Airworthiness Directives; BAE Systems (Operations) Limited Airplanes, 63973-63978 [2022-22202]

Download as PDF Federal Register / Vol. 87, No. 203 / Friday, October 21, 2022 / Proposed Rules (a) Comments Due Date The FAA must receive comments on this airworthiness directive (AD) by December 5, 2022. (b) Affected ADs None. (c) Applicability This AD applies to all MHI RJ Aviation ULC (Type Certificate Previously Held by Bombardier, Inc.) Model CL–600–2B19 (Regional Jet Series 100 & 440) airplanes, certificated in any category. (d) Subject Air Transport Association (ATA) of America Code 35, Oxygen. (e) Unsafe Condition This AD was prompted by a report of an oxygen-fed ground fire event potentially caused by electrical arcing from a faulty surround light wire on the third crew member’s (observer) oxygen mask. An investigation determined that the oxygen supply hose connecting to the rear of the observer oxygen mask box assembly could be subject to chafing damage. This AD was also prompted by the determination that additional inspections and a bracket trim are needed to address the unsafe condition. The FAA is issuing this AD to address possible damage to the observer oxygen mask supply hoses and a potential for an oxygen-fed fire in the vicinity of the observer oxygen mask storage compartment. jspears on DSK121TN23PROD with PROPOSALS (f) Compliance Comply with this AD within the compliance times specified, unless already done. (g) Required Actions Within 4,000 flight hours or 24 months, whichever occurs first after the effective date of this AD, do the actions in paragraphs (g)(1) and (2) of this AD: (1) For airplanes on which the actions specified in MHI RJ Service Bulletin 601R– 35–022, dated June 1, 2021; or MHI RJ Service Bulletin 601R–35–022, Revision A, dated October 12, 2021; have not been accomplished: Do the actions specified in paragraphs (g)(1)(i) and (ii) of this AD. (i) Do a general visual inspection for discrepancies of the observer’s oxygen mask stowage box and stowage compartment, the observer’s mask oxygen hose connections, the hose routing, and the associated electrical harness; reroute the electrical harness and apply protective sealant in accordance with Part A. Section 2.B. of the Accomplishment Instructions of MHI RJ Service Bulletin 601R–35–022, Revision B, dated April 21, 2022. If any discrepancies are found, before further flight, do all applicable corrective actions, in accordance with paragraph 2.B. of the Accomplishment Instructions of MHI RJ Service Bulletin 601R–35–022, Revision B, dated April 21, 2022. (ii) Modify the oxygen mask flexible lamp harness, mounting plate, and compartment panel, including rerouting the electrical harness; apply protective sealant; inspect the flexible lamp assembly for correct installation; and trim and reidentify the VerDate Sep<11>2014 16:38 Oct 20, 2022 Jkt 259001 bracket; in accordance with Part A. Section 2.B. of the Accomplishment Instructions of MHI RJ Service Bulletin 601R–35–022, Revision B, dated April 21, 2022. Do all applicable flexible lamp assembly installation corrections before further flight in accordance with Part A. Section 2.B. of the Accomplishment Instructions of MHI RJ Service Bulletin 601R–35–022, Revision B, dated April 21, 2022. (2) For airplanes on which the actions specified in MHI RJ Service Bulletin 601R– 35–022, dated June 1, 2021; or MHI RJ Service Bulletin 601R–35–022, Revision A, dated October 12, 2021; have been accomplished: Inspect the flexible lamp assembly for correct installation; inspect the wire harness assembly for damage; and trim and reidentify the bracket in accordance with Part B. Section 2.E. of the Accomplishment Instructions of MHI RJ Service Bulletin 601R–35–022, Revision B, dated April 21, 2022. Do all applicable flexible lamp assembly installation corrections and damage repair before further flight in accordance with Part B. Section 2.E. of the Accomplishment Instructions of MHI RJ Service Bulletin 601R–35–022, Revision B, dated April 21, 2022. (h) Other FAA AD Provisions The following provisions also apply to this AD: (1) Alternative Methods of Compliance (AMOCs): The Manager, New York ACO Branch, FAA, has the authority to approve AMOCs for this AD, if requested using the procedures found in 14 CFR 39.19. In accordance with 14 CFR 39.19, send your request to your principal inspector or responsible Flight Standards Office, as appropriate. If sending information directly to the manager of the certification office, send it to ATTN: Program Manager, Continuing Operational Safety, FAA, New York ACO Branch, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; telephone 516–228–7300. Before using any approved AMOC, notify your appropriate principal inspector, or lacking a principal inspector, the manager of the responsible Flight Standards Office. (2) Contacting the Manufacturer: For any requirement in this AD to obtain instructions from a manufacturer, the instructions must be accomplished using a method approved by the Manager, New York ACO Branch, FAA; or Transport Canada Civil Aviation (TCCA); or MHI RJ Aviation ULC’s TCCA Design Approval Organization (DAO). If approved by the DAO, the approval must include the DAO-authorized signature. (i) Additional Information (1) Refer to TCCA AD CF–2021–32R1, dated July 25, 2022, for related information. This TCCA AD may be found in the AD docket at regulations.gov under Docket No. FAA–2022–0141. (2) For more information about this AD, contact Gabriel Kim, Aerospace Engineer, Avionics and Electrical Systems Section, FAA, New York ACO Branch, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; telephone 516–228–7300; email 9-avs-nyacocos@faa.gov. PO 00000 Frm 00006 Fmt 4702 Sfmt 4702 63973 (j) Material Incorporated by Reference (1) The Director of the Federal Register approved the incorporation by reference 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 this AD specifies otherwise. (i) MHI RJ Aviation Service Bulletin 601R– 35–022, Revision B, dated April 21, 2022. (ii) [Reserved] (3) For service information identified in this AD, contact MHI RJ Aviation Group, Customer Response Center, 3655 Ave. des Grandes-Tourelles, Suite 110, Boisbriand, Que´bec J7H 0E2 Canada; North America tollfree telephone 833–990–7272 or direct-dial telephone 450–990–7272; fax 514–855–8501; email thd.crj@mhirj.com; website mhirj.com. (4) You may view this service information at the FAA, Airworthiness Products Section, Operational Safety Branch, 2200 South 216th St., Des Moines, WA. For information on the availability of this material at the FAA, call 206–231–3195. (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, email fr.inspection@nara.gov, or go to: www.archives.gov/federal-register/cfr/ibrlocations.html. Issued on October 7, 2022. Christina Underwood, Acting Director, Compliance & Airworthiness Division, Aircraft Certification Service. [FR Doc. 2022–22275 Filed 10–20–22; 8:45 am] BILLING CODE 4910–13–P DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA–2022–1298; Project Identifier MCAI–2022–00437–T] RIN 2120–AA64 Airworthiness Directives; BAE Systems (Operations) Limited Airplanes Federal Aviation Administration (FAA), DOT. ACTION: Notice of proposed rulemaking (NPRM). AGENCY: The FAA proposes to supersede Airworthiness Directives (ADs) 2005–15–11, 2016–07–09, and 2018–19–24, which apply to all BAE Systems (Operations) Limited Model 4101 airplanes. AD 2005–15–11 requires repetitive detailed and specialized inspections to detect fatigue damage in the fuselage, replacement of certain bolt assemblies, and corrective actions if necessary. AD 2016–07–09 requires a SUMMARY: E:\FR\FM\21OCP1.SGM 21OCP1 63974 Federal Register / Vol. 87, No. 203 / Friday, October 21, 2022 / Proposed Rules revision of the maintenance or inspection program, as applicable. AD 2018–19–24 requires a one-time detailed inspection of a certain fuselage frame and repair, if necessary, and a revision of the maintenance or inspection program, as applicable, to incorporate new or revised maintenance instructions and airworthiness limitations. Since the FAA issued those ADs, the FAA has determined that new or more restrictive airworthiness limitations are necessary. This proposed AD would continue to require the actions in AD 2016–07–09 and 2018– 19–24 and require revising the existing maintenance or inspection program, as applicable, to incorporate new or more restrictive airworthiness limitations. The FAA is proposing this AD to address the unsafe condition on these products. The FAA must receive comments on this NPRM by December 5, 2022. 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 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. AD Docket: You may examine the AD docket at regulations.gov under Docket No. FAA–2022–1298; or in person at Docket Operations between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. The AD docket contains this NPRM, the mandatory continuing airworthiness information (MCAI), any comments received, and other information. The street address for Docket Operations is listed above. Material Incorporated by Reference: • For service information identified in this NPRM, contact BAE Systems (Operations) Limited, Customer Information Department, Prestwick International Airport, Ayrshire, KA9 2RW, Scotland, United Kingdom; telephone +44 1292 675207; fax +44 1292 675704; email RApublications@ baesystems.com; website baesystems.com/Businesses/ RegionalAircraft/index.htm. • You may view this service information at the FAA, Airworthiness Products Section, Operational Safety Branch, 2200 South 216th St., Des jspears on DSK121TN23PROD with PROPOSALS DATES: VerDate Sep<11>2014 16:38 Oct 20, 2022 Jkt 259001 Moines, WA. For information on the availability of this material at the FAA, call 206–231–3195. FOR FURTHER INFORMATION CONTACT: Todd Thompson, Aerospace Engineer, Large Aircraft Section, FAA, International Validation Branch, 2200 South 216th St., Des Moines, WA 98198; telephone 206–231–3228; email todd.thompson@faa.gov. SUPPLEMENTARY INFORMATION: Comments Invited The FAA invites you to send any written relevant data, views, or arguments about this proposal. Send your comments to an address listed under ADDRESSES. Include ‘‘Docket No. FAA–2022–1298; Project Identifier MCAI–2022–00437–T’’ at the beginning of your comments. The most helpful comments reference a specific portion of the proposal, explain the reason for any recommended change, and include supporting data. The FAA will consider all comments received by the closing date and may amend the proposal because of those comments. Except for Confidential Business Information (CBI) as described in the following paragraph, and other information as described in 14 CFR 11.35, the FAA will post all comments received, without change, to regulations.gov, including any personal information you provide. The agency will also post a report summarizing each substantive verbal contact received about this NPRM. Confidential Business Information CBI is commercial or financial information that is both customarily and actually treated as private by its owner. Under the Freedom of Information Act (FOIA) (5 U.S.C. 552), CBI is exempt from public disclosure. If your comments responsive to this NPRM contain commercial or financial information that is customarily treated as private, that you actually treat as private, and that is relevant or responsive to this NPRM, it is important that you clearly designate the submitted comments as CBI. Please mark each page of your submission containing CBI as ‘‘PROPIN.’’ The FAA will treat such marked submissions as confidential under the FOIA, and they will not be placed in the public docket of this NPRM. Submissions containing CBI should be sent to Todd Thompson, Aerospace Engineer, Large Aircraft Section, FAA, International Validation Branch, 2200 South 216th St., Des Moines, WA 98198; telephone 206–231– 3228; email todd.thompson@faa.gov. Any commentary that the FAA receives PO 00000 Frm 00007 Fmt 4702 Sfmt 4702 that is not specifically designated as CBI will be placed in the public docket for this rulemaking. Background The FAA issued AD 2005–15–11, Amendment 39–14200 (70 FR 43025, July 26, 2005) (AD 2005–15–11) for all BAE Systems (Operations) Limited Model 4101 airplanes. AD 2005–15–11 was prompted by MCAI originated by the Civil Aviation Authority (CAA), which is the aviation authority for the United Kingdom (U.K.) (U.K. CAA). The U.K. CAA issued AD 2005–15–11 to correct an unsafe condition identified by a review of primary airframe fatigue test results and a Maintenance Steering Group 3 (MSG–3) analysis, which found a need to issue an AD to detect and correct fatigue damage of the fuselage, door, engine nacelle, empennage, and wing structures, which could result in reduced structural integrity of the airplane. AD 2005–15–11 requires repetitive detailed and specialized inspections to detect fatigue damage in the fuselage, replacement of certain bolt assemblies, and corrective actions if necessary. The FAA issued AD 2005–15–11 to address fatigue damage of the fuselage, door, engine nacelle, empennage, and wing structures, which could result in reduced structural integrity of the airplane. The FAA issued AD 2016–07–09, Amendment 39–18454 (81 FR 21263, April 11, 2016) (AD 2016–07–09), for all BAE Systems (Operations) Limited Model 4101 airplanes. AD 2016–07–09 was prompted by MCAI originated by the European Aviation Safety Agency (EASA), which is the Technical Agent for the Member States of the European Union. EASA issued AD 2014–0043, dated February 21, 2014 (EASA AD 2014–0043), to correct an unsafe condition identified as failure of certain structurally significant items, including the main landing gear and nose landing gear, and fuel vapor ignition sources. AD 2016–07–09 requires a revision of the maintenance or inspection program. The FAA issued AD 2016–07–09 to address failure of certain structurally significant items, including the main landing gear and nose landing gear, which could result in reduced structural integrity of the airplane; and to prevent fuel vapor ignition sources, which could result in a fuel tank explosion and consequent loss of the airplane. The FAA issued AD 2018–19–24, Amendment 39–19425 (83 FR 49786, October 3, 2018) (AD 2018–19–24), for all BAE Systems (Operations) Limited Model 4101 airplanes. AD 2018–19–24 was prompted by MCAI originated by E:\FR\FM\21OCP1.SGM 21OCP1 Federal Register / Vol. 87, No. 203 / Friday, October 21, 2022 / Proposed Rules jspears on DSK121TN23PROD with PROPOSALS EASA. EASA issued AD 2017–0187, September 22, 2017 (EASA AD 2017– 0187), to correct an unsafe condition identified as cracking in fuselage frame 90 and fatigue damage of various airplane structures. AD 2018–19–24 requires a one-time detailed inspection of a certain fuselage frame and repair, if necessary, and a revision of the maintenance or inspection program, as applicable, to incorporate new or revised maintenance instructions and airworthiness limitations. The FAA issued AD 2018– 19–24 to address cracking in fuselage frame 90, which could cause it to fail and thereby compromise the structural integrity of the aircraft pressure hull. The FAA also issued AD 2018–19–24 to address fatigue damage of various airplane structures, which could result in reduced structural integrity of the airplane. AD 2018–19–24 specifies that accomplishing the revision required by that AD terminates all requirements of AD 2005–15–11. J41Aircraft Maintenance Manual (AMM), Revision 44, dated June 15, 2021, for effectivity group 403; and BAE Systems (Operations) Limited J41 AMM, Revision 44, dated June 15, 2021, for effectivity group 408. This service information specifies airworthiness limitations for fuel tank systems and certification maintenance requirements. These documents are distinct since they apply to different airplanes. This proposed AD would also require: • Subjects 05–10–10, ‘‘Airworthiness Limitations’’; 05–10–20, ‘‘Certification Maintenance Requirements’’; and 05– 10–30, ‘‘Critical Design Configuration Control Limitations (CDCCL)—Fuel System’’; of Chapter 05, ‘‘Airworthiness Limitations,’’ of the BAE Systems (Operations) Limited J41 AMM, Revision 38, dated September 15, 2013, which the Director of the Federal Register approved for incorporation by reference as of May 16, 2016 (81 FR 21263, April 11, 2016); • BAE Systems (Operations) Limited Service Bulletin J41–51–001, Revision 4, dated July 11, 2017, which the Director of the Federal Register approved for incorporation by reference as of November 7, 2018 (83 FR 49786, October 3, 2018); and • BAE Systems (Operations) Limited Alert Service Bulletin J41–A53–058, dated December 6, 2016, which the Director of the Federal Register approved for incorporation by reference as of November 7, 2018 (83 FR 49786, October 3, 2018). 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. Actions Since ADs 2015–15–11, 2016– 07–09, and 2018–19–24 Were Issued Since the FAA issued ADs 2015–15– 11, 2016–07–09, and 2018–19–24, the U.K. CAA superseded EASA ADs 2014– 0043 and 2017–0187, and issued U.K. CAA AD G–2022–0006, dated March 30, 2022 (U.K. CAA AD G–2022–0006; also referred to as the MCAI). U.K. CAA AD G–2022–0006 states that the repetitive inspection requirements for Structural Significant Items (SSI) 53–10–029 were not addressed in EASA AD 2017–0187, and additional SSI inspections are necessary (inspections for cracking of Hi-Shear (now LISL)) collars. U.K. CAA AD G–2022–0006 also states that failure to comply with new or more restrictive actions could result in an unsafe condition. The FAA is issuing this AD to address fatigue damage of various airplane structures and failure of certain structurally significant items, which could result in reduced structural integrity of the airplane. The FAA is also issuing this AD to address fuel vapor ignition sources, which could result in a fuel tank explosion and consequent loss of the airplane. You may examine U.K. CAA AD G–2022– 0006 in the AD docket at regulations.gov under Docket No. FAA–2022–1298. FAA’s Determination This product has been approved by the aviation authority of another country, and is approved for operation in the United States. Pursuant to the FAA’s bilateral agreement with the State of Design Authority, it has notified the FAA of the unsafe condition described in the MCAI and service information described above. The FAA is issuing this NPRM after determining that the unsafe condition described previously is likely to exist or develop on other products of the same type design. Related Service Information Under 1 CFR Part 51 The FAA reviewed Chapter 05 of BAE Systems (Operations) Limited Proposed Requirements of This NPRM This proposed AD would retain none of the requirements of AD 2005–15–11; certain requirements of AD 2016–07–09; VerDate Sep<11>2014 16:38 Oct 20, 2022 Jkt 259001 PO 00000 Frm 00008 Fmt 4702 Sfmt 4702 63975 and all requirements of AD 2018–19–24. This proposed AD would require revising the existing maintenance or inspection program, as applicable, to incorporate new or more restrictive airworthiness limitations. This proposed AD would require revisions to certain operator maintenance documents to include new actions (e.g., inspections) and Critical Design Configuration Control Limitations (CDCCLs). Compliance with these actions and CDCCLs is required by 14 CFR 91.403(c). For airplanes that have been previously modified, altered, or repaired in the areas addressed by this proposed 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 (o)(1) of this proposed AD. Costs of Compliance The FAA estimates that this AD, if adopted as proposed, would affect 10 airplanes of U.S. registry. The FAA estimates the following costs to comply with this proposed AD: The FAA estimates the total cost per operator for the retained actions from AD 2016–07–09 to be $7,650 (90 workhours × $85 per work-hour). The FAA estimates the total cost per operator for the retained maintenance or inspection program revision from AD 2018–19–24 to be $7,650 (90 work-hours × $85 per work-hour) The FAA has determined that revising the maintenance or inspection program takes an average of 90 work-hours per operator, although the agency recognizes that this number may vary from operator to operator. Since operators incorporate maintenance or inspection program changes for their affected fleet(s), the FAA has determined that a per-operator estimate is more accurate than a per-airplane estimate. Therefore, the agency estimates the average total cost per operator to be $7,650 (90 work-hours × $85 per work-hour). The FAA estimates the total cost per operator for the new proposed actions to be $7,650 (90 work-hours × $85 per work-hour). E:\FR\FM\21OCP1.SGM 21OCP1 63976 Federal Register / Vol. 87, No. 203 / Friday, October 21, 2022 / Proposed Rules ESTIMATED COSTS FOR REQUIRED ACTIONS Action Labor cost Inspection (Retained actions from AD 2018– 19–24). 