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and Airworthiness Division, but during (d) Subject Transport Standards Branch, FAA; or the this transition period, the Executive Air Transport Association (ATA) of European Aviation Safety Agency (EASA); or Director has delegated the authority to America Code 54, Nacelles/pylons. Saab AB, Saab Aeronautics’ EASA Design issue ADs applicable to transport Organization Approval (DOA). If approved by (e) Reason category airplanes and associated the DOA, the approval must include the DOA-authorized signature. appliances to the Director of the System This AD was prompted by reports of loose Oversight Division. and irregular fasteners at the forward end of (j) Related Information the nacelle upper longeron, where the Regulatory Findings bulkhead frame and struts are attached to the (1) Refer to Mandatory Continuing engine mounting structure (EMS). The FAA Airworthiness Information (MCAI) EASA AD The FAA determined that this is issuing this AD to address loose and 2019–0054, dated March 18, 2019, for related proposed AD would not have federalism irregular fasteners of the EMS which could information. This MCAI may be found in the implications under Executive Order cause development of cracks in the EMS, AD docket on the internet at http:// 13132. This proposed AD would not leading to failure of the affected engine www.regulations.gov by searching for and have a substantial direct effect on the mount-to-airplane structural connection, locating Docket No. FAA–2019–0520. States, on the relationship between the possibly resulting in significant airframe (2) For more information about this AD, vibrations and detrimental effects on the contact Shahram Daneshmandi, national Government and the States, or Engineer, International Section, Transport on the distribution of power and surrounding pylon/nacelle structure, and loss of structural integrity. Standards Branch, FAA, 2200 South 216th responsibilities among the various St., Des Moines, WA 98198; phone and fax: levels of government. (f) Compliance 206–231–3220. For the reasons discussed above, I Comply with this AD within the (3) For service information identified in certify this proposed regulation: compliance times specified, unless already this AD, contact Saab AB, Saab Aeronautics, (1) Is not a ‘‘significant regulatory done. SE–581 88, Linko¨ping, Sweden; phone: +46 action’’ under Executive Order 12866; 13 18 5591; fax: +46 13 18 4874; email: (2) Will not affect intrastate aviation (g) Modification of the EMS [email protected]; in Alaska; and Within 3,000 flight hours or 24 months, internet: http://www.saabgroup.com. You (3) Will not have a significant whichever occurs first after the effective date may view this service information at the economic impact, positive or negative, of this AD, modify the EMS and structural FAA, Transport Standards Branch, 2200 on a substantial number of small entities attachments, in accordance with the South 216th St., Des Moines, WA. For under the criteria of the Regulatory Accomplishment Instructions of Saab Service information on the availability of this material at the FAA, call 206–231–3195. Flexibility Act. Bulletin 2000–54–036, Revision 02, dated January 18, 2019. Where Saab Service Issued in Des Moines, Washington, on June List of Subjects in 14 CFR Part 39 Bulletin 2000–54–036, Revision 02, dated 21, 2019. January 18, 2019, specifies to contact Saab for Air transportation, Aircraft, Aviation appropriate action: Before further flight, Dionne Palermo, safety, Incorporation by reference, accomplish corrective actions in accordance Acting Director, System Oversight Division, Safety. with the procedures specified in paragraph Aircraft Certification Service. The Proposed Amendment (i)(2) of this AD. [FR Doc. 2019–13889 Filed 7–1–19; 8:45 am] BILLING CODE 4910–13–P Accordingly, under the authority (h) Credit for Previous Actions delegated to me by the Administrator, This paragraph provides credit for actions the FAA proposes to amend 14 CFR part required by paragraph (g) of this AD, if those DEPARTMENT OF TRANSPORTATION 39 as follows: actions were performed before the effective date of this AD using Saab Service Bulletin Federal Aviation Administration PART 39—AIRWORTHINESS 2000–54–036, dated November 6, 2018; or DIRECTIVES Saab Service Bulletin 2000–54–036, Revision 01, dated January 7, 2019. 