Regulations]
[Pages 60759-60761]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2018-25394]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2018-0489; Product Identifier 2018-NM-001-AD; Amendment
39-19500; AD 2018-23-13]
RIN 2120-AA64
Airworthiness Directives; The Boeing Company Airplanes
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Final rule.
-----------------------------------------------------------------------
SUMMARY: We are adopting a new airworthiness directive (AD) for all The
Boeing Company Model 747-8 and 747-8F series airplanes. This AD was
prompted by a report that flightcrew oxygen masks did not function as
designed during flight testing. This AD requires an inspection to
determine if certain oxygen masks/regulators are installed, and
replacement if necessary. We are issuing this AD to address the unsafe
condition on these products.
DATES: This AD is effective January 2, 2019.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in this AD as of January 2,
2019.
ADDRESSES: For service information identified in this final rule,
contact Boeing Commercial Airplanes, Attention: Contractual & Data
Services (C&DS), 2600 Westminster Blvd., MC 110-SK57, Seal Beach, CA
90740-5600; telephone 562-797-1717; internet https://www.myboeingfleet.com. You may view this service information at the
FAA, Transport Standards Branch, 2200 South 216th St., Des Moines, WA.
For information on the availability of this material at the FAA, call
206-231-3195. It is also available on the internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2018-
0489.
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-2018-
0489; 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 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: Susan L. Monroe, Aerospace Engineer,
Cabin Safety and Environmental Systems Section, FAA, Seattle ACO
Branch, 2200 South 216th St., Des Moines, WA 98198; phone and fax: 206-
231-3570; email: [email protected].
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 all The Boeing Company
Model 747-8 and 747-8F series airplanes. The NPRM published in the
Federal Register on May 30, 2018 (83 FR 24688). The NPRM was prompted
by a report that flightcrew oxygen masks did not function as designed
during flight testing. The NPRM proposed to require an inspection to
determine whether certain oxygen masks/regulators and stowage boxes are
installed and replacement if necessary.
We are issuing this AD to address flightcrew oxygen masks/
regulators that do not deploy correctly, which could result in a delay
for the flightcrew to put on the masks, which may lead to hypoxia and
loss of useful consciousness, potentially resulting in loss of control
of the airplane.
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.
Request To Include Training for Proper Mask-Packing
Zodiac Aerospace recommended that we revise paragraphs (g) and (h)
to include training for proper mask-packing as an alternative to
replacement. The commenter stated that if operators have followed
proper packing procedures, no equipment change should be required.
Although we acknowledge Zodiac's recommendation, we note that the
supplier had previously provided mask-packing training to Boeing, and
that trained, certified mask packers had packed the masks that failed.
We have determined that mandating a design change is necessary to
effectively mitigate the unsafe condition. We have not changed this AD
in this regard.
Request To Revise Proposed Parts Installation Limitation
Boeing requested that we revise paragraph (i) of the proposed AD to
provide that subsequent changes or modifications may be handled by
normal operator procedures without requiring approval of an alternative
method of compliance (AMOC) as long as oxygen mask/regulator part
number (P/N) MLD20-626-l is not reintroduced as part of the subsequent
change. Boeing considered paragraph (i)(3) of the proposed AD to be too
restrictive because operators would be burdened with requests for AMOCs
for each subsequent change or modification.
We partially agree with the commenter. We agree that options are
warranted for operators because the proposed AD was highly restrictive,
given the limited nature of the unsafe condition. Therefore, we have
revised paragraph (g) of this AD to provide alternative actions to
correct the unsafe condition, thereby reducing the need for AMOC
requests. We also removed the requirement to inspect for the oxygen
mask stowage box because that inspection is no longer needed based on
these alternative actions.
However, we disagree with revising or deleting paragraph (i)(3) of
this AD because the requirement refers to the dependent relationship
between the new mask/regulator part number and the new oxygen mask
stowage box part number required by the service information. The
installation of oxygen mask/regulator P/N MLD20-726-1 with
[[Page 60760]]
any oxygen mask stowage box part number other than P/N MXP806-7 will
require FAA approval in accordance with the procedures specified in
paragraph (j) of this AD.