2 work-hours × $85 per hour = $170 ............. The FAA has received no definitive data on which to base the cost estimates for the on-condition actions specified in this AD. 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. The FAA is 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. jspears on DSK121TN23PROD with PROPOSALS Regulatory Findings The FAA 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) Would not affect intrastate aviation in Alaska, and (3) Would not have a significant economic impact, positive or negative, on a substantial number of small entities under the criteria of the Regulatory Flexibility Act. List of Subjects in 14 CFR Part 39 Air transportation, Aircraft, Aviation safety, Incorporation by reference, Safety. The Proposed Amendment Accordingly, under the authority delegated to me by the Administrator, VerDate Sep<11>2014 16:38 Oct 20, 2022 Jkt 259001 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: a. Removing Airworthiness Directive AD 2005–15–11, Amendment 39–14200 (70 FR 43025, July 26, 2005); AD 2016– 07–09, Amendment 39–18454 (81 FR 21263, April 11, 2016); and AD 2018– 19–24, Amendment 39–19425 (83 FR 49786, October 3, 2018); and ■ b. Adding the following new airworthiness directive: ■ ■ BAE Systems (Operations) Limited: Docket No. FAA–2022–1298; Project Identifier MCAI–2022–00437–T. (a) Comments Due Date The FAA must receive comments on this airworthiness directive (AD) by December 5, 2022. (b) Affected ADs (1) This AD replaces AD 2005–15–11, Amendment 39–14200 (70 FR 43025, July 26, 2005) (AD 2005–15–11). (2) This AD replaces AD 2016–07–09, Amendment 39–18454 (81 FR 21263, April 11, 2016) (AD 2016–07–09). (3) This AD replaces AD 2018–19–24, Amendment 39–19425 (83 FR 49786, October 3, 2018) (AD 2018–19–24). (c) Applicability This AD applies to all BAE Systems (Operations) Limited Model 4101 airplanes, certificated in any category. (d) Subject Air Transport Association (ATA) of America Code 05, Time Limits/Maintenance Checks. (e) Reason This AD was prompted by a determination that new or more restrictive airworthiness limitations are necessary. The FAA is issuing this AD to address fatigue damage of various airplane structures and failure of certain structurally significant items, which could result in reduced structural integrity of the airplane. The FAA is also issuing this AD to address fuel vapor ignition sources, which could result in a fuel tank explosion and consequent loss of the airplane. PO 00000 Frm 00009 Fmt 4702 Sfmt 4702 Cost per product Parts cost $0 $170 Cost on U.S. operators $1,700 (f) Compliance Comply with this AD within the compliance times specified, unless already done. (g) Retained Revision of the Maintenance or Inspection Program (From AD 2016–07–09), With No Changes This paragraph restates the requirements of paragraph (i) of AD 2016–07–09, with no changes. Within 90 days after May 16, 2016 (the effective date of AD 2016–07–09): Revise the maintenance or inspection program, as applicable, by incorporating Subjects 05–10– 10, ‘‘Airworthiness Limitations’’; 05–10–20, ‘‘Certification Maintenance Requirements’’; and 05–10–30, ‘‘Critical Design Configuration Control Limitations (CDCCL)—Fuel System’’; of Chapter 05, ‘‘Airworthiness Limitations,’’ of the BAE Systems (Operations) Limited J41 AMM, Revision 38, dated September 15, 2013. The initial compliance times for the tasks are at the applicable times specified in paragraphs (g)(1) through (3) of this AD. Accomplishing the revision of the existing maintenance or inspection program required by paragraph (m) of this AD terminates the requirements of this paragraph. (1) For replacement tasks of life limited parts specified in Subject 05–10–10, ‘‘Airworthiness Limitations,’’ of Chapter 05, ‘‘Airworthiness Limitations,’’ of the BAE Systems (Operations) Limited J41 AMM, Revision 38, dated September 15, 2013: Prior to the applicable flight cycles (landings) or flight hours (flying hours) on the part specified in the ‘‘Mandatory Life Limits’’ column in Subject 05–10–10, or within 90 days after May 16, 2016 (the effective date of AD 2016–07–09), whichever occurs later. (2) For structurally significant item tasks specified in Subject 05–10–10, ‘‘Airworthiness Limitations,’’ of Chapter 05, ‘‘Airworthiness Limitations,’’ of the BAE Systems (Operations) Limited J41 AMM, Revision 38, dated September 15, 2013: Prior to the accumulation of the applicable flight cycles specified in the ‘‘Initial Inspection’’ column in Subject 05–10–10, or within 90 days after May 16, 2016 (the effective date of AD 2016–07–09), whichever occurs later. (3) For certification maintenance requirements tasks specified in Subject 05– 10–20, ‘‘Certification Maintenance Requirements,’’ of Chapter 05, ‘‘Airworthiness Limitations,’’ of the BAE Systems (Operations) Limited J41 AMM, Revision 38, dated September 15, 2013: Prior to the accumulation of the applicable flight hours specified in the ‘‘Time Between Checks’’ column in Subject 05–10–20, or within 90 days after May 16, 2016 (the effective date of AD 2016–07–09), whichever occurs later; except for tasks that specify ‘‘first flight of the day’’ in the ‘‘Time Between Checks’’ column in Subject 05–10–20, the E:\FR\FM\21OCP1.SGM 21OCP1 Federal Register / Vol. 87, No. 203 / Friday, October 21, 2022 / Proposed Rules initial compliance time is the first flight of the next day after doing the revision required by paragraph (g) of AD 2016–07–09, or within 90 days after May 16, 2016, whichever occurs later. (h) Retained Restrictions on Alternative Actions, Intervals, and/or (CDCCLs), With No Changes This paragraph restates the requirements of paragraph (j) of AD 2016–07–09, with no changes. Except as required by paragraph (m) of this AD, after the maintenance or inspection program, as applicable, has been revised as required by paragraph (g) of this AD, no alternative actions (e.g., inspections), intervals, and/or CDCCLs may be used unless the actions, intervals, and/or CDCCLs are approved as an alternative method of compliance (AMOC) in accordance with the procedures specified in paragraph (o)(1) of this AD. jspears on DSK121TN23PROD with PROPOSALS (i) Retained Inspection, With No Changes This paragraph restates the requirements of paragraph (g) of AD 2018–19–24, with no changes. At the compliance times specified in paragraphs (i)(1) and (2) of this AD, as applicable: Do a detailed inspection of fuselage frame 90 for cracking or fatigue damage, in accordance with the Accomplishment Instructions of BAE Systems (Operations) Limited Alert Service Bulletin J41–A53–058, dated December 6, 2016. If any cracking or fatigue damage is found: Before further flight, repair using a method approved by the Manager, International Section, Transport Standards Branch, FAA; or the European Aviation Safety Agency (EASA); or BAE Systems (Operations) Limited’s EASA Design Organization Approval (DOA). Accomplishing the revision of the existing maintenance or inspection program required by paragraph (m) of this AD terminates the requirements of this paragraph. (1) For airplanes with 6,300 flight cycles or fewer since Structural Significant Items (SSI) 53–10–029 (Maintenance Planning Document (MPD) 531029–DVl–10010–1) was last accomplished: Within 6,600 flight cycles after the last accomplishment of SSI 53–10– 029 (MPD 531029–DVl–10010–1), or within 6 months after November 7, 2018 (the effective date of AD 2018–19–24), whichever is later. (2) For airplanes with more than 6,300 flight cycles since SSI 53–10–029 (MPD 531029–DVl–10010–1) was last accomplished: Within 300 flight cycles or 4.5 months, whichever is earlier, since the last accomplishment of SSI 53–10–029 (MPD 531029–DVl–10010–1), or within 6 months after November 7, 2018 (the effective date of AD 2018–19–24), whichever is later. (j) Retained Revision of Maintenance or Inspection Program (From AD 2018–19–24), With No Changes This paragraph restates the requirements of paragraph (h) of AD 2018–19–24, with no changes. Within 90 days after November 7, 2018 (the effective date of AD 2018–19–24): Revise the maintenance or inspection program, as applicable, by incorporating the maintenance tasks and associated thresholds and intervals described in, and in accordance with, the Accomplishment Instructions of VerDate Sep<11>2014 16:38 Oct 20, 2022 Jkt 259001 BAE Systems (Operations) Limited Service Bulletin J41–51–001, Revision 4, dated July 11, 2017. The initial compliance times for new or revised tasks are at the applicable times specified in BAE Systems (Operations) Limited Service Bulletin J41–51–001, Revision 4, dated July 11, 2017, or within 6 months after November 7, 2018, whichever is later. Accomplishing the revision of the existing maintenance or inspection program required by paragraph (m) of this AD terminates the requirements of this paragraph. (k) Retained No Alternative Actions and Intervals, With No Changes This paragraph restates the requirements of paragraph (i) of AD 2018–19–24, with no changes. Except as required by paragraph (m) of this AD: After the maintenance or inspection program has been revised as required by paragraph (j) of this AD, no alternative actions (e.g., inspections) or intervals may be used unless the actions or intervals are approved as an AMOC in accordance with the procedures specified in paragraph (o)(1) of this AD. (l) Retained No Reporting Requirement, With No Changes This paragraph restates the requirements of paragraph (k) of AD 2018–19–24, with no changes. Although the Accomplishment Instructions of BAE Systems (Operations) Limited Alert Service Bulletin J41–A53–058, dated December 6, 2016, specify to submit certain information to the manufacturer, this AD does not include that requirement. (m) New Revision of the Existing Maintenance or Inspection Program Within 90 days after the effective date of this AD: Revise the existing maintenance or inspection program, as applicable, by incorporating Subjects 05–10–10, ‘‘Airworthiness Limitations’’; 05–10–20, ‘‘Certification Maintenance Requirements’’; and 05–10–30, ‘‘Critical Design Configuration Control Limitations (CDCCL)—Fuel System’’; of Chapter 05, ‘‘Airworthiness Limitations,’’ of the BAE Systems (Operations) Limited J41 AMM, Revision 44, dated June 15, 2021, for effectivity group 403; or BAE Systems (Operations) Limited