14 CFR Part 39 ■ 1. The authority citation for part 39 (i) Other FAA AD Provisions [Docket No. FAA–2019–0442; Product Identifier 2018–NM–171–AD] continues to read as follows: The following provisions also apply to this Authority: 49 U.S.C. 106(g), 40113, 44701. AD: RIN 2120–AA64 (1) Alternative Methods of Compliance § 39.13 [Amended] (AMOCs): The Manager, International Airworthiness Directives; The ■ 2. The FAA amends § 39.13 by adding Section, Transport Standards Branch, FAA, Company Airplanes the following new airworthiness has the authority to approve AMOCs for this directive (AD): AD, if requested using the procedures found AGENCY: Federal Aviation in 14 CFR 39.19. In accordance with 14 CFR Administration (FAA), DOT. Saab AB, Saab Aeronautics (Formerly 39.19, send your request to your principal Known as Saab AB, Saab Aerosystems): inspector or local Flight Standards District ACTION: Notice of proposed rulemaking Docket No. FAA–2019–0520; Product Office, as appropriate. If sending information (NPRM). Identifier 2019–NM–046–AD. directly to the International Section, send it SUMMARY: (a) Comments Due Date to the attention of the person identified in The FAA proposes to paragraph (j)(2) of this AD. Information may supersede Airworthiness Directive (AD) We must receive comments by August 16, 2017–15–04, which applies to certain 2019. be emailed to: 9-ANM-116-AMOC- [email protected]. Before using any The Boeing Company Model 787–8 and (b) Affected ADs approved AMOC, notify your appropriate 787–9 airplanes. AD 2017–15–04 None. principal inspector, or lacking a principal requires replacement of affected inspector, the manager of the local flight (c) Applicability electromechanical actuators (EMAs). standards district office/certificate holding Since AD 2017–15–04 was issued, the district office. This AD applies to Saab AB, Saab FAA has determined that discrepant Aeronautics (formerly known as Saab AB, (2) Contacting the Manufacturer: For any Saab Aerosystems) Model requirement in this AD to obtain corrective EMAs may have been installed on airplanes, certificated in any category, all actions from a manufacturer, the action must airplanes outside the original serial numbers, except serial numbers 006, be accomplished using a method approved applicability of AD 2017–15–04. This 043, 056, and 061. by the Manager, International Section, proposed AD would retain the

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requirements of AD 2017–15–04, fax: 206–231–3548; email: Related Service Information Under 1 expand the applicability to include all [email protected]. CFR Part 51 The Boeing Company Model 787 series SUPPLEMENTARY INFORMATION: The FAA reviewed Boeing Service airplanes, and add a new requirement to Bulletin B787–81205–SB270030–00, Comments Invited identify, for certain airplanes, the part Issue 002, dated April 7, 2017. The number of EMAs and replace affected service information describes EMAs. The FAA is proposing this AD to The FAA invites you to send any written relevant data, views, or procedures for replacing affected EMAs address the unsafe condition on these with new EMAs. products. arguments about this proposed AD. Send your comments to an address This proposed AD would also require DATES: The FAA must receive comments listed under the ADDRESSES section. Boeing Service Bulletin B787–81205– on this proposed AD by August 16, Include ‘‘Docket No. FAA–2019–0442; SB270030–00, Issue 001, dated October 2019. Product Identifier 2018–NM–171–AD’’ 22, 2015, which the Director of the Federal Register approved for ADDRESSES: You may send comments, at the beginning of your comments. The using the procedures found in 14 CFR FAA specifically invites comments on incorporation by reference as of August 11.43 and 11.45, by any of the following the overall regulatory, economic, 25, 2017 (82 FR 33785, July 21, 2017). methods: environmental, and energy aspects of These documents are distinct since they apply to different airplanes. This • Federal eRulemaking Portal: Go to this NPRM. The agency will consider all service information is reasonably http://www.regulations.gov. Follow the comments received by the closing date available because the interested parties instructions for submitting comments. and may amend this NPRM because of have access to it through their normal • Fax: 202–493–2251. those comments. course of business or by the means • Mail: U.S. Department of The FAA will post all comments, identified in the ADDRESSES section. Transportation, Docket Operations, M– without change, to http:// 30, West Building Ground Floor, Room www.regulations.gov, including any FAA’s Determination personal information you provide. The W12–140, 1200 New Jersey Avenue SE, The FAA is proposing this AD FAA will also post a report Washington, DC 20590. because the agency has evaluated all the • summarizing each substantive verbal Hand Delivery: Deliver to Mail relevant information and determined contact the agency receives about this address above between 9 a.m. and 5 the unsafe