Request To Revise the Proposed Applicability To Include a Similar Part
The commenter, DLH/LHT (Deutsche Lufthansa/Lufthansa-Technik),
requested that we revise the proposed applicability to include P/N
MLC20-626-1 as another affected oxygen mask/regulator in the proposed
AD. The commenter stated that P/N MLC20-626-1 is identical to P/N
MLD20-626-1, except for the goggles, and that this is why the oxygen
mask/regulator shows both of these part numbers on the identification
label. The commenter reasoned that an operator tracking the mask under
the affected part number only would not be subject to the proposed AD.
We do not agree with the request. We are evaluating the associated
risks of P/N MLC20-626-1 in relation to the unsafe condition identified
in this AD; however, it is not in the interest of public safety to
delay this action further. We might consider additional rulemaking to
address our findings. We have not changed this AD in this regard.
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:
<bullet> Are consistent with the intent that was proposed in the
NPRM for addressing 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 final
rule.
Related Service Information Under 1 CFR Part 51
We reviewed Boeing Special Attention Service Bulletin 747-35-2133,
Revision 1, dated November 1, 2017. This service information describes
procedures for replacing certain oxygen masks/regulators and stowage
boxes. 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 18 airplanes of U.S. registry. We
estimate the following costs to comply with this AD:
Estimated Costs for Required Actions
--------------------------------------------------------------------------------------------------------------------------------------------------------
Action Labor cost Parts cost Cost per product Cost on U.S. operators
--------------------------------------------------------------------------------------------------------------------------------------------------------
Inspection.......................... 1 work-hour x $85 per $0 $85................................ $1,530.
hour = $85.
Replacement......................... Up to 6 work-hours x $85 68,256 Up to $68,766...................... Up to $1,237,788.
per hour = $510.
--------------------------------------------------------------------------------------------------------------------------------------------------------
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 transport category airplanes and
associated appliances to the Director of the System Oversight 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 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 adding the following new airworthiness
directive (AD):
2018-23-13 The Boeing Company: Amendment 39-19500; Docket No. FAA-
2018-0489; Product Identifier 2018-NM-001-AD.
(a) Effective Date
This AD is effective January 2, 2019.
(b) Affected ADs
None.
(c) Applicability
This AD applies to all The Boeing Company Model 747-8 and 747-8F
series airplanes, certificated in any category.
(d) Subject
Air Transport Association (ATA) of America Code 35, Oxygen.
[[Page 60761]]
(e) Unsafe Condition
This AD was prompted by a report that flightcrew oxygen masks
did not function as designed during flight testing. We are issuing
this AD to address flightcrew oxygen masks/regulators that do not
deploy correctly, which could result in a delay for the flightcrew
to put on the masks, which may lead to hypoxia and loss of useful
consciousness, potentially resulting in loss of control of the
airplane.
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
(g) Required Actions
For airplanes with an original certificate of airworthiness, or
an original export certificate of airworthiness, issued on or before
the effective date of this AD: Within 72 months after the effective
date of this AD, inspect for oxygen mask/regulator part number (P/N)
MLD20-626-1. A review of airplane maintenance records is acceptable
in lieu of the part number inspection if the part number of the
oxygen mask/regulator can be conclusively determined from that
review. If any oxygen mask/regulator P/N MLD20-626-1 is found,
within 72 months after the effective date of this AD, do the actions
identified in paragraph (g)(1), (g)(2), or (g)(3) of this AD.
(1) Do all applicable actions identified as ``RC'' (required for
compliance) in, and in accordance with, the Accomplishment
Instructions of Boeing Special Attention Service Bulletin 747-35-
2133, Revision 1, dated November 1, 2017, except as provided by
paragraph (h) of this AD.
(2) Except as specified in paragraph (i)(3) of this AD: Remove
oxygen mask/regulator P/N MLD20-626-1 and install any new or
serviceable oxygen mask/regulator that is not P/N MLD20-626-1 and
that is FAA approved for installation on the airplane.
Note 1 to paragraphs (g)(2) and (g)(3) of this AD: Guidance for
the installation procedures can be found in Boeing Model 747
Aircraft Maintenance Manual (AMM) 35-11-18.
(3) Except as specified in paragraph (i)(3) of this AD: Remove
the oxygen mask/regulator P/N MLD20-626-1 and the installed oxygen
mask stowage box combination, and install any new or serviceable
oxygen mask/regulator and stowage box combination that does not
include oxygen mask/regulator P/N MLD20-626-1, and that is FAA
approved for installation on the airplane.