J41 AMM, Revision 44, dated June 15, 2021, for effectivity group 408; as applicable. The initial compliance times for the tasks are at the applicable times specified in paragraphs (m)(1) through (3) of this AD. Accomplishing the revision of the existing maintenance or inspection program required by this paragraph terminates the actions required by paragraphs (g), (i) and (j) of this AD. (1) For replacement tasks of life limited parts specified in Subject 05–10–10, ‘‘Airworthiness Limitations,’’ of Chapter 05, ‘‘Airworthiness Limitations,’’ of the BAE Systems (Operations) Limited J41 AMM, Revision 44, dated June 15, 2021, for effectivity group 403; or BAE Systems (Operations) Limited J41 AMM, Revision 44, dated June 15, 2021, for effectivity group 408; as applicable: Prior to the applicable flight cycles (landings) or flight hours (flying hours) on the part specified in the ‘‘Mandatory Life Limits’’ column in Subject 05–10–10, or within 90 days after the PO 00000 Frm 00010 Fmt 4702 Sfmt 4702 63977 effective date of this AD, whichever occurs later. (2) For structurally significant item tasks specified in Subject 05–10–10, ‘‘Airworthiness Limitations,’’ of Chapter 05, ‘‘Airworthiness Limitations,’’ of the BAE Systems (Operations) Limited J41 AMM, Revision 44, dated June 15, 2021, for effectivity group 403; or BAE Systems (Operations) Limited J41 AMM, Revision 44, dated June 15, 2021. for effectivity group 408; as applicable: Prior to the accumulation of the applicable flight cycles specified in the ‘‘Initial Inspection’’ column in Subject 05– 10–10, or within 90 days after the effective date of this AD, whichever occurs later. (3) For certification maintenance requirements tasks specified in Subject 05– 10–20, ‘‘Certification Maintenance Requirements,’’ of Chapter 05, ‘‘Airworthiness Limitations,’’ of the BAE Systems (Operations) Limited J41 AMM, Revision 44, dated June 15, 2021, for effectivity group 403; or BAE Systems (Operations) Limited J41 AMM, Revision 44, dated June 15, 2021, for effectivity group 408; as applicable: Prior to the accumulation of the applicable flight hours specified in the ‘‘Time Between Checks’’ column in Subject 05–10–20, or within 90 days after the effective date of this AD, whichever occurs later; except for tasks that specify ‘‘first flight of the day’’ in the ‘‘Time Between Checks’’ column in Subject 05–10–20, the initial compliance time is the first flight of the next day after accomplishing the revision required by paragraph (m) of this AD, or within 90 days after the effective date of this AD, whichever occurs later. (n) New No Alternative Actions, Intervals, or Critical Design Configuration Control Limitations (CDCCLs) After the existing maintenance or inspection program has been revised as required by paragraph (m) of this AD, no alternative actions (e.g., inspections), intervals, or CDCCLs may be used unless the actions, intervals, and CDCCLs are approved as an AMOC in accordance with the procedures specified in paragraph (o)(1) of this AD. (o) Additional AD Provisions The following provisions also apply to this AD: (1) Alternative Methods of Compliance (AMOCs): The Manager, International Validation Branch, FAA, has the authority to approve AMOCs for this AD, if requested using the procedures found in 14 CFR 39.19. In accordance with 14 CFR 39.19, send your request to your principal inspector or responsible Flight Standards Office, as appropriate. If sending information directly to the International Validation Branch, send it to the attention of the person identified in paragraph (p)(2) of this AD. Information may be emailed to: 9-AVS-AIR-730-AMOC@ faa.gov. Before using any approved AMOC, notify your appropriate principal inspector, or lacking a principal inspector, the manager of the responsible Flight Standards Office. (2) Contacting the Manufacturer: For any requirement in this AD to obtain instructions from a manufacturer, the instructions must E:\FR\FM\21OCP1.SGM 21OCP1 63978 Federal Register / Vol. 87, No. 203 / Friday, October 21, 2022 / Proposed Rules be accomplished using a method approved by the Manager, International Validation Branch, FAA; or the United Kingdom Civil Aviation Authority (U.K. CAA); or BAE Systems (Operations) Limited’s U.K. CAA Design Organization Approval (DOA). If approved by the DOA, the approval must include the DOA-authorized signature. jspears on DSK121TN23PROD with PROPOSALS (p) Additional Information (1) Refer to U.K. CAA AD G–2022–0006, dated March 30, 2022, for related information. This U.K. CAA AD may be found in the AD docket at regulations.gov under Docket No. FAA–2022–1298. (2) For more information about this AD, contact Todd Thompson, Aerospace Engineer, Large Aircraft Section, FAA, International Validation Branch, 2200 South 216th St., Des Moines, WA 98198; telephone 206–231–3228; email todd.thompson@ faa.gov. (q) 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 this AD specifies otherwise. (3) The following service information was approved for IBR. (i) Chapter 05 of BAE Systems (Operations) Limited J41 Aircraft Maintenance Manual (AMM), Revision 44, dated June 15, 2021, for effectivity group 403; (ii) Chapter 05 of BAE Systems (Operations) Limited J41 AMM, Revision 44, dated June 15, 2021, for effectivity group 408. (4) The following service information was approved for IBR on November 7, 2018 (83 FR 49786, October 3, 2018). (i) BAE Systems (Operations) Limited Alert Service Bulletin J41–A53–058, dated December 6, 2016. (ii) BAE Systems (Operations) Limited Service Bulletin J41–51–001, Revision 4, dated July 11, 2017. (5) The following service information was approved for IBR on May 16, 2016 (81 FR 21263, April 11, 2016). (i) Chapter 05, ‘‘Airworthiness Limitations,’’ of the BAE Systems (Operations) Limited J41 Aircraft Maintenance Manual (AMM), Revision 38, dated September 15, 2013. Page 1 of the ‘‘Publications Transmittal’’ is the only page that shows the revision level of this document. (A) Subject 05–10–10, ‘‘Airworthiness Limitations.’’ (B) Subject 05–10–20, ‘‘Certification Maintenance Requirements.’’ (C) Subject 05–10–30, ‘‘Critical Design Configuration Control Limitations (CDCCL)— Fuel System.’’ (ii) [Reserved] (6) For service information identified in this AD, contact BAE Systems (Operations) Limited, Customer Information Department, Prestwick International Airport, Ayrshire, KA9 2RW, Scotland, United Kingdom; telephone +44 1292 675207; fax +44 1292 675704; email RApublications@ VerDate Sep<11>2014 16:38 Oct 20, 2022 Jkt 259001 baesystems.com; website baesystems.com/ Businesses/RegionalAircraft/index.htm. (7) You may view this service information at the FAA, Airworthiness Products Section, Operational Safety Branch, 2200 South 216th St., Des Moines, WA. For information on the availability of this material at the FAA, call 206–231–3195. (8) 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, email fr.inspection@nara.gov, or go to: www.archives.gov/federal-register/cfr/ibrlocations.html. Issued on October 6, 2022. Christina Underwood, Acting Director, Compliance & Airworthiness Division, Aircraft Certification Service. [FR Doc. 2022–22202 Filed 10–20–22; 8:45 am] BILLING CODE 4910–13–P DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA–2022–1297; Project Identifier MCAI–2022–00570–T] RIN 2120–AA64 Airworthiness Directives; Dassault Aviation Airplanes Federal Aviation Administration (FAA), DOT. ACTION: Notice of proposed rulemaking (NPRM). AGENCY: The FAA proposes to adopt a new airworthiness directive (AD) for certain Dassault Aviation Model FALCON 7X airplanes. This proposed AD was prompted by a report of smoke in the flightdeck and loss of the righthand (RH) primary display unit (PDU) and the secondary flight display (SFD). This proposed AD would require inspecting the two electrical power feeders for damage (deterioration), measuring the clearance between the two electrical power feeders and the forward lavatory bulkhead, and applicable corrective actions, as specified in a European Union Aviation Safety Agency (EASA) AD, which is proposed for incorporation by reference (IBR). The FAA is proposing this AD to address the unsafe condition on these products. DATES: The FAA must receive comments on this proposed AD by December 5, 2022. ADDRESSES: You may send comments, using the procedures found in 14 CFR 11.43 and 11.45, by any of the following methods: SUMMARY: PO 00000 Frm 00011 Fmt 4702 Sfmt 4702 • Federal eRulemaking Portal: Go to 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. AD Docket: You may examine the AD docket at regulations.gov under Docket No. FAA–2022–1297; or in person at Docket Operations between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. The AD docket contains this NPRM, the mandatory continuing airworthiness information (MCAI), any comments received, and other information. The street address for Docket Operations is listed above. Material Incorporated by Reference: • For material that is proposed for IBR in this NPRM, contact EASA, Konrad-Adenauer-Ufer 3, 50668 Cologne, Germany; telephone +49 221 8999 000; email ADs@easa.europa.eu; website easa.europa.eu. You may find this material on the EASA website at ad.easa.europa.eu. It is also available in the AD docket at regulations.gov by searching for and locating Docket No. FAA–2022–1297. • You may view this material at the FAA, Airworthiness Products Section, Operational Safety Branch, 2200 South 216th St., Des Moines, WA. For information on the availability of this material at the FAA, call 206–231–3195. FOR FURTHER INFORMATION CONTACT: Tom Rodriguez, Aerospace Engineer, Large Aircraft Section, FAA, International Validation Branch, 2200 South 216th St., Des Moines, WA 98198; telephone 206–231–3226; email Tom.Rodriguez@ faa.gov. SUPPLEMENTARY INFORMATION: Comments Invited The FAA invites you to send any written relevant data, views, or arguments about this proposal. Send your comments to an address listed under ADDRESSES. Include ‘‘Docket No. FAA–2022–1297; Project Identifier MCAI–2022–00570–T’’ at the beginning of your comments. The most helpful comments reference a specific portion of the proposal, explain the reason for any recommended change, and include supporting data. The FAA will consider all comments received by the closing date and may amend this proposal because of those comments. Except for Confidential Business Information (CBI) as described in the E:\FR\FM\21OCP1.SGM 21OCP1

