Airworthiness Directives; Dassault Aviation Airplanes, 77532-77535 [2022-27298]

Download as PDF 77532 Federal Register / Vol. 87, No. 242 / Monday, December 19, 2022 / Proposed Rules Authority: 15 U.S.C. 632(p), (q), 634(b)(6), 637, 644, 657f, 657q, 657r, and 657s; 38 U.S.C. 501 and 8127. 2. Amend § 125.3 by: a. Removing the number ‘‘$650,000’’ in paragraph (a) introductory text and adding in its place the number ‘‘$750,000’’; ■ b. Revising paragraph (a)(1)(i)(C); ■ c. Removing the word ‘‘and’’ after the semicolon at the end of paragraph (c)(1)(xi); ■ d. Redesignating paragraph (c)(1)(xii) as paragraph (c)(1)(xiii); and ■ e. Adding a new paragraph (c)(1)(xii). The revision and addition read as follows: ■ ■ tkelley on DSK125TN23PROD with PROPOSALS § 125.3 What types of subcontracting assistance are available to small businesses? (a) * * * (1) * * * (i) * * * (C) Where the subcontracting goals pertain only to a single contract with one Federal agency, the contractor may elect to receive credit for small business concerns performing as first-tier subcontractors or subcontractors at any tier pursuant to the subcontracting plans required under paragraph (c) of this section in an amount equal to the dollar value of work awarded to such small business concerns. The election must be recorded in the subcontracting plan. If the contractor elects to receive credit for subcontractors at any tier, the following requirements apply: (1) The prime contractor must incorporate the subcontracting-plan goals of their lower-tier subcontractors in its individual-subcontracting-plan goals. (2) To receive credit for their subcontracting, lower-tier subcontractors must have their own individual subcontracting plans. (3) The prime contractor and any subcontractor with a subcontracting plan are responsible for reporting on subcontracting performance under their contracts or subcontracts at their first tier. This reporting method applies to both individual subcontracting reports and summary subcontracting reports. (4) The prime contractor’s performance under its individual subcontracting plan will be calculated by aggregating the prime contractor’s first-tier subcontracting achievements with the achievements of the prime contractor’s lower-tier subcontractors that have flow-down subcontracting plans. (5) If the subcontracting goals pertain to more than one contract with one or more Federal agencies, or to one contract with more than one Federal VerDate Sep<11>2014 17:45 Dec 16, 2022 Jkt 259001 agency, the prime contractor shall only receive credit for first tier subcontractors that are small business concerns. This restriction applies to all commercial plans, all comprehensive subcontracting plans with the Department of Defense, governmentwide contracts, and multiagency contracts. * * * * * (c) * * * (1) * * * (xii) The prime contractor must provide a written statement of the types of records it will maintain to demonstrate that procedures have been adopted to substantiate the subcontracting credit that the prime contractor elects under paragraph (a)(1)(i)(C) of this section; and * * * * * Isabella Casillas Guzman, Administrator. [FR Doc. 2022–27213 Filed 12–16–22; 8:45 am] BILLING CODE 8026–09–P DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA–2022–1585; Project Identifier MCAI–2022–00892–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 supersede Airworthiness Directive (AD) 2021–03–11, which applies to all Dassault Aviation Model FALCON 2000 airplanes. AD 2021–03–11 requires revising the existing maintenance or inspection program, as applicable, to incorporate new or more restrictive airworthiness limitations. Since the FAA issued AD 2021–03–11, the FAA has determined that new or more restrictive airworthiness limitations are necessary. This proposed AD would continue to require the actions in AD 2021–03–11 and would require revising the existing maintenance or inspection program, as applicable, to incorporate new or more restrictive airworthiness limitations, 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. SUMMARY: PO 00000 Frm 00004 Fmt 4702 Sfmt 4702 The FAA must receive comments on this proposed AD by February 2, 2023. DATES: 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–2022–1585; 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 at regulations.gov under Docket No. FAA– 2022–1585. • 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: Tom Rodriguez, Aerospace Engineer, Large Aircraft Section, International Validation Branch, FAA, 2200 South 216th St., Des Moines, WA 98198; telephone 206–231–3226; email Tom.Rodriguez@faa.gov. SUPPLEMENTARY INFORMATION: ADDRESSES: 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–2022–1585; Project Identifier MCAI–2022–00892–T’’ at the beginning of your comments. The most helpful comments reference a specific portion of E:\FR\FM\19DEP1.SGM 19DEP1 Federal Register / Vol. 87, No. 242 / Monday, December 19, 2022 / Proposed Rules 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 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. tkelley on DSK125TN23PROD with PROPOSALS 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 Tom Rodriguez, Aerospace Engineer, Large Aircraft Section, International Validation Branch, FAA, 2200 South 216th St., Des Moines, WA 98198; telephone 206–231– 3226; email Tom.Rodriguez@faa.gov. 