81 FR 63433 - Airworthiness Directives; The Boeing Company Airplanes
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration Federal Register Volume 81, Issue 179 (September 15, 2016)
Federal Aviation Administration
Federal Register Volume 81, Issue 179 (September 15, 2016)
| Page Range | 63433-63435 | |
| FR Document | 2016-22101 |
[Federal Register Volume 81, Number 179 (Thursday, September 15, 2016)] [Proposed Rules] [Pages 63433-63435] From the Federal Register Online [www.thefederalregister.org] [FR Doc No: 2016-22101] ======================================================================= ----------------------------------------------------------------------- DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2016-9075; Directorate Identifier 2016-NM-082-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 787-8 and 787-9 airplanes. This proposed AD was prompted by a report indicating that a portion of the sealant above the engine pylon between the wing skin and the vapor barrier may have been omitted. This proposed AD would require an inspection for missing sealant in the seam on the outside and inside of the engine struts, and corrective actions if necessary. We are proposing this AD to detect and correct missing sealant above the engine pylon between the wing skin and the vapor barrier, which can create an unintended leak path for fuel, potentially draining onto the aft fairing heat shield above the engine and onto hot engine parts or brakes, which could lead to a major ground fire. DATES: We must receive comments on this proposed AD by October 31, 2016. 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: Data & Services Management, P.O. Box 3707, MC 2H-65, Seattle, WA 98124-2207; telephone 206-544-5000, extension 1; fax 206-766-5680; Internet https://www.myboeingfleet.com. You may view this referenced service information at the FAA, Transport Airplane Directorate, 1601 Lind Avenue SW., Renton, WA. For information on the availability of this material at the FAA, call 425-227-1221. It is also available on the internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2016-9075. 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-2016- 9075; 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 proposed AD, 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: Sherry Vevea, Aerospace Engineer, Propulsion Branch, ANM-140S, FAA, Seattle Aircraft Certification Office (ACO), 1601 Lind Avenue SW., Renton, WA 98057-3356; phone: 425-917- 6514; fax: 425-917-6590; email: [email protected]. SUPPLEMENTARY INFORMATION: Comments Invited We invite you to send any written relevant data, views, or arguments about [[Page 63434]] this proposal. Send your comments to an address listed under the ADDRESSES section. Include ``Docket No. FAA-2016-9075; Directorate Identifier 2016-NM-082-AD'' at the beginning of your comments. We specifically invite comments on the overall regulatory, economic, environmental, and energy aspects of this proposed AD. We will consider all comments received by the closing date and may amend this proposed AD 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 indicating that a portion of the sealant above the engine pylon between the wing skin and the vapor barrier may have been omitted due to a manufacturing sequencing issue. This condition, if not corrected, can create an unintended leak path for fuel, potentially draining onto the aft fairing heat shield above the engine and onto hot engine parts or brakes, which could lead to a major ground fire. Related Service Information Under 1 CFR Part 51 We reviewed Boeing Alert Service Bulletin B787-81205-SB570029-00, Issue 001, dated February 23, 2016. The service information describes procedures for doing an inspection for missing sealant in the seam on the outside and inside of the engine struts, and installing missing sealant. 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 accomplishing the actions specified in the service information described previously. 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-2016- 9075. The phrase ``corrective actions'' is used in this proposed AD. Corrective actions correct or address any condition found. Corrective actions in an AD could include, for example, repairs. Costs of Compliance We estimate that this proposed AD affects 32 airplanes of U.S. registry. We estimate the following costs to comply with this proposed AD: Estimated Costs ---------------------------------------------------------------------------------------------------------------- Cost per Cost on U.S. Action Labor cost Parts cost product operators ---------------------------------------------------------------------------------------------------------------- Inspection............................ 3 work-hours x $85 per $0 $255 $8,160 hour = $255. ---------------------------------------------------------------------------------------------------------------- We estimate the following costs to do any necessary repairs that would be required based on the results of the proposed inspection. We have no way of determining the number of aircraft that might need these repairs: On-Condition Costs ---------------------------------------------------------------------------------------------------------------- Cost per Action Labor cost Parts cost product ---------------------------------------------------------------------------------------------------------------- Repair..................................... Up to 3 work-hours x $85 per hour = (\1\) (\1\) $255. ---------------------------------------------------------------------------------------------------------------- \1\ We have received no definitive data that would enable us to provide cost estimates for the on-condition material costs specified in this proposed AD. According to the manufacturer, some 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 available 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. 