Agencies

[Federal Register Volume 87, Number 203 (Friday, October 21, 2022)]
[Proposed Rules]
[Pages 63973-63978]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2022-22202]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2022-1298; Project Identifier MCAI-2022-00437-T]
RIN 2120-AA64


Airworthiness Directives; BAE Systems (Operations) Limited 
Airplanes

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Notice of proposed rulemaking (NPRM).

-----------------------------------------------------------------------

SUMMARY: The FAA proposes to supersede Airworthiness Directives (ADs) 
2005-15-11, 2016-07-09, and 2018-19-24, which apply to all BAE Systems 
(Operations) Limited Model 4101 airplanes. AD 2005-15-11 requires 
repetitive detailed and specialized inspections to detect fatigue 
damage in the fuselage, replacement of certain bolt assemblies, and 
corrective actions if necessary. AD 2016-07-09 requires a

[[Page 63974]]

revision of the maintenance or inspection program, as applicable. AD 
2018-19-24 requires a one-time detailed inspection of a certain 
fuselage frame and repair, if necessary, and a revision of the 
maintenance or inspection program, as applicable, to incorporate new or 
revised maintenance instructions and airworthiness limitations. Since 
the FAA issued those ADs, the FAA has determined that new or more 
restrictive airworthiness limitations are necessary. This proposed AD 
would continue to require the actions in AD 2016-07-09 and 2018-19-24 
and require revising the existing maintenance or inspection program, as 
applicable, to incorporate new or more restrictive airworthiness 
limitations. The FAA is proposing this AD to address the unsafe 
condition on these products.

DATES: The FAA must receive comments on this NPRM by December 5, 2022.

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 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.
    AD Docket: You may examine the AD docket at regulations.gov under 
Docket No. FAA-2022-1298; or in person at Docket Operations between 9 
a.m. and 5 p.m., Monday through Friday, except Federal holidays. The AD 
docket contains this NPRM, the mandatory continuing airworthiness 
information (MCAI), any comments received, and other information. The 
street address for Docket Operations is listed above.
    Material Incorporated by Reference:
     For service information identified in this NPRM, contact 
BAE Systems (Operations) Limited, Customer Information Department, 
Prestwick International Airport, Ayrshire, KA9 2RW, Scotland, United 
Kingdom; telephone +44 1292 675207; fax +44 1292 675704; email 
[email protected]; website baesystems.com/Businesses/RegionalAircraft/index.htm.
     You may view this service information at the FAA, 
Airworthiness Products Section, Operational Safety Branch, 2200 South 
216th St., Des Moines, WA. For information on the availability of this 
material at the FAA, call 206-231-3195.

FOR FURTHER INFORMATION CONTACT: Todd Thompson, Aerospace Engineer, 
Large Aircraft Section, FAA, International Validation Branch, 2200 
South 216th St., Des Moines, WA 98198; telephone 206-231-3228; email 
[email protected].

SUPPLEMENTARY INFORMATION:

Comments Invited

    The FAA invites you to send any written relevant data, views, or 
arguments about this proposal. Send your comments to an address listed 
under ADDRESSES. Include ``Docket No. FAA-2022-1298; Project Identifier 
MCAI-2022-00437-T'' at the beginning of your comments. The most helpful 
comments reference a specific portion of the proposal, explain the 
reason for any recommended change, and include supporting data. The FAA 
will consider all comments received by the closing date and may amend 
the proposal because of those comments.
    Except for Confidential Business Information (CBI) as described in 
the following paragraph, and other information as described in 14 CFR 
11.35, the FAA will post all comments received, without change, to 
regulations.gov, including any personal information you provide. The 
agency will also post a report summarizing each substantive verbal 
contact received about this NPRM.

Confidential Business Information

    CBI is commercial or financial information that is both customarily 
and actually treated as private by its owner. Under the Freedom of 
Information Act (FOIA) (5 U.S.C. 552), CBI is exempt from public 
disclosure. If your comments responsive to this NPRM contain commercial 
or financial information that is customarily treated as private, that 
you actually treat as private, and that is relevant or responsive to 
this NPRM, it is important that you clearly designate the submitted 
comments as CBI. Please mark each page of your submission containing 
CBI as ``PROPIN.'' The FAA will treat such marked submissions as 
confidential under the FOIA, and they will not be placed in the public 
docket of this NPRM. Submissions containing CBI should be sent to Todd 
Thompson, Aerospace Engineer, Large Aircraft Section, FAA, 
International Validation Branch, 2200 South 216th St., Des Moines, WA 
98198; telephone 206-231-3228; email [email protected]. Any 
commentary that the FAA receives that is not specifically designated as 
CBI will be placed in the public docket for this rulemaking.