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 2021–03–11, Amendment 39–21414 (86 FR 11116, February 24, 2021) (AD 2021–03–11), for all Dassault Aviation Model FALCON 2000 airplanes. AD 2021–03– 11 was prompted by an MCAI originated by EASA, which is the Technical Agent for the Member States of the European Union. EASA issued AD 2020–0113, dated May 20, 2020 (EASA AD 2020– 0113) (which corresponds to FAA AD 2021–03–11), to correct an unsafe condition. AD 2021–03–11 requires revising the existing maintenance or inspection program, as applicable, to incorporate new or more restrictive airworthiness limitations. The FAA issued AD 2021– VerDate Sep<11>2014 17:45 Dec 16, 2022 Jkt 259001 03–11 to address reduced controllability of the airplane. AD 2021–03–11 specifies that accomplishing the revision required by that AD terminates all requirements of AD 2010–26–05, Amendment 39–16544 (75 FR 79952, December 21, 2010) (AD 2010–26–05) for Model FALCON 2000 airplanes only. This proposed AD would therefore continue allowing that termination. Actions Since AD 2021–03–11 Was Issued Since the FAA issued AD 2021–03– 11, EASA superseded AD 2020–0113 and issued EASA AD 2022–0135, dated July 6, 2022 (EASA AD 2022–0135) (referred to after this as the MCAI), for all Dassault Aviation Model FALCON 2000 airplanes. The MCAI states that new or more restrictive airworthiness limitations have been developed. The FAA is proposing this AD to address reduced controllability of the airplane. You may examine the MCAI in the AD docket at regulations.gov under Docket No. FAA–2022–1585. Related Service Information Under 1 CFR Part 51 The FAA reviewed EASA AD 2022– 0135. This service information specifies new or more restrictive airworthiness limitations for airplane structures and safe life limits. This proposed AD would also require EASA AD 2020–0113, which the Director of the Federal Register approved for incorporation by reference as of March 31, 2021 (86 FR 11116, February 24, 2021). This material is reasonably available because the interested parties have access to it through their normal course of business or by the means identified in ADDRESSES. 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 described above. The FAA is issuing this NPRM after determining that the unsafe condition described previously is likely to exist or develop in other products of the same type design. Proposed AD Requirements in This NPRM This proposed AD would retain all of the requirements of AD 2021–03–11. This proposed AD would also require revising the existing maintenance or inspection program, as applicable, to PO 00000 Frm 00005 Fmt 4702 Sfmt 4702 77533 incorporate additional new or more restrictive airworthiness limitations, which are specified in EASA AD 2022– 0135 already described, as proposed for incorporation by reference. Any differences with EASA AD 2022–0135 are identified as exceptions in the regulatory text of this AD. This proposed AD would require revisions to certain operator maintenance documents to include new actions (e.g., inspections). Compliance with these actions is required by 14 CFR 91.403(c). For airplanes that have been previously modified, altered, or repaired in the areas addressed by this 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 (AMOC) according to paragraph (n)(1) of this proposed AD. Explanation of Required Compliance Information In the FAA’s ongoing efforts to improve the efficiency of the AD process, the FAA developed a process to use some civil aviation authority (CAA) ADs as the primary source of information for compliance with requirements for corresponding FAA ADs. The FAA has been coordinating this process with manufacturers and CAAs. As a result, the FAA proposes to retain the IBR of EASA AD 2020–0113 and incorporate EASA AD 2022–0135 by reference in the FAA final rule. This proposed AD would, therefore, require compliance with EASA AD 2022–0135 and EASA AD 2020–0113 through that incorporation, except for any differences identified as exceptions in the regulatory text of this proposed AD. Using common terms that are the same as the heading of a particular section in EASA AD 2022–0135 or EASA AD 2020–0113 does not mean that operators need comply only with that section. For example, where the AD requirement refers to ‘‘all required actions and compliance times,’’ compliance with this AD requirement is not limited to the section titled ‘‘Required Action(s) and Compliance Time(s)’’ in EASA AD 2022–0135 or EASA AD 2020–0113. Service information required by EASA AD 2022–0135 and EASA AD 2020– 0113 for compliance will be available at regulations.gov by searching for and locating Docket No. FAA–2022–1585 after the FAA final rule is published. Airworthiness Limitation ADs Using the New Process The FAA’s process of incorporating by reference MCAI ADs as the primary E:\FR\FM\19DEP1.SGM 19DEP1 77534 Federal Register / Vol. 87, No. 242 / Monday, December 19, 2022 / Proposed Rules source of information for compliance with