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. [[Page 63435]] 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. 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-2016-9075; Directorate Identifier 2016-NM-082-AD. (a) Comments Due Date We must receive comments by October 31, 2016. (b) Affected ADs None. (c) Applicability This AD applies to The Boeing Company Model 787-8 and 787-9 airplanes, certificated in any category, as identified in Boeing Alert Service Bulletin B787-81205-SB570029-00, Issue 001, dated February 23, 2016. (d) Subject Air Transport Association (ATA) of America Code 57; Wings. (e) Unsafe Condition This AD was prompted by a report indicating that a portion of the sealant above the engine pylon between the wing skin and the vapor barrier may have been omitted. We are issuing this AD to detect and correct missing sealant above the engine pylon between the wing skin and the vapor barrier, which can create an unintended leak path for fuel, potentially draining onto the aft fairing heat shield and onto hot engine parts or brakes, which could lead to a major ground fire. (f) Compliance Comply with this AD within the compliance times specified, unless already done. (g) Inspection and Corrective Actions Within 60 months after the effective date of this AD: Do a general visual inspection for missing sealant in the seam on the outside and inside of the engine struts; and do all applicable corrective actions; in accordance with the Accomplishment Instructions of Boeing Alert Service Bulletin B787-81205-SB570029- 00, Issue 001, dated February 23, 2016. Do all applicable corrective actions before further flight. (h) Alternative Methods of Compliance (AMOCs) (1) The Manager, Seattle Aircraft Certification Office (ACO), FAA, has the authority to approve AMOCs for this AD, if requested using the procedures found in 14 CFR 39.19. In accordance with 14 CFR 39.19, send your request to your principal inspector or local Flight Standards District Office, as appropriate. If sending information directly to the manager of the ACO, 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, 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 Required for Compliance (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 sub-step is labeled ``RC Exempt,'' then the RC requirement is removed from that step or sub-step. 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 Sherry Vevea, Aerospace Engineer, Propulsion Branch, ANM-140S, FAA, Seattle Aircraft Certification Office (ACO), 1601 Lind Avenue SW., Renton, WA 98057-3356; phone: 425 917 6514; fax: 425 917 6590; email: [email protected]. (2) For service information identified in this AD, contact Boeing Commercial Airplanes, Attention: Data & Services Management, P. O. Box 3707, MC 2H-65, Seattle, WA 98124-2207; telephone 206-544- 5000, extension 1; fax 206-766-5680; Internet https://www.myboeingfleet.com. You may view this referenced service information at the FAA, Transport Airplane Directorate, 1601 Lind Avenue SW., Renton, WA. For information on the availability of this material at the FAA, call 425-227-1221. Issued in Renton, Washington, on September 6, 2016. Michael Kaszycki, Acting Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. 2016-22101 Filed 9-14-16; 8:45 am] BILLING CODE 4910-13-P
![Federal Register / Vol. 81, No. 179 / Thursday, September 15, 2016 / Proposed Rules 63433
banking exceptions to the prohibition physical metal to hedge a derivative for DATES: We must receive comments on
on buying and selling physical metal. which that metal is the reference asset this proposed AD by October 31, 2016.
For the reasons described above, the so long as the amount of the physical ADDRESSES: You may send comments,
OCC has determined that the proposed metal used for hedging purposes is using the procedures found in 14 CFR
rule would not result in expenditures by nominal. 11.43 and 11.45, by any of the following
state, local, and Tribal governments, or ■ 3. Add § 7.1023 to subpart A to read methods:
by the private sector, of $100 million or as follows: • Federal eRulemaking Portal: Go to
more. Accordingly, the OCC has not http://www.regulations.gov. Follow the
§ 7.1023 Federal savings associations,
prepared a written statement to prohibition on industrial or commercial instructions for submitting comments.
accompany the proposed rule. metal dealing or investing. • Fax: 202–493–2251.
List of subjects in 12 CFR Part 7 (a) In this section, industrial or • Mail: U.S. Department of
commercial metal means metal Transportation, Docket Operations, M–
Banks, banking, Computer 30, West Building Ground Floor, Room
technology, Credit, Federal savings (including an alloy) in a physical form
primarily suited to industrial or W12–140, 1200 New Jersey Avenue SE.,
associations, Insurance, Investments, Washington, DC 20590.
