81 FR 8823 - Airworthiness Directives; The Boeing Company Airplanes
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration Federal Register Volume 81, Issue 35 (February 23, 2016)
Federal Aviation Administration
Federal Register Volume 81, Issue 35 (February 23, 2016)
| Page Range | 8823-8825 | |
| FR Document | 2016-03562 |
[Federal Register Volume 81, Number 35 (Tuesday, February 23, 2016)] [Rules and Regulations] [Pages 8823-8825] From the Federal Register Online [www.thefederalregister.org] [FR Doc No: 2016-03562] ======================================================================= ----------------------------------------------------------------------- DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2016-3699; Directorate Identifier 2015-NM-109-AD; Amendment 39-18402; AD 2016-04-08] RIN 2120-AA64 Airworthiness Directives; The Boeing Company Airplanes AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Final rule; request for comments. ----------------------------------------------------------------------- SUMMARY: We are adopting a new airworthiness directive (AD) for certain The Boeing Company Model 787-8 airplanes. This AD requires revising the maintenance or inspection program, as applicable, to include an airworthiness limitation for repetitive inspections of the web fastener holes in the overwing flex-tees. This AD was prompted by a report that certain web fastener holes in the overwing flex-tees at the wing-to- body interface might not have been deburred properly when manufactured. Fastener holes without the deburr chamfer applied can develop fatigue cracking. We are issuing this AD to detect and correct cracking in the web fastener holes in the overwing flex-tees, which can weaken the primary wing structure so it cannot sustain limit load. DATES: This AD is effective March 9, 2016. The Director of the Federal Register approved the incorporation by reference of a certain publication listed in this AD as of March 9, 2016. We must receive comments on this AD by April 8, 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: U.S. Department of Transportation, Docket Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New Jersey Avenue SE., Washington, DC 20590, between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. For service information identified in this final rule, contact Boeing [[Page 8824]] 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-2016-3699. 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- 3699; 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 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: Melanie Violette, Senior Aerospace Engineer, Airframe Branch, ANM-120S, FAA, Seattle Aircraft Certification Office (ACO), 1601 Lind Avenue SW., Renton, WA 98057- 3356; phone: 425-917-6422; fax: 425-917-6590; email: [email protected]. Discussion We received a report that certain web fastener holes in the overwing flex-tees at the wing-to-body interface might not have been deburred properly when manufactured. A deburr chamfer should have been applied to the fastener holes in the overwing flex-tees. Fastener holes without the deburr chamfer applied can develop fatigue cracking before the required supplemental structural fatigue inspections are scheduled to begin. Such fatigue cracking, if not corrected, could result in the primary wing structure being weakened so it cannot sustain limit load. We are issuing this AD to correct the unsafe condition on these products. Related Service Information Under 1 CFR Part 51 We reviewed Boeing 787 Airworthiness Limitations--Line Number Specific, D011Z009-03-02, dated February 2015. The service information contains airworthiness limitation tasks pertaining to inspections for web fastener holes in the overwing flex-tees at the wing-to-body interface. 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 issuing 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. AD Requirements This AD requires revising the maintenance or inspection program, as applicable, to include an airworthiness limitation for repetitive inspection of the web fastener holes in the overwing flex-tees. This AD requires revisions to certain operator maintenance documents to include new actions (e.g., inspections). Compliance with these actions is required by 14 CFR 91.403(c). For airplanes that have been previously modified, altered, or repaired in the areas addressed by this AD, the operator may not be able to accomplish the actions described in the revisions. In this situation, to comply with 14 CFR 91.403(c), the operator must request approval for an alternative method of compliance according to paragraph (h) of this AD. The request should include a description of changes to the required actions that will ensure the continued operational safety of the airplane. FAA's Justification and Determination of the Effective Date There are no products of this type currently registered in the United States. However, this rule is necessary to ensure that the described unsafe condition is addressed if any of these products are placed on the U.S. Register in the future. Therefore, we find that notice and opportunity for prior public comment are unnecessary and that good cause exists for making this amendment effective in less than 30 days. Comments Invited This AD is a final rule that involves requirements affecting flight safety and was not preceded by notice and an opportunity for public comment. However, we invite you to send any written data, views, or arguments about this AD. Send your comments to an address listed under the ADDRESSES section. Include the docket number FAA-2016-3699 and Directorate Identifier 2015-NM-109-AD at the beginning of your comments. We specifically invite comments on the overall regulatory, economic, environmental, and energy aspects of this AD. We will consider all comments received by the closing date and may amend this 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 AD. Costs of Compliance We estimate that this AD affects 0 airplanes of U.S. registry. We