83 FR 31509 - Airworthiness Directives; The Boeing Company Airplanes
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration Federal Register Volume 83, Issue 130 (July 6, 2018)
Federal Aviation Administration
Federal Register Volume 83, Issue 130 (July 6, 2018)
| Page Range | 31509-31511 | |
| FR Document | 2018-14425 |
[Federal Register Volume 83, Number 130 (Friday, July 6, 2018)] [Proposed Rules] [Pages 31509-31511] From the Federal Register Online [www.thefederalregister.org] [FR Doc No: 2018-14425] ----------------------------------------------------------------------- DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2018-0581; Product Identifier 2018-NM-029-AD] RIN 2120-AA64 Airworthiness Directives; The Boeing Company Airplanes AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Notice of proposed rulemaking (NPRM). ----------------------------------------------------------------------- SUMMARY: We propose to adopt a new airworthiness directive (AD) for certain The Boeing Company Model 777-200, -200LR, -300, and -300ER series airplanes. This proposed AD was prompted by a report that showed a non-compliance exists on some in-service galley attendant seat fitting installations. The non-compliance could result in flight attendant seats failing in a high-G crash. This proposed AD would require modifications for galley mounted seat fittings. We are proposing this AD to address the unsafe condition on these products. DATES: We must receive comments on this proposed AD by August 20, 2018. ADDRESSES: You may send comments, using the procedures found in 14 CFR 11.43 and 11.45, by any of the following methods:Federal eRulemaking Portal: Go to http://www.regulations.gov. Follow the instructions for submitting comments. Fax: 202-493-2251. Mail: U.S. Department of Transportation, Docket Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New Jersey Avenue SE, Washington, DC 20590. Hand Delivery: Deliver to Mail address above between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. For service information identified in this NPRM, 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 referenced 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-2018-0581. 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- 0581; 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 NPRM, the regulatory evaluation, any comments received, and other information. The street address for the Docket Office (phone: 800-647-5527) is in the ADDRESSES section. Comments will be available in the AD docket shortly after receipt. FOR FURTHER INFORMATION CONTACT: Allison Buss, Aerospace Engineer, Cabin Safety and Environmental Systems Section, FAA, Seattle ACO Branch, 2200 South 216th St., Des Moines, WA 98198; phone and fax: 206- 231-3564; email: [email protected]. SUPPLEMENTARY INFORMATION: Comments Invited We invite you to send any written relevant data, views, or arguments about this proposal. Send your comments to an address listed under the ADDRESSES section. Include ``Docket No. FAA-2018-0581; Product Identifier 2018-NM-029-AD'' at the beginning of your comments. We specifically invite comments on the overall regulatory, [[Page 31510]] economic, environmental, and energy aspects of this NPRM. We will consider all comments received by the closing date and may amend this NPRM because of those comments. We will post all comments we receive, without change, to http://www.regulations.gov, including any personal information you provide. We will also post a report summarizing each substantive verbal contact we receive about this proposed AD. Discussion We have received a report that showed a non-compliance exists on some in-service galley attendant seat fitting installations. This condition, if not addressed, could result in flight attendant seats failing in a high-G crash, resulting in potential injury to flight attendants and consequent inability of the flight attendants to assist with passenger evacuation in a timely manner. Related Service Information Under 1 CFR Part 51 We reviewed Boeing Special Attention Service Bulletin 777-25-0649, Revision 1, dated October 6, 2017. The service information describes procedures for modifications for galley mounted seat fittings. 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. FAA's Determination We are proposing this AD because we evaluated all the relevant information and determined the unsafe condition described previously is likely to exist or develop in other products of the same type design. Proposed AD Requirements This proposed AD would require accomplishment of the actions identified as ``RC'' (required for compliance) in the Accomplishment Instructions of Boeing Special Attention Service Bulletin 777-25-0649, Revision 1, dated October 6, 2017, described previously, except as discussed under ``Differences Between this Proposed AD and the Service Information,'' and except for any differences identified as exceptions in the regulatory text of this proposed AD. For information on the procedures and compliance times, see this service information at http://www.regulations.gov by searching for and locating Docket No. FAA-2018-0581. Differences Between This Proposed AD and the Service Information Boeing Special Attention Service Bulletin 777-25-0649, Revision 1, dated October 6, 2017, specifies the compliance time as 1,875 days. For this proposed AD, we specified the compliance time as 6 years. We have coordinated this difference with Boeing. Costs of Compliance We estimate that this proposed AD affects 50 airplanes of U.S. registry. We estimate the following costs to comply with this proposed AD: Estimated Costs for Required Actions ---------------------------------------------------------------------------------------------------------------- Cost per Cost on U.S. Action Labor cost Parts cost product operators ---------------------------------------------------------------------------------------------------------------- Modification....................... 