condition described proposed AD. p.m., Monday through Friday, except previously is likely to exist or develop Federal holidays. Discussion in other products of the same type For service information identified in design. this NPRM, contact Boeing Commercial The FAA issued AD 2017–15–04, Airplanes, Attention: Contractual & Data Amendment 39–18964 (82 FR 33785, Proposed AD Requirements Services (C&DS), 2600 Westminster July 21, 2017) (‘‘AD 2017–15–04’’), for This proposed AD would retain all of Blvd., MC 110–SK57, Seal Beach, CA certain The Boeing Company Model the requirements of AD 2017–15–04, 90740–5600; telephone 562–797–1717; 787–8 and 787–9 airplanes. AD 2017– and expand the applicability to include internet https:// 15–04 requires replacement of affected all The Boeing Company Model 787 www.myboeingfleet.com. You may view EMAs. AD 2017–15–04 resulted from a series airplanes. This proposed AD this service information at the FAA, report of wire harness chafing on the would also require an inspection or Transport Standards Branch, 2200 EMAs for certain spoilers due to records check to identify the part South 216th St., Des Moines, WA. For insufficient separation with adjacent number of the EMA, and for airplanes information on the availability of this structure. The FAA issued AD 2017–15– with affected EMAs, accomplishing the material at the FAA, call 206–231–3195. 04 to address chafing and consequent actions specified in the service It is also available on the internet at wire damage that could result in a information described previously, http://www.regulations.gov by searching potential source of ignition in the except as discussed under ‘‘Differences for and locating Docket No. FAA–2019– flammable leakage zone—an area of the Between this Proposed AD and the 0442. airplane where flammable fluids have Service Information.’’ the potential to accumulate—and a Examining the AD Docket For information on the procedures consequent fire or explosion. and compliance times, see this service You may examine the AD docket on information at http:// the internet at http:// Actions Since AD 2017–15–04 Was Issued www.regulations.gov by searching for www.regulations.gov by searching for and locating Docket No. FAA–2019– and locating Docket No. FAA–2019– Since the FAA issued AD 2017–15– 0442. 0442; or in person at Docket Operations 04, the agency has determined that, between 9 a.m. and 5 p.m., Monday because the affected EMAs are rotable Differences Between This Proposed AD through Friday, except Federal holidays. parts, these affected EMAs could be and the Service Information The AD docket contains this NPRM, the installed on airplanes that did not fall The effectivity of Boeing Service regulatory evaluation, any comments within the applicability of AD 2017–15– Bulletin B787–81205–SB270030–00, received, and other information. The 04, thereby subjecting those airplanes to Issue 002, dated April 7, 2017, is limited street address for Docket Operations is the unsafe condition. In addition, to certain The Boeing Company Model listed above. Comments will be Boeing issued Boeing Service Bulletin 787–8 and 787–9 airplanes. However, available in the AD docket shortly after B787–81205–SB270030–00, Issue 002, the applicability of this proposed AD receipt. dated April 7, 2017, which removes two includes all The Boeing Company FOR FURTHER INFORMATION CONTACT: airplanes from the effectivity, includes Model 787 series airplanes. Because the Douglas Tsuji, Aerospace Engineer, minor editorial changes, and does not affected EMAs are rotable parts, the Systems and Equipment Section, FAA, require additional work for airplanes on FAA has determined that these parts Seattle ACO Branch, 2200 South 216th which the actions required by AD 2017– could be installed on airplanes that St., Des Moines, WA 98198; phone and 15–04 were accomplished. were initially delivered with acceptable

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EMAs, thereby subjecting those Costs of Compliance registry. The agency estimates the airplanes to the unsafe condition. The FAA estimates that this proposed following costs to comply with this AD would affect 93 airplanes of U.S. proposed AD:

ESTIMATED COSTS FOR REQUIRED ACTIONS

Cost on U.S. opera- Action Labor cost Parts cost Cost per product tors

EMA replacement (retained actions from 32 work-hours × $85 per hour = $2,720 * $2,720 * ...... Up to $252,960 * AD 2017-15-04). per EMA replacement. Inspection/records check ...... 1 work-hour × $85 per hour = $85 ...... $0 $85 per inspection $7,905 cycle. * Parts cost is not included in the service information, but Boeing has indicated that existing parts can be modified to become the new parts.