estimate the following costs to comply with this AD: Estimated Costs ---------------------------------------------------------------------------------------------------------------- Cost per Cost on U.S. Action Labor cost Parts cost product operators ---------------------------------------------------------------------------------------------------------------- Maintenance/inspection program 1 work-hour x $85 per $0 $85 $0 revision. hour = $85. ---------------------------------------------------------------------------------------------------------------- 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 [[Page 8825]] 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 This AD will not have federalism implications under Executive Order 13132. This AD will not have a substantial direct effect on the States, on the relationship between the national government and the States, or on the distribution of power and responsibilities among the various levels of government. For the reasons discussed above, I certify that this AD: (1) Is not a ``significant regulatory action'' under Executive Order 12866, (2) Is not a ``significant rule'' under DOT Regulatory Policies and Procedures (44 FR 11034, February 26, 1979), (3) Will not affect intrastate aviation in Alaska, and (4) Will not have a significant economic impact, positive or negative, on a substantial number of small entities under the criteria of the Regulatory Flexibility Act. List of Subjects in 14 CFR Part 39 Air transportation, Aircraft, Aviation safety, Incorporation by reference, Safety. Adoption of the Amendment Accordingly, under the authority delegated to me by the Administrator, the FAA amends 14 CFR part 39 as follows: PART 39--AIRWORTHINESS DIRECTIVES 0 1. The authority citation for part 39 continues to read as follows: Authority: 49 U.S.C. 106(g), 40113, 44701. Sec. 39.13 [Amended] 0 2. The FAA amends Sec. 39.13 by adding the following new airworthiness directive (AD): 2016-04-08 The Boeing Company: Amendment 39-18402; Docket No. FAA- 2016-3699; Directorate Identifier 2015-NM-109-AD. (a) Effective Date This AD is effective March 9, 2016. (b) Affected ADs None. (c) Applicability The Boeing Company Model 787-8 airplanes, certificated in any category, having line numbers 78 and 82. (d) Subject Air Transport Association (ATA) of America Code 57, Wings. (e) Unsafe Condition This AD was prompted by a report that certain web fastener holes in the overwing flex-tees at the wing-to-body interface might not have been deburred properly when manufactured. We are issuing this AD to detect and correct cracking in the web fastener holes in the overwing flex-tees, which can weaken the primary wing structure so it cannot sustain limit load. (f) Compliance Comply with this AD within the compliance times specified, unless already done. (g) Revision to Maintenance or Inspection Program Within 30 days after the effective date of this AD, revise the maintenance or inspection program, as applicable, to incorporate the applicable inspection requirement identified in paragraphs (g)(1) and (g)(2) of this AD, as specified in Boeing 787 Airworthiness Limitations--Line Number Specific, D011Z009-03-02, dated February 2015. The initial compliance time for the tasks is at the applicable time specified in Boeing 787 Airworthiness Limitations--Line Number Specific, D011Z009-03-02, dated February 2015. (1) For the airplane having line number 78: Principal Structural Element 57-10-06a_MRB9, ``Overwing Flex-Tee--Web Fastener Holes.'' (2) For the airplane having line number 82: Principal Structural Element 57-10-06a_MRB10, ``Overwing Flex-Tee--Web Fastener Holes.'' (h) Alternative Methods of Compliance (AMOCs) (1) The Manager, Settle 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) 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. (i) Related Information For more information about this AD, contact Melanie Violette, Senior Aerospace Engineer, Airframe Branch, ANM-120S, FAA, Seattle ACO, 1601 Lind Avenue SW., Renton, WA 98057-3356; phone: 425-917- 6422; fax: 425-917-6590; email: [email protected]. (j) Material Incorporated by Reference (1) The Director of the Federal Register approved the incorporation by reference (IBR) of the service information listed in this paragraph under 5 U.S.C. 552(a) and 1 CFR part 51. (2) You must use this service information as applicable to do the actions required by this AD, unless the AD specifies otherwise. (i) Boeing 787 Airworthiness Limitations--Line Number Specific, D011Z009-03-02, dated February 2015. (ii) Reserved. (3) 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. (4) You may view this service information at 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. (5) You may view this service information that is incorporated by reference at the National Archives and Records Administration (NARA). For information on the availability of this material at NARA, call 202-741-6030, or go to: http://www.archives.gov/federal-register/cfr/ibr-locations.html. Issued in Renton, Washington, on February 10, 2016. Michael Kaszycki, Acting Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. 2016-03562 Filed 2-22-16; 8:45 am] BILLING CODE 4910-13-P
![Federal Register / Vol. 81, No. 35 / Tuesday, February 23, 2016 / Rules and Regulations 8823
Promotion and Economics Division, been estimated that there are DEPARTMENT OF TRANSPORTATION
Specialty Crops Program, AMS, USDA, approximately 170 domestic
1400 Independence Avenue SW., Room manufacturers and 70 importers who Federal Aviation Administration
1406–S, Stop 0244, Washington, DC will be eligible to vote in the
20250–0244, telephone: (202) 720–9915; referendum. It will take an average of 15 14 CFR Part 39
facsimile: (202) 205–2800; or contact minutes for each voter to read the voting [Docket No. FAA–2016–3699; Directorate
Maureen Pello at (503) 632–8848 or via instructions and complete the Identifier 2015–NM–109–AD; Amendment
electronic mail: Maureen.Pello@ referendum ballot. 39–18402; AD 2016–04–08]
ams.usda.gov.
