Airworthiness Directives; The Boeing Company Airplanes, 63433-63435 [2016-22101]

Download as PDF Federal Register / Vol. 81, No. 179 / Thursday, September 15, 2016 / Proposed Rules banking exceptions to the prohibition on buying and selling physical metal. For the reasons described above, the OCC has determined that the proposed rule would not result in expenditures by state, local, and Tribal governments, or by the private sector, of $100 million or more. Accordingly, the OCC has not prepared a written statement to accompany the proposed rule. physical metal to hedge a derivative for which that metal is the reference asset so long as the amount of the physical metal used for hedging purposes is nominal. ■ 3. Add § 7.1023 to subpart A to read as follows: List of subjects in 12 CFR Part 7 Banks, banking, Computer technology, Credit, Federal savings associations, Insurance, Investments, Metals, National banks, Reporting and recordkeeping requirements, Securities, Surety bonds. For the reasons set forth in the preamble, OCC proposes to amend 12 CFR part 7 as follows: (a) In this section, industrial or commercial metal means metal (including an alloy) in a physical form primarily suited to industrial or commercial use, for example, copper cathodes. (b) Federal savings associations may not deal or invest in industrial or commercial metal. Federal savings associations may not buy or sell industrial or commercial metal if the purchase or sale is impermissible for a national bank. PART 7—BANK ACTIVITIES AND OPERATIONS § 7.1023 Federal savings associations, prohibition on industrial or commercial metal dealing or investing. Dated: September 7, 2016 Thomas J. Curry, Comptroller of the Currency. 1. The authority citation for part 7 is amended to read as follows: ■ Authority: 12 U.S.C. 1 et seq., 25b, 71, 71a, 92, 92a, 93, 93a, 371, 371a, 481, 484, 1463, 1464, 1818, and 5412(b)(2)(B). 2. Add § 7.1022 to subpart A to read as follows: [FR Doc. 2016–22017 Filed 9–14–16; 8:45 am] BILLING CODE 4810–33–P ■ DEPARTMENT OF TRANSPORTATION rmajette on DSK2TPTVN1PROD with PROPOSALS § 7.1022 National bank authority to buy and sell exchange, coin, and bullion. Federal Aviation Administration (a) In this section, industrial or commercial metal means metal (including an alloy) in a physical form primarily suited to industrial or commercial use, for example, copper cathodes. (b) Scope of authorization. Section 24 (Seventh) of the National Bank Act authorizes national banks to buy and sell exchange, coin, and bullion. Industrial or commercial metal is not exchange, coin, and bullion within the meaning of this authorization. (c) Buying and selling metal as part of or incidental to the business of banking. Section 24 (Seventh) authorizes national banks to engage in activities that are part of, or incidental to, the business of banking. Buying and selling industrial or commercial metal for the purpose of dealing or investing in that metal is not part of or incidental to the business of banking pursuant to section 24 (Seventh). (d) Other authorities not affected. This section shall not be construed to preclude a national bank from acquiring or selling metal in connection with its incidental authority to foreclose on loan collateral, compromise doubtful claims, or avoid loss in connection with a debt previously contracted. This section also shall not be construed to preclude a national bank from buying and selling 14 CFR Part 39 VerDate Sep<11>2014 14:41 Sep 14, 2016 Jkt 238001 [Docket No. FAA–2016–9075; Directorate Identifier 2016–NM–082–AD] RIN 2120–AA64 Airworthiness Directives; The Boeing Company Airplanes Federal Aviation Administration (FAA), DOT. ACTION: Notice of proposed rulemaking (NPRM). AGENCY: 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. SUMMARY: PO 00000 Frm 00006 Fmt 4702 Sfmt 4702 63433 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 https://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 https:// www.regulations.gov by searching for and locating Docket No. FAA–2016– 9075. DATES: Examining the AD Docket You may examine the AD docket on the Internet at https:// www.regulations.gov by searching for and locating Docket No. FAA–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: sherry.vevea@faa.gov. SUPPLEMENTARY INFORMATION: Comments Invited We invite you to send any written relevant data, views, or arguments about E:\FR\FM\15SEP1.SGM 15SEP1 63434 Federal Register / Vol. 81, No. 179 / Thursday, September 15, 2016 / Proposed Rules 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 https:// 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 https:// 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 Action Labor cost Inspection ........................................................ 