7 work-hours x $85 per hour $0 $595 $29,750 = $595. ---------------------------------------------------------------------------------------------------------------- According to the manufacturer, some or all of the costs of this proposed 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 known costs in our cost estimate. 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 proposed 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 to the Director of the System Oversight Division. Regulatory Findings We determined that this proposed AD would not have federalism implications under Executive Order 13132. This proposed AD would 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 proposed regulation: (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. The Proposed Amendment Accordingly, under the authority delegated to me by the Administrator, the FAA proposes to amend 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. [[Page 31511]] Sec. 39.13 [Amended] 0 2. The FAA amends Sec. 39.13 by adding the following new airworthiness directive (AD): The Boeing Company: Docket No. FAA-2018-0581; Product Identifier 2018-NM-029-AD. (a) Comments Due Date We must receive comments by August 20, 2018. (b) Affected ADs None. (c) Applicability This AD applies to The Boeing Company Model 777-200, -200LR, - 300, and -300ER series airplanes, certificated in any category, as identified in Boeing Special Attention Service Bulletin 777-25-0649, Revision 1, dated October 6, 2017. (d) Subject Air Transport Association (ATA) of America Code 25, Equipment/ furnishings. (e) Unsafe Condition This AD was prompted by a report that showed a non-compliance exists on some in-service galley attendant seat fitting installations. The non-compliance could result in flight attendant seats failing in a high-G crash. We are issuing this AD to address non-compliant flight attendant seats, which could fail in a high-G crash and result in potential injury to flight attendants and consequent inability of the flight attendants to assist with passenger evacuation in a timely manner. (f) Compliance Comply with this AD within the compliance times specified, unless already done. (g) Required Actions Within 6 years after the effective date of this AD, do all applicable actions identified as ``RC'' (required for compliance) in, and in accordance with, the Accomplishment Instructions of Boeing Special Attention Service Bulletin 777-25-0649, Revision 1, dated October 6, 2017. (h) 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 (i)(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) For service information that contains steps that are labeled as RC, the provisions of paragraphs (h)(4)(i) and (h)(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. (i) Related Information (1) For more information about this AD, contact Allison Buss, Aerospace Engineer, Cabin Safety and Environmental Systems Section, FAA, Seattle ACO Branch, 2200 South 216th St., Des Moines, WA 98198; phone and fax: 206-231-3564; email: [email protected]. (2) 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. You may view this referenced 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. Issued in Des Moines, Washington, on June 21, 2018. Michael Kaszycki, Acting Director, System Oversight Division, Aircraft Certification Service. [FR Doc. 2018-14425 Filed 7-5-18; 8:45 am] BILLING CODE 4910-13-P
![Federal Register / Vol. 83, No. 130 / Friday, July 6, 2018 / Proposed Rules 31509
the Accomplishment Instructions of Boeing or inspection program without obtaining 11.43 and 11.45, by any of the following
Requirements Bulletin 737–25–1758 RB, approval of an AMOC, provided the RC steps, methods:
dated November 8, 2017. including substeps and identified figures, can • Federal eRulemaking Portal: Go to
still be done as specified, and the airplane
Note 1 to paragraph (g)(2) of this AD: can be put back in an airworthy condition.
http://www.regulations.gov. Follow the
Guidance for accomplishing the actions instructions for submitting comments.
required by this AD can be found in Boeing (j) Related Information • Fax: 202–493–2251.
Service Bulletin 737–25–1758, dated (1) For more information about this AD, • Mail: U.S. Department of
November 8, 2017, which is referred to in contact Scott Craig, Aerospace Engineer, Transportation, Docket Operations,
Boeing Requirements Bulletin 737–25–1758 Cabin Safety and Environmental Systems M–30, West Building Ground Floor,
RB, dated November 8, 2017. Section, FAA, Seattle ACO Branch, 2200 Room W12–140, 1200 New Jersey
South 216th St., Des Moines, WA 98198;
Avenue SE, Washington, DC 20590.
phone and fax: 206–231–3566; email:
(h) Exceptions to Service Information
Michael.S.Craig@faa.gov. • Hand Delivery: Deliver to Mail
Specifications address above between 9 a.m. and 5
(2) For service information identified in
(1) For purposes of determining this AD, contact Boeing Commercial p.m., Monday through Friday, except
compliance with the requirements of this AD: Airplanes, Attention: Contractual & Data Federal holidays.