Background

    The FAA issued AD 2005-15-11, Amendment 39-14200 (70 FR 43025, July 
26, 2005) (AD 2005-15-11) for all BAE Systems (Operations) Limited 
Model 4101 airplanes. AD 2005-15-11 was prompted by MCAI originated by 
the Civil Aviation Authority (CAA), which is the aviation authority for 
the United Kingdom (U.K.) (U.K. CAA). The U.K. CAA issued AD 2005-15-11 
to correct an unsafe condition identified by a review of primary 
airframe fatigue test results and a Maintenance Steering Group 3 (MSG-
3) analysis, which found a need to issue an AD to detect and correct 
fatigue damage of the fuselage, door, engine nacelle, empennage, and 
wing structures, which could result in reduced structural integrity of 
the airplane.
    AD 2005-15-11 requires repetitive detailed and specialized 
inspections to detect fatigue damage in the fuselage, replacement of 
certain bolt assemblies, and corrective actions if necessary. The FAA 
issued AD 2005-15-11 to address fatigue damage of the fuselage, door, 
engine nacelle, empennage, and wing structures, which could result in 
reduced structural integrity of the airplane.
    The FAA issued AD 2016-07-09, Amendment 39-18454 (81 FR 21263, 
April 11, 2016) (AD 2016-07-09), for all BAE Systems (Operations) 
Limited Model 4101 airplanes. AD 2016-07-09 was prompted by MCAI 
originated by the European Aviation Safety Agency (EASA), which is the 
Technical Agent for the Member States of the European Union. EASA 
issued AD 2014-0043, dated February 21, 2014 (EASA AD 2014-0043), to 
correct an unsafe condition identified as failure of certain 
structurally significant items, including the main landing gear and 
nose landing gear, and fuel vapor ignition sources.
    AD 2016-07-09 requires a revision of the maintenance or inspection 
program. The FAA issued AD 2016-07-09 to address failure of certain 
structurally significant items, including the main landing gear and 
nose landing gear, which could result in reduced structural integrity 
of the airplane; and to prevent fuel vapor ignition sources, which 
could result in a fuel tank explosion and consequent loss of the 
airplane.
    The FAA issued AD 2018-19-24, Amendment 39-19425 (83 FR 49786, 
October 3, 2018) (AD 2018-19-24), for all BAE Systems (Operations) 
Limited Model 4101 airplanes. AD 2018-19-24 was prompted by MCAI 
originated by

[[Page 63975]]

EASA. EASA issued AD 2017-0187, September 22, 2017 (EASA AD 2017-0187), 
to correct an unsafe condition identified as cracking in fuselage frame 
90 and fatigue damage of various airplane structures.
    AD 2018-19-24 requires a one-time detailed inspection of a certain 
fuselage frame and repair, if necessary, and a revision of the 
maintenance or inspection program, as applicable, to incorporate new or 
revised maintenance instructions and airworthiness limitations. The FAA 
issued AD 2018-19-24 to address cracking in fuselage frame 90, which 
could cause it to fail and thereby compromise the structural integrity 
of the aircraft pressure hull. The FAA also issued AD 2018-19-24 to 
address fatigue damage of various airplane structures, which could 
result in reduced structural integrity of the airplane. AD 2018-19-24 
specifies that accomplishing the revision required by that AD 
terminates all requirements of AD 2005-15-11.

Actions Since ADs 2015-15-11, 2016-07-09, and 2018-19-24 Were Issued

    Since the FAA issued ADs 2015-15-11, 2016-07-09, and 2018-19-24, 
the U.K. CAA superseded EASA ADs 2014-0043 and 2017-0187, and issued 
U.K. CAA AD G-2022-0006, dated March 30, 2022 (U.K. CAA AD G-2022-0006; 
also referred to as the MCAI). U.K. CAA AD G-2022-0006 states that the 
repetitive inspection requirements for Structural Significant Items 
(SSI) 53-10-029 were not addressed in EASA AD 2017-0187, and additional 
SSI inspections are necessary (inspections for cracking of Hi-Shear 
(now LISL)) collars. U.K. CAA AD G-2022-0006 also states that failure 
to comply with new or more restrictive actions could result in an 
unsafe condition. The FAA is issuing this AD to address fatigue damage 
of various airplane structures and failure of certain structurally 
significant items, which could result in reduced structural integrity 
of the airplane. The FAA is also issuing this AD to address fuel vapor 
ignition sources, which could result in a fuel tank explosion and 
consequent loss of the airplane. You may examine U.K. CAA AD G-2022-
0006 in the AD docket at regulations.gov under Docket No. FAA-2022-
1298.

Related Service Information Under 1 CFR Part 51

    The FAA reviewed Chapter 05 of BAE Systems (Operations) Limited 
J41Aircraft Maintenance Manual (AMM), Revision 44, dated June 15, 2021, 
for effectivity group 403; and BAE Systems (Operations) Limited J41 
AMM, Revision 44, dated June 15, 2021, for effectivity group 408. This 
service information specifies airworthiness limitations for fuel tank 
systems and certification maintenance requirements. These documents are 
distinct since they apply to different airplanes.
    This proposed AD would also require:
     Subjects 05-10-10, ``Airworthiness Limitations''; 05-10-
20, ``Certification Maintenance Requirements''; and 05-10-30, 
``Critical Design Configuration Control Limitations (CDCCL)--Fuel 
System''; of Chapter 05, ``Airworthiness Limitations,'' of the BAE 
Systems (Operations) Limited J41 AMM, Revision 38, dated September 15, 
2013, which the Director of the Federal Register approved for 
incorporation by reference as of May 16, 2016 (81 FR 21263, April 11, 
2016);
     BAE Systems (Operations) Limited Service Bulletin J41-51-
001, Revision 4, dated July 11, 2017, which the Director of the Federal 
Register approved for incorporation by reference as of November 7, 2018 
(83 FR 49786, October 3, 2018); and
     BAE Systems (Operations) Limited Alert Service Bulletin 
J41-A53-058, dated December 6, 2016, which the Director of the Federal 
Register approved for incorporation by reference as of November 7, 2018 
(83 FR 49786, October 3, 2018).
    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

    This product has been approved by the aviation authority of another 
country, and is approved for operation in the United States. Pursuant 
to the FAA's bilateral agreement with the State of Design Authority, it 
has notified the FAA of the unsafe condition described in the MCAI and 
service information described above. The FAA is issuing this NPRM after 
determining that the unsafe condition described previously is likely to 
exist or develop on other products of the same type design.

Proposed Requirements of This NPRM

    This proposed AD would retain none of the requirements of AD 2005-
15-11; certain requirements of AD 2016-07-09; and all requirements of 
AD 2018-19-24. This proposed AD would require revising the existing 
maintenance or inspection program, as applicable, to incorporate new or 
more restrictive airworthiness limitations.
    This proposed AD would require revisions to certain operator 
maintenance documents to include new actions (e.g., inspections) and 
Critical Design Configuration Control Limitations (CDCCLs). Compliance 
with these actions and CDCCLs is required by 14 CFR 91.403(c). For 
airplanes that have been previously modified, altered, or repaired in 
the areas addressed by this proposed 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 
(o)(1) of this proposed AD.

Costs of Compliance

    The FAA estimates that this AD, if adopted as proposed, would 
affect 10 airplanes of U.S. registry. The FAA estimates the following 
costs to comply with this proposed AD:
    The FAA estimates the total cost per operator for the retained 
actions from AD 2016-07-09 to be $7,650 (90 work-hours x $85 per work-
hour).
    The FAA estimates the total cost per operator for the retained 
maintenance or inspection program revision from AD 2018-19-24 to be 
$7,650 (90 work-hours x $85 per work-hour)
    The FAA has determined that revising the maintenance or inspection 
program takes an average of 90 work-hours per operator, although the 
agency recognizes that this number may vary from operator to operator. 
Since operators incorporate maintenance or inspection program changes 
for their affected fleet(s), the FAA has determined that a per-operator 
estimate is more accurate than a per-airplane estimate. Therefore, the 
agency estimates the average total cost per operator to be $7,650 (90 
work-hours x $85 per work-hour).
    The FAA estimates the total cost per operator for the new proposed 
actions to be $7,650 (90 work-hours x $85 per work-hour).