(h) Exceptions to Service Information Specifications
Where Boeing Special Attention Service Bulletin 747-35-2133,
Revision 1, dated November 1, 2017, refers to or specifies
installing a new (or changed) part, for this AD, a new or
serviceable (or changed) part is acceptable.
(i) Parts Installation Limitations
(1) For airplanes with an original certificate of airworthiness,
or an original export certificate of airworthiness, issued on or
before the effective date of this AD: As of the effective date of
this AD, no person may install an oxygen mask/regulator P/N MLD20-
626-1 on any airplane, except that prior to 72 months after the
effective date of this AD, installation of P/N MLD20-626-1 is
acceptable for unscheduled maintenance as a replacement only for
another P/N MLD20-626-1, and only into a stowage box having P/N
MXP806-1. If an oxygen mask/regulator having a part number other
than P/N MLD20-626-1 is installed, it may not be replaced with P/N
MLD20-626-1. For the purposes of this AD, unscheduled maintenance is
defined as maintenance that was not planned for or scheduled in
advance, such as changing a defective or unserviceable oxygen mask
at dispatch.
(2) For airplanes with an original certificate of airworthiness
or an original export certificate of airworthiness issued after the
effective date of this AD: As of the effective date of this AD, no
person may install oxygen mask/regulator P/N MLD20-626-1 on any
airplane.
(3) For all airplanes: As of the effective date of this AD, no
person may install oxygen mask/regulator P/N MLD20-726-1 in
combination with any stowage box part number that is not P/N MXP806-
7 on any airplane.
(j) Alternative Methods of Compliance (AMOCs)
(1) The Manager, Seattle 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 certification office, send it to the attention of the
person identified in paragraph (k)(1) of this AD. Information may be
emailed to: [email protected].
(2) Before using any approved AMOC, notify your appropriate
principal inspector, or lacking a principal inspector, the manager
of the local flight standards district office/certificate holding
district office.
(3) An AMOC that provides an acceptable level of safety may be
used for any repair, modification, or alteration required by this AD
if it is approved by the Boeing Commercial Airplanes Organization
Designation Authorization (ODA) that has been authorized by the
Manager, Seattle ACO Branch, FAA, to make those findings. To be
approved, the repair method, modification deviation, or alteration
deviation must meet the certification basis of the airplane, and the
approval must specifically refer to this AD.
(4) Except as required by paragraph (h) of this AD: For service
information that contains steps that are labeled as RC, the
provisions of paragraphs (j)(4)(i) and (j)(4)(ii) of this AD apply.
(i) The steps labeled as RC, including substeps under an RC step
and any figures identified in an RC step, must be done to comply
with the AD. If a step or substep is labeled ``RC Exempt,'' then the
RC requirement is removed from that step or substep. An AMOC is
required for any deviations to RC steps, including substeps and
identified figures.
(ii) Steps not labeled as RC may be deviated from using accepted
methods in accordance with the operator's maintenance or inspection
program without obtaining approval of an AMOC, provided the RC
steps, including substeps and identified figures, can still be done
as specified, and the airplane can be put back in an airworthy
condition.
(k) Related Information
(1) For more information about this AD, contact Susan L. Monroe,
Aerospace Engineer, Cabin Safety and Environmental Systems Section,
FAA, Seattle ACO Branch, 2200 South 216th St., Des Moines, WA 98198;
phone and fax: 206-231-3570; email: [email protected].
(2) Service information identified in this AD that is not
incorporated by reference is available at the addresses specified in
paragraphs (k)(3) and (k)(4) of this AD.
(l) 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) Boeing Special Attention Service Bulletin 747-35-2133,
Revision 1, dated November 1, 2017.
(ii) [Reserved]
(3) For service information identified in this AD, contact
Boeing Commercial Airplanes, Attention: Contractual & Data Services
(C&DS), 2600 Westminster Blvd., MC 110-SK57, Seal Beach, CA 90740-
5600; telephone 562-797-1717; internet https://www.myboeingfleet.com.
(4) You may view this service information at the FAA, Transport
Standards Branch, 2200 South 216th St., Des Moines, WA. For
information on the availability of this material at the FAA, call
206-231-3195.
(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: http://www.archives.gov/federal-register/cfr/ibr-locations.html.
Issued in Des Moines, Washington, on November 8, 2018.
Chris Spangenberg,
Acting Director, System Oversight Division, Aircraft Certification
Service.
[FR Doc. 2018-25394 Filed 11-26-18; 8:45 am]
BILLING CODE 4910-13-P
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