corresponding FAA ADs has been limited to certain MCAI ADs (primarily those with service bulletins as the primary source of information for accomplishing the actions required by the FAA AD). However, the FAA is now expanding the process to include MCAI ADs that require a change to airworthiness limitation documents, such as airworthiness limitation sections. For these ADs that incorporate by reference an MCAI AD that changes airworthiness limitations, the FAA requirements are unchanged. Operators must revise the existing maintenance or inspection program, as applicable, to incorporate the information specified in the new airworthiness limitation document. The airworthiness limitations must be followed according to 14 CFR 91.403(c) and 91.409(e). The previous format of the airworthiness limitation ADs included a paragraph that specified that 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 the AMOCs paragraph under ‘‘Additional AD Provisions.’’ This new format includes a ‘‘New Provisions for Alternative Actions and Intervals’’ paragraph that does not specifically refer to AMOCs, but operators may still request an AMOC to use an alternative action or interval. tkelley on DSK125TN23PROD with PROPOSALS Costs of Compliance The FAA estimates that this AD, if adopted as proposed, would affect 168 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 2021–03–11 to be $7,650 (90 workhours × $85 per work-hour). The FAA has determined that revising the existing maintenance or inspection program takes an average of 90 workhours per operator, although the agency recognizes that this number may vary from operator to operator. In the past, the agency has estimated that this action takes 1 work-hour per airplane. 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. The FAA estimates the total cost per operator for the new proposed actions to be $7,650 (90 work-hours × $85 per work-hour). VerDate Sep<11>2014 17:45 Dec 16, 2022 Jkt 259001 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 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: PO 00000 Frm 00006 Fmt 4702 Sfmt 4702 a. Removing Airworthiness Directive (AD) 2021–03–11, Amendment 39– 21414 (86 FR 11116, February 24, 2021); and ■ b. Adding the following new AD: ■ Dassault Aviation: Docket No. FAA–2022– 1585; Project Identifier MCAI–2022– 00892–T. (a) Comments Due Date The FAA must receive comments on this airworthiness directive (AD) by February 2, 2023. (b) Affected ADs (1) This AD replaces AD 2021–03–11, Amendment 39–21414 (86 FR 11116, February 24, 2021) (AD 2021–03–11). (2) This AD affects AD 2010–26–05, Amendment 39–16544 (75 FR 79952, December 21, 2010) (AD 2010–26–05). (c) Applicability This AD applies to all Dassault Aviation Model FALCON 2000 airplanes, certificated in any category. (d) Subject Air Transport Association (ATA) of America Code 05, Time Limits/Maintenance Checks. (e) Unsafe Condition This AD was prompted by a determination that new or more restrictive airworthiness limitations are necessary. The FAA is issuing this AD to address reduced controllability of the airplane. (f) Compliance Comply with this AD within the compliance times specified, unless already done. (g) Retained Revision of the Existing Maintenance or Inspection Program, With No Changes This paragraph restates the requirements of paragraph (i) of AD 2021–03–11, with no changes. Except as specified in paragraph (h) of this AD: Comply with all required actions and compliance times specified in, and in accordance with, European Union Aviation Safety Agency (EASA) AD 2020–0113, dated May 20, 2020 (EASA AD 2020–0113). Accomplishing the revision of the existing maintenance or inspection program required by paragraph (j) of this AD terminates the requirements of this paragraph. (h) Retained Exceptions to EASA AD 2020– 0113, With No Changes This paragraph restates the exceptions specified in paragraph (j) of AD 2021–03–11, with no changes. (1) The requirements specified in paragraphs (1) and (2) of EASA AD 2020– 0113 do not apply to this AD. (2) Paragraph (3) of EASA AD 2020–0113 specifies revising ‘‘the approved AMP’’ within 12 months after its effective date, but this AD requires revising the existing maintenance or inspection program, as applicable, to incorporate the ‘‘limitations, tasks and associated thresholds and intervals’’ specified in paragraph (3) of EASA E:\FR\FM\19DEP1.SGM 19DEP1 Federal Register / Vol. 87, No. 242 / Monday, December 19, 2022 / Proposed Rules AD 2020–0113 within 90 days after the effective date of this AD. (3) The initial compliance time for doing the tasks specified in paragraph (3) of EASA AD 2020–0113 is at the applicable ‘‘associated thresholds’’ specified in paragraph (3) of EASA AD 2020–0113, or within 90 days after the effective date of this AD, whichever occurs later. (4) The provisions specified in paragraphs (4) and (5) of EASA AD 2020–0113 do not apply to this AD. (5) The ‘‘Remarks’’ section of EASA AD 2020–0113 does not apply to this AD. (i) Retained No Alternative Actions or Intervals With a New Exception This paragraph restates the requirements of paragraph (k) of AD 2021–03–11, with a new exception. Except as required by