3 work-hours × $85 per hour = $255 ............. We estimate the following costs to do any necessary repairs that would be Cost per product Parts cost required based on the results of the proposed inspection. We have no way of $0 Cost on U.S. operators $255 $8,160 determining the number of aircraft that might need these repairs: ON-CONDITION COSTS Action Labor cost Repair .............................................. Up to 3 work-hours × $85 per hour = $255 .............................................. Cost per product Parts cost (1) (1 ) 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. rmajette on DSK2TPTVN1PROD with PROPOSALS 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: VerDate Sep<11>2014 14:41 Sep 14, 2016 Jkt 238001 ‘‘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 PO 00000 Frm 00007 Fmt 4702 Sfmt 4702 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. E:\FR\FM\15SEP1.SGM 15SEP1 Federal Register / Vol. 81, No. 179 / Thursday, September 15, 2016 / Proposed Rules 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 1. The authority citation for part 39 continues to read as follows: ■ Authority: 49 U.S.C. 106(g), 40113, 44701. § 39.13 [Amended] 2. The FAA amends § 39.13 by adding the following new airworthiness directive (AD): ■ 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. rmajette on DSK2TPTVN1PROD with PROPOSALS (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. VerDate Sep<11>2014 14:41 Sep 14, 2016 Jkt 238001 (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: 9-ANM-Seattle-ACO-AMOCRequests@faa.gov. (2) Before using any approved AMOC, notify your appropriate principal inspector, or lacking a principal inspector, the manager of the local flight standards district office/ certificate holding district office. (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: sherry.vevea@faa.gov. (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. PO 00000 Frm 00008 Fmt 4702 Sfmt 4702 63435 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 TRADE COMMISSION 16 CFR Part 682 RIN 3084–AB41 Disposal of Consumer Report Information and Records Federal Trade Commission. Request for public comment. AGENCY: ACTION: The Federal Trade Commission (‘‘FTC’’ or ‘‘The Commission) requests public comment on its rule regarding Disposal of Consumer Report Information and Records (‘‘Disposal Rule’’ or ‘‘Rule’’). The Commission is soliciting comment as part of the FTC’s systematic review of all current Commission regulations and guides. DATES: Comments must be received on or before November 21, 2016. ADDRESSES: Interested parties may file a comment online or on paper by following the Instructions for Submitting Comments part of the SUPPLEMENTARY INFORMATION section below. Write ‘‘Disposal Rule, 16 CFR part 682, Project No. 165410’’ on your comment and file your comment online at https://ftcpublic.commentworks.com/ ftc/disposalrule by following the instructions on the web-based form. If you prefer to file your comment on paper, write ‘‘Disposal Rule, 16 CFR part 682, Project No. 165410’’ on your comment and on the envelope and mail your comment to the following address: Federal Trade Commission, Office of the Secretary, 600 Pennsylvania Avenue NW., Suite CC–5610 (Annex H), Washington, DC 20580, or deliver your comment to the following address: Federal Trade Commission, Office of the Secretary, Constitution Center, 400 7th Street SW., 5th Floor, Suite 5610 (Annex H), Washington, DC 20024. FOR FURTHER INFORMATION CONTACT: Tiffany George, Division of Privacy and Identity Protection, Bureau of Consumer Protection, Federal Trade Commission, 600 Pennsylvania Avenue NW., Washington, DC 20580, (202) 326–3040. SUPPLEMENTARY INFORMATION: SUMMARY: I. Background The Fair and Accurate Credit Transactions Act (‘‘FACTA’’ or ‘‘Act’’) E:\FR\FM\15SEP1.SGM 15SEP1

Agencies

[Federal Register Volume 81, Number 179 (Thursday, September 15, 2016)]
[Proposed Rules]
[Pages 63433-63435]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[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 https://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 https://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 https://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: sherry.vevea@faa.gov.

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 https://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 https://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: 9-ANM-Seattle-ACO-AMOC-Requests@faa.gov.
    (2) Before using any approved AMOC, notify your appropriate 
principal inspector, or lacking a principal inspector, the manager 
of the local flight standards district office/certificate holding 
district office.
    (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: 
sherry.vevea@faa.gov.
    (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
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