Authority for This Rulemaking (1) Is not a ‘‘significant regulatory (e) Unsafe Condition action’’ under Executive Order 12866, Title 49 of the United States Code This AD was prompted by wire harness specifies the FAA’s authority to issue (2) Will not affect intrastate aviation chafing on the electro-mechanical actuators (EMAs) for certain spoilers due to rules on aviation safety. Subtitle I, in Alaska, and (3) Will not have a significant insufficient separation with adjacent Section 106, describes the authority of structure. The FAA is issuing this AD to the FAA Administrator. Subtitle VII, economic impact, positive or negative, on a substantial number of small entities address chafing and consequent wire damage Aviation Programs, describes in more that could result in a potential source of detail the scope of the Agency’s under the criteria of the Regulatory ignition in the flammable leakage zone and authority. Flexibility Act. a consequent fire or explosion. The FAA is issuing this rulemaking List of Subjects in 14 CFR Part 39 (f) Compliance under the authority described in Air transportation, Aircraft, Aviation Comply with this AD within the Subtitle VII, Part A, Subpart III, Section safety, Incorporation by reference, compliance times specified, unless already 44701, ‘‘General requirements.’’ Under Safety. done. that section, Congress charges the FAA with promoting safe flight of civil The Proposed Amendment (g) Retained EMA Replacement, With aircraft in air commerce by prescribing Revised Compliance Language Accordingly, under the authority This paragraph restates the requirements of regulations for practices, methods, and delegated to me by the Administrator, procedures the Administrator finds paragraph (g) of AD 2017–15–04 with revised the FAA proposes to amend 14 CFR part compliance language. For airplanes necessary for safety in air commerce. 39 as follows: This regulation is within the scope of identified in Boeing Service Bulletin B787– 81205–SB270030–00, Issue 001, dated that authority because it addresses an PART 39—AIRWORTHINESS October 22, 2015: Within 40 months after unsafe condition that is likely to exist or DIRECTIVES August 25, 2017 (the effective date of AD develop on products identified in this 2017–15–04), replace the EMAs with new rulemaking action. ■ 1. The authority citation for part 39 EMAs, in accordance with the This proposed AD is issued in continues to read as follows: Accomplishment Instructions of Boeing Service Bulletin B787–81205–SB270030–00, accordance with authority delegated by Authority: 49 U.S.C. 106(g), 40113, 44701. the Executive Director, Aircraft Issue 001, dated October 22, 2015; or Boeing Certification Service, as authorized by § 39.13 [Amended] Service Bulletin B787–81205–SB270030–00, Issue 002, dated April 7, 2017. FAA Order 8000.51C. In accordance ■ 2. The FAA amends § 39.13 by with that order, issuance of ADs is removing Airworthiness Directive (AD) (h) New Definition normally a function of the Compliance 2017–15–04, Amendment 39–18964 (82 For the purpose of this AD, an ‘‘affected and Airworthiness Division, but during FR 33785, July 21, 2017), and adding the part’’ is an EMA for spoiler 4, 5, 10, or 11 this transition period, the Executive following new AD: having part number C99144–004 or C99144– Director has delegated the authority to 005. The Boeing Company: Docket No. FAA– issue ADs applicable to transport 2019–0442; Product Identifier 2018– (i) New EMA Identification and Replacement category airplanes and associated NM–171–AD. appliances to the Director of the System For airplanes not identified in paragraph (a) Comments Due Date (g) of this AD with an original airworthiness Oversight Division. certificate or an original export certificate of The FAA must receive comments on this airworthiness dated before or on the effective Regulatory Findings AD action by August 16, 2019. date of this AD, do the actions specified in The FAA has determined that this (b) Affected ADs paragraphs (i)(1) and (i)(2) of this AD. proposed AD would not have federalism This AD replaces AD 2017–15–04, (1) Within 40 months after the effective