paragraph (j) of this AD, after the existing maintenance or inspection program has been revised as required by paragraph (g) of this AD, no alternative actions (e.g., inspections) or intervals may be used unless they are approved as specified in the provisions of the ‘‘Ref. Publications’’ section of EASA AD 2020–0113. (j) New Maintenance or Inspection Program Revision Except as specified in paragraph (k) of this AD: Comply with all required actions and compliance times specified in, and in accordance with, EASA AD 2022–0135, dated July 6, 2022 (EASA AD 2022–0135). Accomplishing the maintenance or inspection program revision required by this paragraph terminates the requirements of paragraph (g) of this AD. tkelley on DSK125TN23PROD with PROPOSALS (k) Exceptions to EASA AD 2022–0135 (1) The requirements specified in paragraphs (1) and (2) of EASA AD 2022– 0135 do not apply to this AD. (2) Paragraph (3) of EASA AD 2022–0135 specifies revising ‘‘the approved AMP’’ within 12 months after its effective date, but this AD requires revising the existing maintenance or inspection program, as applicable, within 90 days after the effective date of this AD. (3) The initial compliance time for doing the tasks specified in paragraph (3) of EASA AD 2022–0135 is at the applicable ‘‘limitations’’ and ‘‘associated thresholds’’ as incorporated by the requirements of paragraph (3) of EASA AD 2022–0135, or within 90 days after the effective date of this AD, whichever occurs later. (4) The provisions specified in paragraphs (4) and (5) of EASA AD 2022–0135 do not apply to this AD. (5) The ‘‘Remarks’’ section of EASA AD 2022–0135 does not apply to this AD. (l) New Provisions for Alternative Actions and Intervals After the existing maintenance or inspection program has been revised as required by paragraph (j) of this AD, no alternative actions (e.g., inspections), and intervals are allowed unless they are approved as specified in the provisions of the ‘‘Ref. Publications’’ section of EASA AD 2022–0135. VerDate Sep<11>2014 17:45 Dec 16, 2022 Jkt 259001 (m) Terminating Action for AD 2010–26–05 Accomplishing the actions required by paragraph (g) or (j) of this AD terminates the requirements of paragraph (g) of AD 2010– 26–05 for Model FALCON 2000 airplanes only. (n) 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 (o) 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 be accomplished using a method approved by the Manager, International Validation Branch, FAA; or EASA; or Dassault Aviation’s EASA Design Organization Approval (DOA). If approved by the DOA, the approval must include the DOAauthorized signature. (o) Additional Information For more information about this AD, contact Tom Rodriguez, Aerospace Engineer, Large Aircraft Section, International Validation Branch, FAA, 2200 South 216th St., Des Moines, WA 98198; telephone 206– 231–3226; email Tom.Rodriguez@faa.gov. (p) 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 on [DATE 35 DAYS AFTER PUBLICATION OF THE FINAL RULE]. (i) European Union Aviation Safety Agency (EASA) AD 2022–0135, dated July 6, 2022. (ii) [Reserved] (4) The following service information was approved for IBR on March 31, 2021 (86 FR 11116, February 24, 2021). (i) European Union Aviation Safety Agency (EASA) AD 2020–0113, dated May 20, 2020. (ii) [Reserved] (5) For EASA ADs 2022–0135 and 2020– 0113, 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 these EASA ADs on the EASA website at ad.easa.europa.eu. (6) You may view this service information at the FAA, Airworthiness Products Section, PO 00000 Frm 00007 Fmt 4702 Sfmt 4702 77535 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. (7) 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 December 12, 2022. Christina Underwood, Acting Director, Compliance & Airworthiness Division, Aircraft Certification Service. [FR Doc. 2022–27298 Filed 12–16–22; 8:45 am] BILLING CODE 4910–13–P DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA–2022–1645; Project Identifier MCAI–2022–00734–T] RIN 2120–AA64 Airworthiness Directives; Airbus SAS Airplanes Federal Aviation Administration (FAA), DOT. ACTION: Notice of proposed rulemaking (NPRM). AGENCY: The FAA proposes to supersede Airworthiness Directive (AD) 2020–21–10, which applies to certain Airbus SAS Model A318, A320, and A321 series airplanes; and Model A319– 111, –112, –113, –114, –115, –131, –132, –133, –151N, and –153N airplanes; and AD 2022–07–08, which applies to all Airbus SAS Model A318, A319, A320 and A321 series airplanes. AD 2020–21– 10 and AD 2022–07–08 require revising the existing maintenance or inspection program, as applicable, to incorporate new or more restrictive airworthiness limitations. Since the FAA issued AD 2020–21–10 and AD 2022–07–08, the FAA has determined that new or more restrictive airworthiness limitations are necessary. This proposed AD would continue to require the actions in AD 2020–21–10 and AD 2022–07–08 and require revising the existing maintenance or inspection program, as applicable, to incorporate additional new or more restrictive airworthiness limitations, 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. SUMMARY: E:\FR\FM\19DEP1.SGM 19DEP1