Where Boeing Service Bulletin 737–25–1728, Services (C&DS), 2600 Westminster Blvd., For service information identified in
dated October 10, 2016, uses the phrase ‘‘the MC 110–SK57, Seal Beach, CA 90740–5600; this NPRM, contact Boeing Commercial
original issue date of this service bulletin,’’ telephone 562–797–1717; internet https://
this AD requires using ‘‘the effective date of
Airplanes, Attention: Contractual & Data
www.myboeingfleet.com. You may view this
this AD.’’ Services (C&DS), 2600 Westminster
referenced service information at the FAA,
(2) For purposes of determining Transport Standards Branch, 2200 South Blvd., MC 110–SK57, Seal Beach, CA
compliance with the requirements of this AD: 216th St., Des Moines, WA. For information 90740–5600; telephone 562–797–1717;
Where Boeing Requirements Bulletin 737– on the availability of this material at the internet https://www.myboeingfleet.
25–1758 RB, dated November 8, 2017, uses FAA, call 206–231–3195. com. You may view this referenced
the phrase ‘‘the original issue date of the service information at the FAA,
Requirements Bulletin (RB),’’ this AD Issued in Des Moines, Washington, on June
21, 2018. Transport Standards Branch, 2200
requires using ‘‘the effective date of this AD.’’
Michael Kaszycki, South 216th St., Des Moines, WA. For
(i) Alternative Methods of Compliance
Acting Director, System Oversight Division, information on the availability of this
(AMOCs) material at the FAA, call 206–231–3195.
Aircraft Certification Service.
(1) The Manager, Seattle ACO Branch, [FR Doc. 2018–14397 Filed 7–5–18; 8:45 am]
It is also available on the internet at
FAA, has the authority to approve AMOCs http://www.regulations.gov by searching
for this AD, if requested using the procedures BILLING CODE 4910–13–P
for and locating Docket No. FAA–2018–
found in 14 CFR 39.19. In accordance with 0581.
14 CFR 39.19, send your request to your
principal inspector or local Flight Standards DEPARTMENT OF TRANSPORTATION Examining the AD Docket
District Office, as appropriate. If sending
information directly to the manager of the Federal Aviation Administration You may examine the AD docket on
certification office, send it to the attention of the internet at http://
the person identified in paragraph (j)(1) of 14 CFR Part 39 www.regulations.gov by searching for
this AD. Information may be emailed to: 9- and locating Docket No. FAA–2018–
ANM-Seattle-ACO-AMOC-Requests@faa.gov. [Docket No. FAA–2018–0581; Product 0581; or in person at the Docket
(2) Before using any approved AMOC, Identifier 2018–NM–029–AD]
Management Facility between 9 a.m.
notify your appropriate principal inspector, RIN 2120–AA64 and 5 p.m., Monday through Friday,
or lacking a principal inspector, the manager
except Federal holidays. The AD docket
of the local flight standards district office/ Airworthiness Directives; The Boeing
certificate holding district office. contains this NPRM, the regulatory
Company Airplanes evaluation, any comments received, and
(3) An AMOC that provides an acceptable
level of safety may be used for any repair, AGENCY: Federal Aviation other information. The street address for
modification, or alteration required by this Administration (FAA), DOT. the Docket Office (phone: 800–647–
AD if it is approved by the Boeing 5527) is in the ADDRESSES section.
ACTION: Notice of proposed rulemaking
Commercial Airplanes Organization Comments will be available in the AD
Designation Authorization (ODA) that has (NPRM).
docket shortly after receipt.
been authorized by the Manager, Seattle ACO
Branch, FAA, to make those findings. To be
SUMMARY: We propose to adopt a new FOR FURTHER INFORMATION CONTACT:
approved, the repair method, modification airworthiness directive (AD) for certain Allison Buss, Aerospace Engineer,
deviation, or alteration deviation must meet The Boeing Company Model 777–200, Cabin Safety and Environmental
the certification basis of the airplane, and the –200LR, –300, and –300ER series Systems Section, FAA, Seattle ACO
approval must specifically refer to this AD. airplanes. This proposed AD was Branch, 2200 South 216th St., Des
(4) For service information that contains prompted by a report that showed a Moines, WA 98198; phone and fax: 206–
steps that are labeled as RC, the provisions non-compliance exists on some in- 231–3564; email: Allison.buss@faa.gov.