Metals, National banks, Reporting and commercial use, for example, copper
cathodes. • Hand Delivery: Deliver to Mail
recordkeeping requirements, Securities, address above between 9 a.m. and 5
(b) Federal savings associations may
Surety bonds. p.m., Monday through Friday, except
not deal or invest in industrial or
For the reasons set forth in the commercial metal. Federal savings Federal holidays.
preamble, OCC proposes to amend 12 associations may not buy or sell For service information identified in
CFR part 7 as follows: industrial or commercial metal if the this NPRM, contact Boeing Commercial
purchase or sale is impermissible for a Airplanes, Attention: Data & Services
PART 7—BANK ACTIVITIES AND Management, P.O. Box 3707, MC 2H–65,
national bank.
OPERATIONS Seattle, WA 98124–2207; telephone
Dated: September 7, 2016
■1. The authority citation for part 7 is Thomas J. Curry,
206–544–5000, extension 1; fax 206–
amended to read as follows: 766–5680; Internet https://
Comptroller of the Currency.
www.myboeingfleet.com. You may view
Authority: 12 U.S.C. 1 et seq., 25b, 71, 71a, [FR Doc. 2016–22017 Filed 9–14–16; 8:45 am]
this referenced service information at
92, 92a, 93, 93a, 371, 371a, 481, 484, 1463, BILLING CODE 4810–33–P
1464, 1818, and 5412(b)(2)(B).
the FAA, Transport Airplane
Directorate, 1601 Lind Avenue SW.,
■ 2. Add § 7.1022 to subpart A to read Renton, WA. For information on the
as follows: DEPARTMENT OF TRANSPORTATION availability of this material at the FAA,
§ 7.1022 National bank authority to buy call 425–227–1221. It is also available
Federal Aviation Administration on the internet at http://
and sell exchange, coin, and bullion.
(a) In this section, industrial or www.regulations.gov by searching for
14 CFR Part 39
commercial metal means metal and locating Docket No. FAA–2016–
(including an alloy) in a physical form [Docket No. FAA–2016–9075; Directorate 9075.
Identifier 2016–NM–082–AD]
primarily suited to industrial or Examining the AD Docket
commercial use, for example, copper RIN 2120–AA64
You may examine the AD docket on
cathodes.
(b) Scope of authorization. Section 24 Airworthiness Directives; The Boeing the Internet at http://
(Seventh) of the National Bank Act Company Airplanes www.regulations.gov by searching for
authorizes national banks to buy and and locating Docket No. FAA–2016–
AGENCY: Federal Aviation 9075; or in person at the Docket
sell exchange, coin, and bullion. Administration (FAA), DOT.
Industrial or commercial metal is not Management Facility between 9 a.m.
ACTION: Notice of proposed rulemaking and 5 p.m., Monday through Friday,
exchange, coin, and bullion within the (NPRM).
meaning of this authorization. except Federal holidays. The AD docket
(c) Buying and selling metal as part of SUMMARY: We propose to adopt a new contains this proposed AD, the
or incidental to the business of banking. airworthiness directive (AD) for certain regulatory evaluation, any comments
Section 24 (Seventh) authorizes national The Boeing Company Model 787–8 and received, and other information. The
banks to engage in activities that are 787–9 airplanes. This proposed AD was street address for the Docket Office
part of, or incidental to, the business of prompted by a report indicating that a (phone: 800–647–5527) is in the
banking. Buying and selling industrial ADDRESSES section. Comments will be
portion of the sealant above the engine
or commercial metal for the purpose of pylon between the wing skin and the available in the AD docket shortly after
dealing or investing in that metal is not vapor barrier may have been omitted. receipt.
part of or incidental to the business of This proposed AD would require an FOR FURTHER INFORMATION CONTACT:
banking pursuant to section 24 inspection for missing sealant in the Sherry Vevea, Aerospace Engineer,
(Seventh). seam on the outside and inside of the Propulsion Branch, ANM–140S, FAA,
(d) Other authorities not affected. engine struts, and corrective actions if Seattle Aircraft Certification Office
This section shall not be construed to necessary. We are proposing this AD to (ACO), 1601 Lind Avenue SW., Renton,
rmajette on DSK2TPTVN1PROD with PROPOSALS
preclude a national bank from acquiring detect and correct missing sealant above WA 98057–3356; phone: 425–917–6514;
or selling metal in connection with its the engine pylon between the wing skin fax: 425–917–6590; email:
incidental authority to foreclose on loan and the vapor barrier, which can create sherry.vevea@faa.gov.