Agencies

[Federal Register Volume 87, Number 242 (Monday, December 19, 2022)]
[Proposed Rules]
[Pages 77532-77535]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2022-27298]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2022-1585; Project Identifier MCAI-2022-00892-T]
RIN 2120-AA64


Airworthiness Directives; Dassault Aviation Airplanes

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Notice of proposed rulemaking (NPRM).

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

SUMMARY: The FAA proposes to supersede Airworthiness Directive (AD) 
2021-03-11, which applies to all Dassault Aviation Model FALCON 2000 
airplanes. AD 2021-03-11 requires revising the existing maintenance or 
inspection program, as applicable, to incorporate new or more 
restrictive airworthiness limitations. Since the FAA issued AD 2021-03-
11, the FAA has determined that new or more restrictive airworthiness 
limitations are necessary. This proposed AD would continue to require 
the actions in AD 2021-03-11 and would require revising the existing 
maintenance or inspection program, as applicable, to incorporate new or 
more restrictive airworthiness limitations, 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 February 2, 
2023.

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-2022-1585; 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 [email protected]; website easa.europa.eu. You 
may find this material on the EASA website at ad.easa.europa.eu. It is 
also available at regulations.gov under Docket No. FAA-2022-1585.
     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: Tom Rodriguez, Aerospace Engineer, 
Large Aircraft Section, International Validation Branch, FAA, 2200 
South 216th St., Des Moines, WA 98198; telephone 206-231-3226; 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-2022-1585; Project Identifier 
MCAI-2022-00892-T'' at the beginning of your comments. The most helpful 
comments reference a specific portion of

[[Page 77533]]