Referendum Order RIN 2120–AA64
FOR FURTHER INFORMATION CONTACT:
Maureen Pello, Marketing Specialist, Maureen Pello, Marketing Specialist, Airworthiness Directives; The Boeing
PED, SC, AMS, USDA, 1400 and Heather Pichelman, Director, PED, Company Airplanes
Independence Avenue SW., Room SC, AMS, USDA, Stop 0244, Room
1406–S, Stop 0244, Washington, DC AGENCY: Federal Aviation
1406–S, 1400 Independence Avenue Administration (FAA), DOT.
20250–0244; telephone: (202) 720–9915, SW., Washington, DC 20250–0244, are
(503) 632–8848 (direct line); facsimile: ACTION: Final rule; request for
designated as the referendum agents to comments.
(202) 205–2800; or electronic mail:
conduct this referendum. The
Maureen.Pello@ams.usda.gov.
referendum procedures at 7 CFR SUMMARY: We are adopting a new
SUPPLEMENTARY INFORMATION: Pursuant
1217.100 through 1217.108, which were airworthiness directive (AD) for certain
to the Commodity Promotion, Research The Boeing Company Model 787–8
issued pursuant to the Act, shall be used
and Information Act of 1996 (7 U.S.C. airplanes. This AD requires revising the
to conduct the referendum.
7411–7425) (Act), it is hereby directed maintenance or inspection program, as
that a referendum be conducted to The referendum agent will mail the
applicable, to include an airworthiness
ascertain whether continuance of the ballots to be cast in the referendum and
limitation for repetitive inspections of
Order (7 CFR part 1217) is favored by voting instructions to all known, eligible
the web fastener holes in the overwing
eligible domestic manufacturers and domestic manufacturers and importers
flex-tees. This AD was prompted by a
importers of softwood lumber. The prior to the first day of the voting report that certain web fastener holes in
Order is authorized under the Act. period. Persons who domestically the overwing flex-tees at the wing-to-
The representative period for manufactured and shipped or imported body interface might not have been
establishing voter eligibility for the 15 million board feet or more of deburred properly when manufactured.
referendum shall be the period from softwood lumber during the Fastener holes without the deburr
January 1 through December 31, 2015. representative period, paid assessments chamfer applied can develop fatigue
Persons who domestically manufactured during that period, and are currently cracking. We are issuing this AD to
and shipped or imported 15 million softwood lumber domestic detect and correct cracking in the web
board feet or more of softwood lumber manufacturers or importers subject to fastener holes in the overwing flex-tees,
during the representative period, paid
assessment under the Order are eligible which can weaken the primary wing
assessments during that period, and are
to vote. Persons who received an structure so it cannot sustain limit load.
currently softwood lumber
exemption from assessments during the DATES: This AD is effective March 9,
manufacturers or importers subject to
assessment under the Order are eligible entire representative period are 2016.
to vote. Persons who received an ineligible to vote. Any eligible domestic The Director of the Federal Register
exemption from assessments for the manufacturer or importer who does not approved the incorporation by reference
entire representative period are receive a ballot should contact the of a certain publication listed in this AD
ineligible to vote. The referendum will referendum agent no later than one as of March 9, 2016.
be conducted by mail ballot from week before the end of the voting We must receive comments on this
August 1 through 25, 2016. period. Ballots must be received by the AD by April 8, 2016.