of paragraphs (i)(4)(i) and (i)(4)(ii) of this AD service galley attendant seat fitting
apply. SUPPLEMENTARY INFORMATION:
(i) The steps labeled as RC, including
installations. The non-compliance could
result in flight attendant seats failing in Comments Invited
substeps under an RC step and any figures
identified in an RC step, must be done to a high-G crash. This proposed AD We invite you to send any written
daltland on DSKBBV9HB2PROD with PROPOSALS
comply with the AD. If a step or substep is would require modifications for galley relevant data, views, or arguments about
labeled ‘‘RC Exempt,’’ then the RC mounted seat fittings. We are proposing this proposal. Send your comments to
requirement is removed from that step or this AD to address the unsafe condition an address listed under the ADDRESSES
substep. An AMOC is required for any on these products.
deviations to RC steps, including substeps
section. Include ‘‘Docket No. FAA–
DATES: We must receive comments on 2018–0581; Product Identifier 2018–
and identified figures.
(ii) Steps not labeled as RC may be this proposed AD by August 20, 2018. NM–029–AD’’ at the beginning of your
deviated from using accepted methods in ADDRESSES: You may send comments, comments. We specifically invite
accordance with the operator’s maintenance using the procedures found in 14 CFR comments on the overall regulatory,
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![Federal Register / Vol. 83, No. 130 / Friday, July 6, 2018 / Proposed Rules 31511
§ 39.13 [Amended] modification, or alteration required by this ACTION: Proposed rule.
■ 2. The FAA amends § 39.13 by adding AD if it is approved by the Boeing
the following new airworthiness Commercial Airplanes Organization SUMMARY: Pursuant to the Federal Clean
Designation Authorization (ODA) that has
directive (AD): Air Act (CAA or the Act), the
been authorized by the Manager, Seattle ACO
The Boeing Company: Docket No. FAA– Branch, FAA, to make those findings. To be Environmental Protection Agency (EPA)
2018–0581; Product Identifier 2018– approved, the repair method, modification is proposing to approve revisions to the
NM–029–AD. deviation, or alteration deviation must meet State Implementation Plan (SIP) for
the certification basis of the airplane, and the Oklahoma submitted by the State of
(a) Comments Due Date approval must specifically refer to this AD. Oklahoma designee with a letter dated
We must receive comments by August 20, (4) For service information that contains February 14, 2017. The submittal covers
2018. steps that are labeled as RC, the provisions updates to the Oklahoma SIP, as
of paragraphs (h)(4)(i) and (h)(4)(ii) of this
(b) Affected ADs AD apply. contained in annual SIP updates for
None. (i) The steps labeled as RC, including 2013, 2014, 2015, and 2016, and
substeps under an RC step and any figures incorporates the latest changes to EPA
(c) Applicability
identified in an RC step, must be done to regulations. This action will address the
This AD applies to The Boeing Company comply with the AD. If a step or substep is revisions submitted to the Oklahoma
Model 777–200, –200LR, –300, and –300ER labeled ‘‘RC Exempt,’’ then the RC SIP pertaining to incorporation by
series airplanes, certificated in any category, requirement is removed from that step or
as identified in Boeing Special Attention
reference of federal requirements and
substep. An AMOC is required for any
Service Bulletin 777–25–0649, Revision 1, deviations to RC steps, including substeps
emission inventory reporting
dated October 6, 2017. and identified figures. requirements.
(ii) Steps not labeled as RC may be
(d) Subject
deviated from using accepted methods in
DATES: Written comments must be
Air Transport Association (ATA) of accordance with the operator’s maintenance received on or before August 6, 2018.
America Code 25, Equipment/furnishings. or inspection program without obtaining ADDRESSES: Submit your comments,
(e) Unsafe Condition approval of an AMOC, provided the RC steps, identified by Docket No. EPA–R06–
including substeps and identified figures, can
This AD was prompted by a report that still be done as specified, and the airplane
OAR–2018–0350, at http://
showed a non-compliance exists on some in- can be put back in an airworthy condition. www.regulations.gov or via email to
service galley attendant seat fitting wiley.adina@epa.gov. Follow the online
installations. The non-compliance could (i) Related Information instructions for submitting comments.
result in flight attendant seats failing in a (1) For more information about this AD, Once submitted, comments cannot be
high-G crash. We are issuing this AD to contact Allison Buss, Aerospace Engineer, edited or removed from Regulations.gov.