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 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 Tom 
Rodriguez, Aerospace Engineer, Large Aircraft Section, International 
Validation Branch, FAA, 2200 South 216th St., Des Moines, WA 98198; 
telephone 206-231-3226; 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 2021-03-11, Amendment 39-21414 (86 FR 11116, 
February 24, 2021) (AD 2021-03-11), for all Dassault Aviation Model 
FALCON 2000 airplanes. AD 2021-03-11 was prompted by an MCAI originated 
by EASA, which is the Technical Agent for the Member States of the 
European Union. EASA issued AD 2020-0113, dated May 20, 2020 (EASA AD 
2020-0113) (which corresponds to FAA AD 2021-03-11), to correct an 
unsafe condition.
    AD 2021-03-11 requires revising the existing maintenance or 
inspection program, as applicable, to incorporate new or more 
restrictive airworthiness limitations. The FAA issued AD 2021-03-11 to 
address reduced controllability of the airplane. AD 2021-03-11 
specifies that accomplishing the revision required by that AD 
terminates all requirements of AD 2010-26-05, Amendment 39-16544 (75 FR 
79952, December 21, 2010) (AD 2010-26-05) for Model FALCON 2000 
airplanes only. This proposed AD would therefore continue allowing that 
termination.

Actions Since AD 2021-03-11 Was Issued

    Since the FAA issued AD 2021-03-11, EASA superseded AD 2020-0113 
and issued EASA AD 2022-0135, dated July 6, 2022 (EASA AD 2022-0135) 
(referred to after this as the MCAI), for all Dassault Aviation Model 
FALCON 2000 airplanes. The MCAI states that new or more restrictive 
airworthiness limitations have been developed.
    The FAA is proposing this AD to address reduced controllability of 
the airplane. You may examine the MCAI in the AD docket at 
regulations.gov under Docket No. FAA-2022-1585.

Related Service Information Under 1 CFR Part 51

    The FAA reviewed EASA AD 2022-0135. This service information 
specifies new or more restrictive airworthiness limitations for 
airplane structures and safe life limits.
    This proposed AD would also require EASA AD 2020-0113, which the 
Director of the Federal Register approved for incorporation by 
reference as of March 31, 2021 (86 FR 11116, February 24, 2021).
    This material is reasonably available because the interested 
parties have access to it through their normal course of business or by 
the means identified in ADDRESSES.

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 
described above. The FAA is issuing this NPRM after determining that 
the unsafe condition described previously is likely to exist or develop 
in other products of the same type design.

Proposed AD Requirements in This NPRM

    This proposed AD would retain all of the requirements of AD 2021-
03-11. This proposed AD would also require revising the existing 
maintenance or inspection program, as applicable, to incorporate 
additional new or more restrictive airworthiness limitations, which are 
specified in EASA AD 2022-0135 already described, as proposed for 
incorporation by reference. Any differences with EASA AD 2022-0135 are 
identified as exceptions in the regulatory text of this AD.
    This proposed AD would require revisions to certain operator 
maintenance documents to include new actions (e.g., inspections). 
Compliance with these actions is required by 14 CFR 91.403(c). For 
airplanes that have been previously modified, altered, or repaired in 
the areas addressed by this 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 (AMOC) according to 
paragraph (n)(1) of this proposed AD.

Explanation of Required Compliance Information

    In the FAA's ongoing efforts to improve the efficiency of the AD 
process, the FAA developed a process to use some civil aviation 
authority (CAA) ADs as the primary source of information for compliance 
with requirements for corresponding FAA ADs. The FAA has been 
coordinating this process with manufacturers and CAAs. As a result, the 
FAA proposes to retain the IBR of EASA AD 2020-0113 and incorporate 
EASA AD 2022-0135 by reference in the FAA final rule. This proposed AD 
would, therefore, require compliance with EASA AD 2022-0135 and EASA AD 
2020-0113 through that incorporation, except for any differences 
identified as exceptions in the regulatory text of this proposed AD. 
Using common terms that are the same as the heading of a particular 
section in EASA AD 2022-0135 or EASA AD 2020-0113 does not mean that 
operators need comply only with that section. For example, where the AD 
requirement refers to ``all required actions and compliance times,'' 
compliance with this AD requirement is not limited to the section 
titled ``Required Action(s) and Compliance Time(s)'' in EASA AD 2022-
0135 or EASA AD 2020-0113. Service information required by EASA AD 
2022-0135 and EASA AD 2020-0113 for compliance will be available at 
regulations.gov by searching for and locating Docket No. FAA-2022-1585 
after the FAA final rule is published.