implications under Executive Order Amendment 39–18964 (82 FR 33785, July 21, date of this AD, perform a general visual 13132. This proposed AD would not 2017) (‘‘AD 2017–15–04’’). inspection of the EMAs for spoilers 4, 5, 10, have a substantial direct effect on the and 11 to determine the part number. A States, on the relationship between the (c) Applicability review of airplane maintenance records is national Government and the States, or This AD applies to all The Boeing acceptable in lieu of this inspection if the part number of the EMA can be conclusively on the distribution of power and Company Model 787 series airplanes, certificated in any category. determined from that review. responsibilities among the various (2) If the EMA is an affected part: Within levels of government. (d) Subject 40 months after the effective date of this AD, For the reasons discussed above, I Air Transport Association (ATA) of replace the EMA in accordance with the certify that the proposed regulation: America Code 27, Flight Controls. Accomplishment Instructions of Boeing

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Service Bulletin B787–81205–SB270030–00, Systems and Equipment Section, FAA, ADDRESSES: You may send comments, Issue 002, dated April 7, 2017. Seattle ACO Branch, 2200 South 216th St., identified by number 1076–AF47, by Des Moines, WA 98198; phone and fax: 206– any of the following methods: (j) Parts Installation Prohibition 231–3548; email: [email protected]. As of the effective date of this AD, do not (2) For service information identified in —Federal rulemaking portal: http:// install on any airplane an EMA having part this AD, contact Boeing Commercial www.regulations.gov. Follow the number (P/N) C99144–004 or C99144–005. Airplanes, Attention: Contractual & Data instructions for sending comments. (k) Credit for Previous Actions Services (C&DS), 2600 Westminster Blvd., —Email: [email protected]. Include MC 110–SK57, Seal Beach, CA 90740–5600; the number 1076–AF47 in the subject This paragraph provides credit for the telephone 562–797–1717; internet https:// action specified in paragraph (i)(2) of this line of the message. www.myboeingfleet.com. You may view this —Mail or hand-delivery: Elizabeth AD, if those actions were performed before service information at the FAA, Transport the effective date of this AD using Boeing Standards Branch, 2200 South 216th St., Des Appel, Office of Regulatory Affairs & Service Bulletin B787–81205–SB270030–00, Moines, WA. You may view this referenced Collaborative Action, U.S. Department Issue 001, dated October 22, 2015. service information at the FAA, Transport of the Interior, 1849 C Street NW, (l) Alternative Methods of Compliance Standards Branch, 2200 South 216th St., Des MIB–4660–MS, Washington, DC (AMOCs) Moines, WA. For information on the 20240. Include the number 1076– availability of this material at the FAA, call (1) The Manager, Seattle ACO Branch, AF47 in the subject line of the 206–231–3195. FAA, has the authority to approve AMOCs message. for this AD, if requested using the procedures Issued in Des Moines, Washington, on June Instructions: All submissions received 14, 2019. found in 14 CFR 39.19. In accordance with must include ‘‘Bureau of Indian Affairs’’ 14 CFR 39.19, send your request to your Michael Kaszycki, principal inspector or local Flight Standards and ‘‘1076–AF47.’’ All comments Acting Director, System Oversight Division, received will be posted without change District Office, as appropriate. If sending Aircraft Certification Service. information directly to the manager of the to http://www.regulations.gov, including certification office, send it to the attention of [FR Doc. 2019–13673 Filed 7–1–19; 8:45 am] any personal information provided. the person identified in paragraph (m)(1) of BILLING CODE 4910–13–P Docket: For access to the docket to this AD. Information may be emailed to: 9– read background documents or [email protected]. comments received, go to http:// (2) Before using any approved AMOC, www.regulations.gov. We cannot ensure notify your appropriate principal inspector, DEPARTMENT OF THE