address non-compliant flight attendant seats, Cabin Safety and Environmental Systems The EPA may publish any comment
which could fail in a high-G crash and result Section, FAA, Seattle ACO Branch, 2200
in potential injury to flight attendants and South 216th St., Des Moines, WA 98198; received to its public docket. Do not
consequent inability of the flight attendants phone and fax: 206–231–3564; email: submit electronically any information
to assist with passenger evacuation in a Allison.buss@faa.gov. you consider to be Confidential
timely manner. (2) For service information identified in Business Information (CBI) or other
this AD, contact Boeing Commercial information whose disclosure is
(f) Compliance Airplanes, Attention: Contractual & Data restricted by statute. Multimedia
Comply with this AD within the Services (C&DS), 2600 Westminster Blvd., submissions (audio, video, etc.) must be
compliance times specified, unless already MC 110–SK57, Seal Beach, CA 90740–5600; accompanied by a written comment.
done. telephone 562–797–1717; internet https://
www.myboeingfleet.com. You may view this The written comment is considered the
(g) Required Actions referenced service information at the FAA, official comment and should include
Within 6 years after the effective date of Transport Standards Branch, 2200 South discussion of all points you wish to
this AD, do all applicable actions identified 216th St., Des Moines, WA. For information make. The EPA will generally not
as ‘‘RC’’ (required for compliance) in, and in on the availability of this material at the consider comments or comment
accordance with, the Accomplishment FAA, call 206–231–3195. contents located outside of the primary
Instructions of Boeing Special Attention submission (i.e. on the web, cloud, or
Service Bulletin 777–25–0649, Revision 1, Issued in Des Moines, Washington, on June
21, 2018.
other file sharing system). For
dated October 6, 2017.
additional submission methods, please
(h) Alternative Methods of Compliance Michael Kaszycki,
contact Adina Wiley, 214–665–2115,
(AMOCs) Acting Director, System Oversight Division,
wiley.adina@epa.gov. For the full EPA
Aircraft Certification Service.
(1) The Manager, Seattle ACO Branch, public comment policy, information
FAA, has the authority to approve AMOCs [FR Doc. 2018–14425 Filed 7–5–18; 8:45 am]
about CBI or multimedia submissions,
for this AD, if requested using the procedures BILLING CODE 4910–13–P and general guidance on making
found in 14 CFR 39.19. In accordance with effective comments, please visit http://
14 CFR 39.19, send your request to your www2.epa.gov/dockets/commenting-
principal inspector or local Flight Standards ENVIRONMENTAL PROTECTION
District Office, as appropriate. If sending
epa-dockets.
AGENCY Docket: The index to the docket for
information directly to the manager of the
certification office, send it to the attention of 40 CFR Part 52 this action is available electronically at
the person identified in paragraph (i)(1) of www.regulations.gov and in hard copy
daltland on DSKBBV9HB2PROD with PROPOSALS
this AD. Information may be emailed to: 9- [EPA–R06–OAR–2018–0350; FRL–9979– at the EPA Region 6, 1445 Ross Avenue,
ANM-Seattle-ACO-AMOC-Requests@faa.gov. 54—Region 6] Suite 700, Dallas, Texas. While all
(2) Before using any approved AMOC,
documents in the docket are listed in
notify your appropriate principal inspector, Approval and Promulgation of
or lacking a principal inspector, the manager the index, some information may be
Implementation Plans; Oklahoma;
of the local flight standards district office/ publicly available only at the hard copy
General SIP Updates
certificate holding district office. location (e.g., copyrighted material), and
(3) An AMOC that provides an acceptable AGENCY: Environmental Protection some may not be publicly available at
level of safety may be used for any repair, Agency (EPA). either location (e.g., CBI).
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Document Created: 2018-07-06 00:46:52
Document Modified: 2018-07-06 00:46:52
| Category | Regulatory Information | |
| Collection | Federal Register | |
| sudoc Class | AE 2.7: GS 4.107: AE 2.106: | |
| Publisher | Office of the Federal Register, National Archives and Records Administration | |
| Section | Proposed Rules | |
| Action | Notice of proposed rulemaking (NPRM). | |
| Dates | We must receive comments on this proposed AD by August 20, 2018. | |
| Contact | Allison Buss, Aerospace Engineer, Cabin Safety and Environmental Systems Section, FAA, Seattle ACO Branch, 2200 South 216th St., Des Moines, WA 98198; phone and fax: 206- 231-3564; email: [email protected] | |
| FR Citation | 83 FR 31509 | |
| RIN Number | 2120-AA64 | |
| CFR Associated | Air Transportation; Aircraft; Aviation Safety; Incorporation by Reference and Safety |
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