Airworthiness Limitation ADs Using the New Process

    The FAA's process of incorporating by reference MCAI ADs as the 
primary

[[Page 77534]]

source of information for compliance with corresponding FAA ADs has 
been limited to certain MCAI ADs (primarily those with service 
bulletins as the primary source of information for accomplishing the 
actions required by the FAA AD). However, the FAA is now expanding the 
process to include MCAI ADs that require a change to airworthiness 
limitation documents, such as airworthiness limitation sections.
    For these ADs that incorporate by reference an MCAI AD that changes 
airworthiness limitations, the FAA requirements are unchanged. 
Operators must revise the existing maintenance or inspection program, 
as applicable, to incorporate the information specified in the new 
airworthiness limitation document. The airworthiness limitations must 
be followed according to 14 CFR 91.403(c) and 91.409(e).
    The previous format of the airworthiness limitation ADs included a 
paragraph that specified that 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 
the AMOCs paragraph under ``Additional AD Provisions.'' This new format 
includes a ``New Provisions for Alternative Actions and Intervals'' 
paragraph that does not specifically refer to AMOCs, but operators may 
still request an AMOC to use an alternative action or interval.

Costs of Compliance

    The FAA estimates that this AD, if adopted as proposed, would 
affect 168 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 2021-03-11 to be $7,650 (90 work-hours x $85 per work-
hour).
    The FAA has determined that revising the existing 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. In the past, the agency has estimated that this action 
takes 1 work-hour per airplane. 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.
    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).

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) 2021-03-11, Amendment 39-21414 
(86 FR 11116, February 24, 2021); and
0
b. Adding the following new AD:

Dassault Aviation: Docket No. FAA-2022-1585; Project Identifier 
MCAI-2022-00892-T.

(a) Comments Due Date

    The FAA must receive comments on this airworthiness directive 
(AD) by February 2, 2023.

(b) Affected ADs

    (1) This AD replaces AD 2021-03-11, Amendment 39-21414 (86 FR 
11116, February 24, 2021) (AD 2021-03-11).
    (2) This AD affects AD 2010-26-05, Amendment 39-16544 (75 FR 
79952, December 21, 2010) (AD 2010-26-05).

(c) Applicability

    This AD applies to all Dassault Aviation Model FALCON 2000 
airplanes, certificated in any category.

(d) Subject

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

(e) Unsafe Condition

    This AD was prompted by a determination that new or more 
restrictive airworthiness limitations are necessary. The FAA is 
issuing this AD to address reduced controllability of the airplane.

(f) Compliance

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

(g) Retained Revision of the Existing Maintenance or Inspection 
Program, With No Changes

    This paragraph restates the requirements of paragraph (i) of AD 
2021-03-11, with no changes. Except as specified in paragraph (h) of 
this AD: Comply with all required actions and compliance times 
specified in, and in accordance with, European Union Aviation Safety 
Agency (EASA) AD 2020-0113, dated May 20, 2020 (EASA AD 2020-0113). 
Accomplishing the revision of the existing maintenance or inspection 
program required by paragraph (j) of this AD terminates the 
requirements of this paragraph.

(h) Retained Exceptions to EASA AD 2020-0113, With No Changes

    This paragraph restates the exceptions specified in paragraph 
(j) of AD 2021-03-11, with no changes.
    (1) The requirements specified in paragraphs (1) and (2) of EASA 
AD 2020-0113 do not apply to this AD.
    (2) Paragraph (3) of EASA AD 2020-0113 specifies revising ``the 
approved AMP'' within 12 months after its effective date, but this 
AD requires revising the existing maintenance or inspection program, 
as applicable, to incorporate the ``limitations, tasks and 
associated thresholds and intervals'' specified in paragraph (3) of 
EASA

[[Page 77535]]

AD 2020-0113 within 90 days after the effective date of this AD.
    (3) The initial compliance time for doing the tasks specified in 
paragraph (3) of EASA AD 2020-0113 is at the applicable ``associated 
thresholds'' specified in paragraph (3) of EASA AD 2020-0113, or 
within 90 days after the effective date of this AD, whichever occurs 
later.
    (4) The provisions specified in paragraphs (4) and (5) of EASA 
AD 2020-0113 do not apply to this AD.
    (5) The ``Remarks'' section of EASA AD 2020-0113 does not apply 
to this AD.