collateral, compromise doubtful claims, an unintended leak path for fuel, SUPPLEMENTARY INFORMATION:
or avoid loss in connection with a debt potentially draining onto the aft fairing
previously contracted. This section also heat shield above the engine and onto Comments Invited
shall not be construed to preclude a hot engine parts or brakes, which could We invite you to send any written
national bank from buying and selling lead to a major ground fire. relevant data, views, or arguments about
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![Federal Register / Vol. 81, No. 179 / Thursday, September 15, 2016 / Proposed Rules 63435
List of Subjects in 14 CFR Part 39 (h) Alternative Methods of Compliance Issued in Renton, Washington, on
(AMOCs) September 6, 2016.
Air transportation, Aircraft, Aviation
(1) The Manager, Seattle Aircraft Michael Kaszycki,
safety, Incorporation by reference,
Certification Office (ACO), FAA, has the Acting Manager, Transport Airplane
Safety.
authority to approve AMOCs for this AD, if Directorate, Aircraft Certification Service.
The Proposed Amendment requested using the procedures found in 14 [FR Doc. 2016–22101 Filed 9–14–16; 8:45 am]
CFR 39.19. In accordance with 14 CFR 39.19,
Accordingly, under the authority send your request to your principal inspector
BILLING CODE 4910–13–P
delegated to me by the Administrator, or local Flight Standards District Office, as
the FAA proposes to amend 14 CFR part appropriate. If sending information directly
39 as follows: to the manager of the ACO, send it to the FEDERAL TRADE COMMISSION
attention of the person identified in
PART 39—AIRWORTHINESS paragraph (i)(1) of this AD. Information may 16 CFR Part 682
DIRECTIVES be emailed to: 9-ANM-Seattle-ACO-AMOC-
RIN 3084–AB41
Requests@faa.gov.
■ 1. The authority citation for part 39 (2) Before using any approved AMOC,
continues to read as follows: Disposal of Consumer Report
notify your appropriate principal inspector,
or lacking a principal inspector, the manager
Information and Records
Authority: 49 U.S.C. 106(g), 40113, 44701.
of the local flight standards district office/ AGENCY: Federal Trade Commission.
§ 39.13 [Amended] certificate holding district office.
(3) An AMOC that provides an acceptable
ACTION: Request for public comment.
■ 2. The FAA amends § 39.13 by adding
the following new airworthiness level of safety may be used for any repair, SUMMARY: The Federal Trade
modification, or alteration required by this
directive (AD): Commission (‘‘FTC’’ or ‘‘The
AD if it is approved by the Boeing
The Boeing Company: Docket No. FAA– Commercial Airplanes Organization Commission) requests public comment
2016–9075; Directorate Identifier 2016– Designation Authorization (ODA) that has on its rule regarding Disposal of
NM–082–AD. been authorized by the Manager, Seattle Consumer Report Information and
(a) Comments Due Date ACO, to make those findings. To be Records (‘‘Disposal Rule’’ or ‘‘Rule’’).
We must receive comments by October 31, approved, the repair method, modification The Commission is soliciting comment
2016. deviation, or alteration deviation must meet as part of the FTC’s systematic review
the certification basis of the airplane, and the of all current Commission regulations
(b) Affected ADs approval must specifically refer to this AD. and guides.
None. (4) For service information that contains
DATES: Comments must be received on
steps that are labeled as Required for
(c) Applicability Compliance (RC), the provisions of or before November 21, 2016.