Section 518 of the Act authorizes referendum agent by 4:30 p.m. Eastern ADDRESSES: You may send comments,
continuance referenda. Under time, August 25, 2016, in order to be using the procedures found in 14 CFR
§ 1217.81(b) of the Order, the U.S. counted. 11.43 and 11.45, by any of the following
Department of Agriculture (USDA) must methods:
conduct a referendum 5 years after the List of Subjects in 7 CFR Part 1217 • Federal eRulemaking Portal: Go to
program has been in effect to determine Administrative practice and http://www.regulations.gov. Follow the
whether persons subject to assessment procedure, Advertising, Consumer instructions for submitting comments.
favor continuance of the Order. The • Fax: 202–493–2251.
information, Marketing agreements,
program became effective in 2011. • Mail: U.S. Department of
Promotion, Reporting and
USDA would continue the Order if Transportation, Docket Operations,
recordkeeping requirements, Softwood M–30, West Building Ground Floor,
continuance is favored by a majority of
lumber. Room W12–140, 1200 New Jersey
the domestic manufacturers and
importers voting in the referendum, Authority: 7 U.S.C. 7411–7425; 7 U.S.C. Avenue SE., Washington, DC 20590.
who also represent a majority of the 7401. • Hand Delivery: U.S. Department of
asabaliauskas on DSK5VPTVN1PROD with RULES
volume of softwood lumber represented Dated: February 18, 2016. Transportation, Docket Operations,
in the referendum. M–30, West Building Ground Floor,
Elanor Starmer,
In accordance with the Paperwork Room W12–140, 1200 New Jersey
Reduction Act of 1995 (44 U.S.C. Acting Administrator, Agricultural Marketing Avenue SE., Washington, DC 20590,
chapter 35), the referendum ballot has Service. between 9 a.m. and 5 p.m., Monday
been approved by the Office of [FR Doc. 2016–03805 Filed 2–22–16; 8:45 am] through Friday, except Federal holidays.
Management and Budget (OMB) and BILLING CODE 3410–02–P For service information identified in
assigned OMB No. 0581–0093. It has this final rule, contact Boeing
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![Federal Register / Vol. 81, No. 35 / Tuesday, February 23, 2016 / Rules and Regulations 8825
is within the scope of that authority (e) Unsafe Condition Engineer, Airframe Branch, ANM–120S,
because it addresses an unsafe condition This AD was prompted by a report that FAA, Seattle ACO, 1601 Lind Avenue SW.,
that is likely to exist or develop on certain web fastener holes in the overwing Renton, WA 98057–3356; phone: 425–917–
flex-tees at the wing-to-body interface might 6422; fax: 425–917–6590; email:
products identified in this rulemaking
not have been deburred properly when Melanie.Violette@faa.gov.
action.
manufactured. We are issuing this AD to (j) Material Incorporated by Reference
Regulatory Findings detect and correct cracking in the web
fastener holes in the overwing flex-tees, (1) The Director of the Federal Register
This AD will not have federalism approved the incorporation by reference
which can weaken the primary wing
implications under Executive Order (IBR) of the service information listed in this
structure so it cannot sustain limit load.
13132. This AD will not have a paragraph under 5 U.S.C. 552(a) and 1 CFR
substantial direct effect on the States, on (f) Compliance part 51.
the relationship between the national Comply with this AD within the (2) You must use this service information
government and the States, or on the compliance times specified, unless already as applicable to do the actions required by
done. this AD, unless the AD specifies otherwise.
distribution of power and (i) Boeing 787 Airworthiness Limitations—
responsibilities among the various (g) Revision to Maintenance or Inspection Line Number Specific, D011Z009–03–02,
levels of government. Program dated February 2015.
For the reasons discussed above, I (ii) Reserved.
Within 30 days after the effective date of
certify that this AD: this AD, revise the maintenance or inspection (3) For service information identified in
(1) Is not a ‘‘significant regulatory program, as applicable, to incorporate the this AD, contact Boeing Commercial
action’’ under Executive Order 12866, applicable inspection requirement identified Airplanes, Attention: Data & Services
(2) Is not a ‘‘significant rule’’ under in paragraphs (g)(1) and (g)(2) of this AD, as Management, P.O. Box 3707, MC 2H–65,
DOT Regulatory Policies and Procedures specified in Boeing 787 Airworthiness Seattle, WA 98124–2207; telephone 206–
(44 FR 11034, February 26, 1979), Limitations—Line Number Specific, 544–5000, extension 1; fax 206–766–5680;
(3) Will not affect intrastate aviation D011Z009–03–02, dated February 2015. The Internet https://www.myboeingfleet.com.
in Alaska, and initial compliance time for the tasks is at the (4) You may view this service information
(4) Will not have a significant applicable time specified in Boeing 787 at FAA, Transport Airplane Directorate, 1601
Airworthiness Limitations—Line Number Lind Avenue SW., Renton, WA. For
economic impact, positive or negative, information on the availability of this
on a substantial number of small entities Specific, D011Z009–03–02, dated February
2015. material at the FAA, call 425–227–1221.
under the criteria of the Regulatory (5) You may view this service information
(1) For the airplane having line number 78:
Flexibility Act. Principal Structural Element 57–10–06a_ that is incorporated by reference at the
MRB9, ‘‘Overwing Flex-Tee—Web Fastener National Archives and Records
List of Subjects in 14 CFR Part 39 Administration (NARA). For information on
Holes.’’