INTERIOR or lacking a principal inspector, the manager that comments received after the close of the local flight standards district office/ Bureau of Indian Affairs of the comment period (see DATES) will certificate holding district office. be included in the docket for this (3) An AMOC that provides an acceptable 25 CFR Part 224 rulemaking and considered. level of safety may be used for any repair, Comments on the information modification, or alteration required by this RIN 1076–AF47 collections contained in this proposed AD if it is approved by The Boeing Company regulation (see ‘‘Paperwork Reduction Organization Designation Authorization [192D0102DR/DS5A300000/ Act’’ section, below) are separate from (ODA) that has been authorized by the DR.5A311.IA000118] Manager, Seattle ACO Branch, FAA, to make those on the substance of the rule. Send those findings. To be approved, the repair Tribal Energy Resource Agreements comments on the information collection method, modification deviation, or alteration burden to OMB by facsimile to (202) deviation must meet the certification basis of AGENCY: Bureau of Indian Affairs, 395–5806 or email to the OMB Desk the airplane, and the approval must Interior. Officer for the Department of the specifically refer to this AD. _ ACTION: Proposed rule. Interior at OIRA DOCKET@ (4) AMOCs approved previously for AD omb.eop.gov. Please send a copy of your 2017–15–04 are approved as AMOCs for the SUMMARY: The Bureau of Indian Affairs corresponding provisions of paragraph (g) of comments to the person listed in the this AD. (BIA) proposes to amend its regulations FOR FURTHER INFORMATION CONTACT (5) For service information that contains governing Tribal Energy Resource section of this notice. steps that are labeled as Required for Agreements (TERAs) between the Please see ‘‘III. Tribal Consultation’’ of Compliance (RC), the provisions of Secretary of the Interior (Secretary) and this preamble for addresses of Tribal paragraphs (l)(5)(i) and (l)(5)(ii) of this AD Indian Tribes. Tribes, at their discretion, consultation sessions on this proposed apply. may apply for TERAs. TERAs allow rule. (i) The steps labeled as RC, including Tribes to enter into leases, business FOR FURTHER INFORMATION CONTACT: substeps under an RC step and any figures agreements, and rights-of-way for energy identified in an RC step, must be done to Elizabeth Appel, Director, Office of resource development on Tribal land comply with the AD. If a step or substep is Regulatory Affairs & Collaborative without the Secretary’s review and labeled ‘‘RC Exempt,’’ then the RC Action, (202) 273–4680; approval. This proposed rule would requirement is removed from that step or [email protected]. substep. An AMOC is required for any update the regulations to incorporate deviations to RC steps, including substeps changes recently made by Congress to SUPPLEMENTARY INFORMATION: and identified figures. the Act authorizing TERAs. This I. Background (ii) Steps not labeled as RC may be II. Summary of This Proposed Rule proposed rule would also establish how III. Tribal Consultation deviated from using accepted methods in Tribal Energy Development accordance with the operator’s maintenance IV. Procedural Requirements or inspection program without obtaining Organizations (TEDOs) may obtain A. Regulatory Planning and Review (E.O. approval of an AMOC, provided the RC steps, certification, as an alternative to a 12866, 13563, and 13771) including substeps and identified figures, can TERA. B. Regulatory Flexibility Act still be done as specified, and the airplane C. Small Business Regulatory Enforcement DATES: Please submit comments by can be put back in an airworthy condition. Fairness Act September 3, 2019. Please see ‘‘III. D. Unfunded Mandates Reform Act (m) Related Information Tribal Consultation’’ of this preamble E. Takings (E.O. 12630) (1) For more information about this AD, for dates of Tribal consultation sessions F. Federalism (E.O. 13132) contact Douglas Tsuji, Aerospace Engineer, on this proposed rule. G. Civil Justice Reform (E.O. 12988)

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