[[Page 63976]]



                                      Estimated Costs for Required Actions
----------------------------------------------------------------------------------------------------------------
                                                                                     Cost per      Cost on U.S.
                Action                         Labor cost           Parts cost        product        operators
----------------------------------------------------------------------------------------------------------------
Inspection (Retained actions from AD    2 work-hours x $85 per                $0            $170          $1,700
 2018-19-24).                            hour = $170.
----------------------------------------------------------------------------------------------------------------

    The FAA has received no definitive data on which to base the cost 
estimates for the on-condition actions specified in this AD.

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.
    The FAA is 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

    The FAA 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) Would not affect intrastate aviation in Alaska, and
    (3) Would not have a significant economic impact, positive or 
negative, on a substantial number of small entities under the criteria 
of the Regulatory Flexibility Act.

List of Subjects in 14 CFR Part 39

    Air transportation, Aircraft, Aviation safety, Incorporation by 
reference, Safety.

The Proposed Amendment

    Accordingly, under the authority delegated to me by the 
Administrator, the FAA proposes to amend 14 CFR part 39 as follows:

PART 39--AIRWORTHINESS DIRECTIVES

0
1. The authority citation for part 39 continues to read as follows:

    Authority: 49 U.S.C. 106(g), 40113, 44701.


Sec.  39.13  [Amended]

0
2. The FAA amends Sec.  39.13 by:
0
a. Removing Airworthiness Directive AD 2005-15-11, Amendment 39-14200 
(70 FR 43025, July 26, 2005); AD 2016-07-09, Amendment 39-18454 (81 FR 
21263, April 11, 2016); and AD 2018-19-24, Amendment 39-19425 (83 FR 
49786, October 3, 2018); and
0
b. Adding the following new airworthiness directive:

BAE Systems (Operations) Limited: Docket No. FAA-2022-1298; Project 
Identifier MCAI-2022-00437-T.

(a) Comments Due Date

    The FAA must receive comments on this airworthiness directive 
(AD) by December 5, 2022.

(b) Affected ADs

    (1) This AD replaces AD 2005-15-11, Amendment 39-14200 (70 FR 
43025, July 26, 2005) (AD 2005-15-11).
    (2) This AD replaces AD 2016-07-09, Amendment 39-18454 (81 FR 
21263, April 11, 2016) (AD 2016-07-09).
    (3) This AD replaces AD 2018-19-24, Amendment 39-19425 (83 FR 
49786, October 3, 2018) (AD 2018-19-24).

(c) Applicability

    This AD applies to all BAE Systems (Operations) Limited Model 
4101 airplanes, certificated in any category.

(d) Subject

    Air Transport Association (ATA) of America Code 05, Time Limits/
Maintenance Checks.

(e) Reason

    This AD was prompted by a determination that new or more 
restrictive airworthiness limitations are necessary. The FAA is 
issuing this AD to address fatigue damage of various airplane 
structures and failure of certain structurally significant items, 
which could result in reduced structural integrity of the airplane. 
The FAA is also issuing this AD to address fuel vapor ignition 
sources, which could result in a fuel tank explosion and consequent 
loss of the airplane.

(f) Compliance

    Comply with this AD within the compliance times specified, 
unless already done.

(g) Retained Revision of the Maintenance or Inspection Program (From AD 
2016-07-09), With No Changes

    This paragraph restates the requirements of paragraph (i) of AD 
2016-07-09, with no changes. Within 90 days after May 16, 2016 (the 
effective date of AD 2016-07-09): Revise the maintenance or 
inspection program, as applicable, by incorporating Subjects 05-10-
10, ``Airworthiness Limitations''; 05-10-20, ``Certification 
Maintenance Requirements''; and 05-10-30, ``Critical Design 
Configuration Control Limitations (CDCCL)--Fuel System''; of Chapter 
05, ``Airworthiness Limitations,'' of the BAE Systems (Operations) 
Limited J41 AMM, Revision 38, dated September 15, 2013. The initial 
compliance times for the tasks are at the applicable times specified 
in paragraphs (g)(1) through (3) of this AD. Accomplishing the 
revision of the existing maintenance or inspection program required 
by paragraph (m) of this AD terminates the requirements of this 
paragraph.
    (1) For replacement tasks of life limited parts specified in 
Subject 05-10-10, ``Airworthiness Limitations,'' of Chapter 05, 
``Airworthiness Limitations,'' of the BAE Systems (Operations) 
Limited J41 AMM, Revision 38, dated September 15, 2013: Prior to the 
applicable flight cycles (landings) or flight hours (flying hours) 
on the part specified in the ``Mandatory Life Limits'' column in 
Subject 05-10-10, or within 90 days after May 16, 2016 (the 
effective date of AD 2016-07-09), whichever occurs later.
    (2) For structurally significant item tasks specified in Subject 
05-10-10, ``Airworthiness Limitations,'' of Chapter 05, 
``Airworthiness Limitations,'' of the BAE Systems (Operations) 
Limited J41 AMM, Revision 38, dated September 15, 2013: Prior to the 
accumulation of the applicable flight cycles specified in the 
``Initial Inspection'' column in Subject 05-10-10, or within 90 days 
after May 16, 2016 (the effective date of AD 2016-07-09), whichever 
occurs later.
    (3) For certification maintenance requirements tasks specified 
in Subject 05-10-20, ``Certification Maintenance Requirements,'' of 
Chapter 05, ``Airworthiness Limitations,'' of the BAE Systems 
(Operations) Limited J41 AMM, Revision 38, dated September 15, 2013: 
Prior to the accumulation of the applicable flight hours specified 
in the ``Time Between Checks'' column in Subject 05-10-20, or within 
90 days after May 16, 2016 (the effective date of AD 2016-07-09), 
whichever occurs later; except for tasks that specify ``first flight 
of the day'' in the ``Time Between Checks'' column in Subject 05-10-
20, the

[[Page 63977]]

initial compliance time is the first flight of the next day after 
doing the revision required by paragraph (g) of AD 2016-07-09, or 
within 90 days after May 16, 2016, whichever occurs later.

(h) Retained Restrictions on Alternative Actions, Intervals, and/or 
(CDCCLs), With No Changes

    This paragraph restates the requirements of paragraph (j) of AD 
2016-07-09, with no changes. Except as required by paragraph (m) of 
this AD, after the maintenance or inspection program, as applicable, 
has been revised as required by paragraph (g) of this AD, no 
alternative actions (e.g., inspections), intervals, and/or CDCCLs 
may be used unless the actions, intervals, and/or CDCCLs are 
approved as an alternative method of compliance (AMOC) in accordance 
with the procedures specified in paragraph (o)(1) of this AD.

(i) Retained Inspection, With No Changes

    This paragraph restates the requirements of paragraph (g) of AD 
2018-19-24, with no changes. At the compliance times specified in 
paragraphs (i)(1) and (2) of this AD, as applicable: Do a detailed 
inspection of fuselage frame 90 for cracking or fatigue damage, in 
accordance with the Accomplishment Instructions of BAE Systems 
(Operations) Limited Alert Service Bulletin J41-A53-058, dated 
December 6, 2016. If any cracking or fatigue damage is found: Before 
further flight, repair using a method approved by the Manager, 
International Section, Transport Standards Branch, FAA; or the 
European Aviation Safety Agency (EASA); or BAE Systems (Operations) 
Limited's EASA Design Organization Approval (DOA). Accomplishing the 
revision of the existing maintenance or inspection program required 
by paragraph (m) of this AD terminates the requirements of this 
paragraph.
    (1) For airplanes with 6,300 flight cycles or fewer since 
Structural Significant Items (SSI) 53-10-029 (Maintenance Planning 
Document (MPD) 531029-DVl-10010-1) was last accomplished: Within 
6,600 flight cycles after the last accomplishment of SSI 53-10-029 
(MPD 531029-DVl-10010-1), or within 6 months after November 7, 2018 
(the effective date of AD 2018-19-24), whichever is later.
    (2) For airplanes with more than 6,300 flight cycles since SSI 
53-10-029 (MPD 531029-DVl-10010-1) was last accomplished: Within 300 
flight cycles or 4.5 months, whichever is earlier, since the last 
accomplishment of SSI 53-10-029 (MPD 531029-DVl-10010-1), or within 
6 months after November 7, 2018 (the effective date of AD 2018-19-
24), whichever is later.

(j) Retained Revision of Maintenance or Inspection Program (From AD 
2018-19-24), With No Changes

    This paragraph restates the requirements of paragraph (h) of AD 
2018-19-24, with no changes. Within 90 days after November 7, 2018 
(the effective date of AD 2018-19-24): Revise the maintenance or 
inspection program, as applicable, by incorporating the maintenance 
tasks and associated thresholds and intervals described in, and in 
accordance with, the Accomplishment Instructions of BAE Systems 
(Operations) Limited Service Bulletin J41-51-001, Revision 4, dated 
July 11, 2017. The initial compliance times for new or revised tasks 
are at the applicable times specified in BAE Systems (Operations) 
Limited Service Bulletin J41-51-001, Revision 4, dated July 11, 
2017, or within 6 months after November 7, 2018, whichever is later. 
Accomplishing the revision of the existing maintenance or inspection 
program required by paragraph (m) of this AD terminates the 
requirements of this paragraph.