(i) Retained No Alternative Actions or Intervals With a New Exception

    This paragraph restates the requirements of paragraph (k) of AD 
2021-03-11, with a new exception. Except as required by paragraph 
(j) of this AD, after the existing maintenance or inspection program 
has been revised as required by paragraph (g) of this AD, no 
alternative actions (e.g., inspections) or intervals may be used 
unless they are approved as specified in the provisions of the 
``Ref. Publications'' section of EASA AD 2020-0113.

(j) New Maintenance or Inspection Program Revision

    Except as specified in paragraph (k) of this AD: Comply with all 
required actions and compliance times specified in, and in 
accordance with, EASA AD 2022-0135, dated July 6, 2022 (EASA AD 
2022-0135). Accomplishing the maintenance or inspection program 
revision required by this paragraph terminates the requirements of 
paragraph (g) of this AD.

(k) Exceptions to EASA AD 2022-0135

    (1) The requirements specified in paragraphs (1) and (2) of EASA 
AD 2022-0135 do not apply to this AD.
    (2) Paragraph (3) of EASA AD 2022-0135 specifies revising ``the 
approved AMP'' within 12 months after its effective date, but this 
AD requires revising the existing maintenance or inspection program, 
as applicable, within 90 days after the effective date of this AD.
    (3) The initial compliance time for doing the tasks specified in 
paragraph (3) of EASA AD 2022-0135 is at the applicable 
``limitations'' and ``associated thresholds'' as incorporated by the 
requirements of paragraph (3) of EASA AD 2022-0135, or within 90 
days after the effective date of this AD, whichever occurs later.
    (4) The provisions specified in paragraphs (4) and (5) of EASA 
AD 2022-0135 do not apply to this AD.
    (5) The ``Remarks'' section of EASA AD 2022-0135 does not apply 
to this AD.

(l) New Provisions for Alternative Actions and Intervals

    After the existing maintenance or inspection program has been 
revised as required by paragraph (j) of this AD, no alternative 
actions (e.g., inspections), and intervals are allowed unless they 
are approved as specified in the provisions of the ``Ref. 
Publications'' section of EASA AD 2022-0135.

(m) Terminating Action for AD 2010-26-05

    Accomplishing the actions required by paragraph (g) or (j) of 
this AD terminates the requirements of paragraph (g) of AD 2010-26-
05 for Model FALCON 2000 airplanes only.

(n) 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 (o) 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 be 
accomplished using a method approved by the Manager, International 
Validation Branch, FAA; or EASA; or Dassault Aviation's EASA Design 
Organization Approval (DOA). If approved by the DOA, the approval 
must include the DOA-authorized signature.

(o) Additional Information

    For more information about this AD, contact Tom Rodriguez, 
Aerospace Engineer, Large Aircraft Section, International Validation 
Branch, FAA, 2200 South 216th St., Des Moines, WA 98198; telephone 
206-231-3226; email [email protected].

(p) 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 on 
[DATE 35 DAYS AFTER PUBLICATION OF THE FINAL RULE].
    (i) European Union Aviation Safety Agency (EASA) AD 2022-0135, 
dated July 6, 2022.
    (ii) [Reserved]
    (4) The following service information was approved for IBR on 
March 31, 2021 (86 FR 11116, February 24, 2021).
    (i) European Union Aviation Safety Agency (EASA) AD 2020-0113, 
dated May 20, 2020.
    (ii) [Reserved]
    (5) For EASA ADs 2022-0135 and 2020-0113, contact EASA, Konrad-
Adenauer-Ufer 3, 50668 Cologne, Germany; telephone +49 221 8999 000; 
email [email protected]; website easa.europa.eu. You may find these 
EASA ADs on the EASA website at ad.easa.europa.eu.
    (6) 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.
    (7) 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 December 12, 2022.
Christina Underwood,
Acting Director, Compliance & Airworthiness Division, Aircraft 
Certification Service.
[FR Doc. 2022-27298 Filed 12-16-22; 8:45 am]
BILLING CODE 4910-13-P
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