This AD applies to The Boeing Company paragraphs (h)(4)(i) and (h)(4)(ii) of this AD ADDRESSES: Interested parties may file a
Model 787–8 and 787–9 airplanes, apply. comment online or on paper by
certificated in any category, as identified in (i) The steps labeled as RC, including following the Instructions for
Boeing Alert Service Bulletin B787–81205– substeps under an RC step and any figures Submitting Comments part of the
SB570029–00, Issue 001, dated February 23, identified in an RC step, must be done to SUPPLEMENTARY INFORMATION section
2016. comply with the AD. If a step or sub-step is
below. Write ‘‘Disposal Rule, 16 CFR
(d) Subject labeled ‘‘RC Exempt,’’ then the RC
requirement is removed from that step or part 682, Project No. 165410’’ on your
Air Transport Association (ATA) of sub-step. An AMOC is required for any comment and file your comment online
America Code 57; Wings. deviations to RC steps, including substeps at https://ftcpublic.commentworks.com/
(e) Unsafe Condition and identified figures. ftc/disposalrule by following the
(ii) Steps not labeled as RC may be instructions on the web-based form. If
This AD was prompted by a report
indicating that a portion of the sealant above
deviated from using accepted methods in you prefer to file your comment on
the engine pylon between the wing skin and accordance with the operator’s maintenance paper, write ‘‘Disposal Rule, 16 CFR
the vapor barrier may have been omitted. We or inspection program without obtaining part 682, Project No. 165410’’ on your
are issuing this AD to detect and correct approval of an AMOC, provided the RC steps, comment and on the envelope and mail
missing sealant above the engine pylon including substeps and identified figures, can
your comment to the following address:
between the wing skin and the vapor barrier, still be done as specified, and the airplane
can be put back in an airworthy condition. Federal Trade Commission, Office of the
which can create an unintended leak path for Secretary, 600 Pennsylvania Avenue
fuel, potentially draining onto the aft fairing (i) Related Information NW., Suite CC–5610 (Annex H),
heat shield and onto hot engine parts or
brakes, which could lead to a major ground (1) For more information about this AD, Washington, DC 20580, or deliver your
fire. contact Sherry Vevea, Aerospace Engineer, comment to the following address:
Propulsion Branch, ANM–140S, FAA, Seattle Federal Trade Commission, Office of the
(f) Compliance Aircraft Certification Office (ACO), 1601 Lind Secretary, Constitution Center, 400 7th
Comply with this AD within the Avenue SW., Renton, WA 98057–3356;
Street SW., 5th Floor, Suite 5610
compliance times specified, unless already phone: 425 917 6514; fax: 425 917 6590;
email: sherry.vevea@faa.gov. (Annex H), Washington, DC 20024.
done.
(2) For service information identified in FOR FURTHER INFORMATION CONTACT:
(g) Inspection and Corrective Actions this AD, contact Boeing Commercial Tiffany George, Division of Privacy and
Within 60 months after the effective date Airplanes, Attention: Data & Services Identity Protection, Bureau of Consumer
rmajette on DSK2TPTVN1PROD with PROPOSALS
of this AD: Do a general visual inspection for Management, P. O. Box 3707, MC 2H–65, Protection, Federal Trade Commission,
missing sealant in the seam on the outside Seattle, WA 98124–2207; telephone 206– 600 Pennsylvania Avenue NW.,
and inside of the engine struts; and do all 544–5000, extension 1; fax 206–766–5680; Washington, DC 20580, (202) 326–3040.
applicable corrective actions; in accordance Internet https://www.myboeingfleet.com. You
with the Accomplishment Instructions of may view this referenced service information SUPPLEMENTARY INFORMATION:
Boeing Alert Service Bulletin B787–81205– at the FAA, Transport Airplane Directorate, I. Background
SB570029–00, Issue 001, dated February 23, 1601 Lind Avenue SW., Renton, WA. For
2016. Do all applicable corrective actions information on the availability of this The Fair and Accurate Credit
before further flight. material at the FAA, call 425–227–1221. Transactions Act (‘‘FACTA’’ or ‘‘Act’’)
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Document Created: 2018-02-09 13:18:09
Document Modified: 2018-02-09 13:18:09
| 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 October 31, 2016. | |
| Contact | Sherry Vevea, Aerospace Engineer, Propulsion Branch, ANM-140S, FAA, Seattle Aircraft Certification Office (ACO), 1601 Lind Avenue SW., Renton, WA 98057-3356; phone: 425-917- 6514; fax: 425-917-6590; email: [email protected] | |
| FR Citation | 81 FR 63433 | |
| RIN Number | 2120-AA64 | |
| CFR Associated | Air Transportation; Aircraft; Aviation Safety; Incorporation by Reference and Safety |
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