(k) Retained No Alternative Actions and Intervals, With No Changes

    This paragraph restates the requirements of paragraph (i) of AD 
2018-19-24, with no changes. Except as required by paragraph (m) of 
this AD: After the maintenance or inspection program has been 
revised as required by paragraph (j) of this AD, no alternative 
actions (e.g., inspections) or intervals may be used unless the 
actions or intervals are approved as an AMOC in accordance with the 
procedures specified in paragraph (o)(1) of this AD.

(l) Retained No Reporting Requirement, With No Changes

    This paragraph restates the requirements of paragraph (k) of AD 
2018-19-24, with no changes. Although the Accomplishment 
Instructions of BAE Systems (Operations) Limited Alert Service 
Bulletin J41-A53-058, dated December 6, 2016, specify to submit 
certain information to the manufacturer, this AD does not include 
that requirement.

(m) New Revision of the Existing Maintenance or Inspection Program

    Within 90 days after the effective date of this AD: Revise the 
existing maintenance or inspection program, as applicable, by 
incorporating Subjects 05-10-10, ``Airworthiness Limitations''; 05-
10-20, ``Certification Maintenance Requirements''; and 05-10-30, 
``Critical Design Configuration Control Limitations (CDCCL)--Fuel 
System''; of Chapter 05, ``Airworthiness Limitations,'' of the BAE 
Systems (Operations) Limited J41 AMM, Revision 44, dated June 15, 
2021, for effectivity group 403; or BAE Systems (Operations) Limited 
J41 AMM, Revision 44, dated June 15, 2021, for effectivity group 
408; as applicable. The initial compliance times for the tasks are 
at the applicable times specified in paragraphs (m)(1) through (3) 
of this AD. Accomplishing the revision of the existing maintenance 
or inspection program required by this paragraph terminates the 
actions required by paragraphs (g), (i) and (j) of this AD.
    (1) For replacement tasks of life limited parts specified in 
Subject 05-10-10, ``Airworthiness Limitations,'' of Chapter 05, 
``Airworthiness Limitations,'' of the BAE Systems (Operations) 
Limited J41 AMM, Revision 44, dated June 15, 2021, for effectivity 
group 403; or BAE Systems (Operations) Limited J41 AMM, Revision 44, 
dated June 15, 2021, for effectivity group 408; as applicable: Prior 
to the applicable flight cycles (landings) or flight hours (flying 
hours) on the part specified in the ``Mandatory Life Limits'' column 
in Subject 05-10-10, or within 90 days after the effective date of 
this AD, whichever occurs later.
    (2) For structurally significant item tasks specified in Subject 
05-10-10, ``Airworthiness Limitations,'' of Chapter 05, 
``Airworthiness Limitations,'' of the BAE Systems (Operations) 
Limited J41 AMM, Revision 44, dated June 15, 2021, for effectivity 
group 403; or BAE Systems (Operations) Limited J41 AMM, Revision 44, 
dated June 15, 2021. for effectivity group 408; as applicable: Prior 
to the accumulation of the applicable flight cycles specified in the 
``Initial Inspection'' column in Subject 05-10-10, or within 90 days 
after the effective date of this AD, whichever occurs later.
    (3) For certification maintenance requirements tasks specified 
in Subject 05-10-20, ``Certification Maintenance Requirements,'' of 
Chapter 05, ``Airworthiness Limitations,'' of the BAE Systems 
(Operations) Limited J41 AMM, Revision 44, dated June 15, 2021, for 
effectivity group 403; or BAE Systems (Operations) Limited J41 AMM, 
Revision 44, dated June 15, 2021, for effectivity group 408; as 
applicable: Prior to the accumulation of the applicable flight hours 
specified in the ``Time Between Checks'' column in Subject 05-10-20, 
or within 90 days after the effective date of this AD, whichever 
occurs later; except for tasks that specify ``first flight of the 
day'' in the ``Time Between Checks'' column in Subject 05-10-20, the 
initial compliance time is the first flight of the next day after 
accomplishing the revision required by paragraph (m) of this AD, or 
within 90 days after the effective date of this AD, whichever occurs 
later.

(n) New No Alternative Actions, Intervals, or Critical Design 
Configuration Control Limitations (CDCCLs)

    After the existing maintenance or inspection program has been 
revised as required by paragraph (m) of this AD, no alternative 
actions (e.g., inspections), intervals, or CDCCLs may be used unless 
the actions, intervals, and CDCCLs are approved as an AMOC in 
accordance with the procedures specified in paragraph (o)(1) of this 
AD.

(o) Additional AD Provisions

    The following provisions also apply to this AD:
    (1) Alternative Methods of Compliance (AMOCs): The Manager, 
International Validation Branch, FAA, has the authority to approve 
AMOCs for this AD, if requested using the procedures found in 14 CFR 
39.19. In accordance with 14 CFR 39.19, send your request to your 
principal inspector or responsible Flight Standards Office, as 
appropriate. If sending information directly to the International 
Validation Branch, send it to the attention of the person identified 
in paragraph (p)(2) of this AD. Information may be emailed to: [email protected]. Before using any approved AMOC, notify 
your appropriate principal inspector, or lacking a principal 
inspector, the manager of the responsible Flight Standards Office.
    (2) Contacting the Manufacturer: For any requirement in this AD 
to obtain instructions from a manufacturer, the instructions must

[[Page 63978]]

be accomplished using a method approved by the Manager, 
International Validation Branch, FAA; or the United Kingdom Civil 
Aviation Authority (U.K. CAA); or BAE Systems (Operations) Limited's 
U.K. CAA Design Organization Approval (DOA). If approved by the DOA, 
the approval must include the DOA-authorized signature.

(p) Additional Information

    (1) Refer to U.K. CAA AD G-2022-0006, dated March 30, 2022, for 
related information. This U.K. CAA AD may be found in the AD docket 
at regulations.gov under Docket No. FAA-2022-1298.
    (2) For more information about this AD, contact Todd Thompson, 
Aerospace Engineer, Large Aircraft Section, FAA, International 
Validation Branch, 2200 South 216th St., Des Moines, WA 98198; 
telephone 206-231-3228; email [email protected].

(q) 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 this AD specifies otherwise.
    (3) The following service information was approved for IBR.
    (i) Chapter 05 of BAE Systems (Operations) Limited J41 Aircraft 
Maintenance Manual (AMM), Revision 44, dated June 15, 2021, for 
effectivity group 403;
    (ii) Chapter 05 of BAE Systems (Operations) Limited J41 AMM, 
Revision 44, dated June 15, 2021, for effectivity group 408.
    (4) The following service information was approved for IBR on 
November 7, 2018 (83 FR 49786, October 3, 2018).
    (i) BAE Systems (Operations) Limited Alert Service Bulletin J41-
A53-058, dated December 6, 2016.
    (ii) BAE Systems (Operations) Limited Service Bulletin J41-51-
001, Revision 4, dated July 11, 2017.
    (5) The following service information was approved for IBR on 
May 16, 2016 (81 FR 21263, April 11, 2016).
    (i) Chapter 05, ``Airworthiness Limitations,'' of the BAE 
Systems (Operations) Limited J41 Aircraft Maintenance Manual (AMM), 
Revision 38, dated September 15, 2013. Page 1 of the ``Publications 
Transmittal'' is the only page that shows the revision level of this 
document.
    (A) Subject 05-10-10, ``Airworthiness Limitations.''
    (B) Subject 05-10-20, ``Certification Maintenance 
Requirements.''
    (C) Subject 05-10-30, ``Critical Design Configuration Control 
Limitations (CDCCL)--Fuel System.''
    (ii) [Reserved]
    (6) For service information identified in this AD, contact BAE 
Systems (Operations) Limited, Customer Information Department, 
Prestwick International Airport, Ayrshire, KA9 2RW, Scotland, United 
Kingdom; telephone +44 1292 675207; fax +44 1292 675704; email 
[email protected]; website baesystems.com/Businesses/RegionalAircraft/index.htm.
    (7) You may view this service information at the FAA, 
Airworthiness Products Section, Operational Safety Branch, 2200 
South 216th St., Des Moines, WA. For information on the availability 
of this material at the FAA, call 206-231-3195.
    (8) 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, email [email protected], or go to: www.archives.gov/federal-register/cfr/ibr-locations.html.

    Issued on October 6, 2022.
Christina Underwood,
Acting Director, Compliance & Airworthiness Division, Aircraft 
Certification Service.
[FR Doc. 2022-22202 Filed 10-20-22; 8:45 am]
BILLING CODE 4910-13-P
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