Air transportation, Aircraft, Aviation (2) For the airplane having line number 82: the availability of this material at NARA, call
safety, Incorporation by reference, Principal Structural Element 57–10–06a_ 202–741–6030, or go to: http://
Safety. MRB10, ‘‘Overwing Flex-Tee—Web Fastener www.archives.gov/federal-register/cfr/ibr-
Holes.’’ locations.html.
Adoption of the Amendment
(h) Alternative Methods of Compliance Issued in Renton, Washington, on February
Accordingly, under the authority 10, 2016.
(AMOCs)
delegated to me by the Administrator, Michael Kaszycki,
the FAA amends 14 CFR part 39 as (1) The Manager, Settle Aircraft
Certification Office (ACO), FAA, has the Acting Manager, Transport Airplane
follows: Directorate, Aircraft Certification Service.
authority to approve AMOCs for this AD, if
requested using the procedures found in 14 [FR Doc. 2016–03562 Filed 2–22–16; 8:45 am]
PART 39—AIRWORTHINESS
CFR 39.19. In accordance with 14 CFR 39.19, BILLING CODE 4910–13–P
DIRECTIVES send your request to your principal inspector
or local Flight Standards District Office, as
■ 1. The authority citation for part 39
appropriate. If sending information directly
continues to read as follows: to the manager of the ACO, send it to the DEPARTMENT OF COMMERCE
Authority: 49 U.S.C. 106(g), 40113, 44701. attention of the person identified in
paragraph (i) of this AD. Information may be Bureau of Industry and Security
§ 39.13 [Amended] emailed to: 9-ANM-Seattle-ACO-AMOC-
■ 2. The FAA amends § 39.13 by adding Requests@faa.gov. 15 CFR Part 744
the following new airworthiness (2) Before using any approved AMOC, [Docket No. 151209999–5999–01]
directive (AD): notify your appropriate principal inspector,
or lacking a principal inspector, the manager RIN 0694—AG81
2016–04–08 The Boeing Company: of the local flight standards district office/
Amendment 39–18402; Docket No. certificate holding district office. Addition of Certain Persons and
FAA–2016–3699; Directorate Identifier (3) An AMOC that provides an acceptable
2015–NM–109–AD.
Modification of Certain Entries to the
level of safety may be used for any repair, Entity List; and Removal of Certain
(a) Effective Date modification, or alteration required by this Persons From the Entity List
This AD is effective March 9, 2016. AD if it is approved by the Boeing
Commercial Airplanes Organization AGENCY: Bureau of Industry and
(b) Affected ADs Designation Authorization (ODA) that has Security, Commerce.
None. been authorized by the Manager, Seattle ACTION: Final rule.
asabaliauskas on DSK5VPTVN1PROD with RULES
ACO, to make those findings. To be
(c) Applicability approved, the repair method, modification SUMMARY: This rule amends the Export
The Boeing Company Model 787–8 deviation, or alteration deviation must meet Administration Regulations (EAR) by
airplanes, certificated in any category, having the certification basis of the airplane, and the
adding eight persons under eight entries
line numbers 78 and 82. approval must specifically refer to this AD.
to the Entity List. The eight persons who
(d) Subject (i) Related Information are added to the Entity List have been
Air Transport Association (ATA) of For more information about this AD, determined by the U.S. Government to
America Code 57, Wings. contact Melanie Violette, Senior Aerospace be acting contrary to the national
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Document Created: 2018-02-02 14:33:04
Document Modified: 2018-02-02 14:33:04
| 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 | Rules and Regulations | |
| Action | Final rule; request for comments. | |
| Dates | This AD is effective March 9, 2016. | |
| Contact | Melanie Violette, Senior Aerospace Engineer, Airframe Branch, ANM-120S, FAA, Seattle Aircraft Certification Office (ACO), 1601 Lind Avenue SW., Renton, WA 98057- 3356; phone: 425-917-6422; fax: 425-917-6590; email: [email protected] | |
| FR Citation | 81 FR 8823 | |
| RIN Number | 2120-AA64 | |
| CFR Associated | Air Transportation; Aircraft; Aviation Safety; Incorporation by Reference and Safety |
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