Rules and Regulations. Final rule

1,912 words·~9 min read·/register/2021/12/23/2021-27628

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BILLING CODE 4910-13-P DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2020-0364; Project Identifier MCAI-2019-00119-E; Amendment 39-21872; AD 2021-26-13] RIN 2120-AA64 Airworthiness Directives; Rolls-Royce Deutschland Ltd & Co KG (Type Certificate Previously Held by Rolls-Royce plc) Turbofan Engines AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Final rule. SUMMARY: The FAA is adopting a new airworthiness directive

(AD)for all Rolls-Royce Deutschland Ltd & Co KG

(RRD)Trent 1000-A2, Trent 1000-AE2, Trent 1000-C2, Trent 1000-CE2, Trent 1000-D2, Trent 1000-E2, Trent 1000-G2, Trent 1000-H2, Trent 1000-J2, Trent 1000-K2, and Trent 1000-L2 model turbofan engines. This AD was prompted by the manufacturer revising the engine Time Limits Manual

(TLM)life limits of certain critical rotating parts, updating direct accumulation counting

(DAC)data files, and updating certain maintenance tasks. This AD requires revision of the engine TLM life limits of certain critical rotating parts and DAC data files, as specified in a European Union Aviation Safety Agency

(EASA)AD, which is incorporated by reference. The FAA is issuing this AD to address the unsafe condition on these products. DATES: This AD is effective January 27, 2022. The Director of the Federal Register approved the incorporation by reference of a certain publication listed in this AD as of January 27, 2022. ADDRESSES: For material incorporated by reference in this AD, contact the EASA, Konrad-Adenauer-Ufer 3, 50668 Cologne, Germany; phone: +49 221 8999 000; email: *ADs@easa.europa.eu* . You may find this material on the EASA website at *https://ad.easa.europa.eu* . You may view this material at the FAA, Airworthiness Products Section, Operational Safety Branch, 1200 District Avenue, Burlington, MA 01803. For information on the availability of this material at the FAA, call

(817)222-5110. It is also available at *https://www.regulations.gov* by searching for and locating Docket No. FAA-2020-0364. Examining the AD Docket You may examine the AD docket at *https://www.regulations.gov* by searching for and locating Docket No. FAA-2020-0364; 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 final rule, the EASA AD, any comments received, and other information. The address for Docket Operations is U.S. Department of Transportation, Docket Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New Jersey Avenue SE, Washington, DC 20590. FOR FURTHER INFORMATION CONTACT: Kevin M. Clark, Aviation Safety Engineer, ECO Branch, FAA, 1200 District Avenue, Burlington, MA 01803; phone:

(781)238-7088; fax:

(781)238-7199; email: *kevin.m.clark@faa.gov* . SUPPLEMENTARY INFORMATION: Background The FAA issued a supplemental notice of proposed rulemaking (SNPRM) to amend 14 CFR part 39 by adding an AD that would apply to RRD Trent 1000-A2, Trent 1000-AE2, Trent 1000-C2, Trent 1000-CE2, Trent 1000-D2, Trent 1000-E2, Trent 1000-G2, Trent 1000-H2, Trent 1000-J2, Trent 1000-K2, and Trent 1000-L2 model turbofan engines. The SNPRM published in the **Federal Register** on September 20, 2021 (86 FR 52111). The SNPRM was prompted by the manufacturer revising the engine TLM life limits of certain critical rotating parts, updating DAC data files, and updating certain maintenance tasks. The SNPRM proposed to require operators to revise the ALS of their approved maintenance program by incorporating the revised tasks of the applicable TLM for each affected model turbofan engine. The SNPRM proposed to require accomplishing the actions specified in EASA AD 2020-0241, dated November 5, 2020 (also referred to as the Mandatory Continuing Airworthiness Information, or the MCAI), as incorporated by reference, except for any differences identified as exceptions in the regulatory text of the proposed AD and except as discussed under “Differences Between this Proposed AD and the EASA AD.” The FAA is issuing this AD to address the unsafe condition on these products. See the MCAI for additional background information. EASA, which is the Technical Agent for the Member States of the European Union, has issued EASA AD 2020-0241 to correct an unsafe condition for all RRD Trent 1000-A2, Trent 1000-AE2, Trent 1000-C2, Trent 1000-CE2, Trent 1000-D2, Trent 1000-E2, Trent 1000-G2, Trent 1000-H2, Trent 1000-J2, Trent 1000-K2, and Trent 1000-L2 model turbofan engines. Discussion of Final Airworthiness Directive Comments The FAA received one comment from an individual commenter. The commenter expressed support for the SNPRM without change, but incorrectly referenced automotive engines within the rationale for the support. Conclusion The FAA reviewed the relevant data, considered the comment received, and determined that air safety requires adopting this AD as proposed. Accordingly, the FAA is issuing this AD to address the unsafe condition on these products. Except for minor editorial changes, this AD is adopted as proposed in the SNPRM. None of the changes will increase the economic burden on any operator. Related Service Information Under 1 CFR Part 51 The FAA reviewed EASA AD 2020-0241. EASA AD 2020-0241 requires accomplishment of the actions specified in RRD's updated TLM for affected engines as specified in Rolls-Royce Trent 1000 TLM T-Trent-10RRC, Chapters 05-10 and 05-20, Revision 20, dated August 1, 2020. 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 ADDRESSES . Costs of Compliance The FAA estimates that this AD affects 20 engines installed on airplanes of U.S. registry. The FAA estimates the following costs to comply with this AD: Estimated Costs Action Labor cost Parts cost Cost per product Cost on U.S. operators Revise the continuous airworthiness maintenance program 1 work-hour × $85 per hour = $85 $0 $85 $1,700 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 This AD will not have federalism implications under Executive Order 13132. This AD will not have a substantial direct effect on the States, on the relationship between the national government and the States, or on the distribution of power and responsibilities among the various levels of government. For the reasons discussed above, I certify that this AD:

(1)Is not a “significant regulatory action” under Executive Order 12866,

(2)Will not affect intrastate aviation in Alaska, and

(3)Will not have a significant economic impact, positive or negative, on a substantial number of small entities under the criteria of the Regulatory Flexibility Act. List of Subjects in 14 CFR Part 39 Air transportation, Aircraft, Aviation safety, Incorporation by reference, Safety. The Amendment Accordingly, under the authority delegated to me by the Administrator, the FAA amends 14 CFR part 39 as follows: PART 39—AIRWORTHINESS DIRECTIVES 1. The authority citation for part 39 continues to read as follows: Authority: 49 U.S.C. 106(g), 40113, 44701. § 39.13 [Amended] 2. The FAA amends § 39.13 by adding the following new airworthiness directive: **2021-26-13 Rolls-Royce Deutschland Ltd & Co KG (Type Certificate previously held by Rolls-Royce plc):** Amendment 39-21872; Docket No. FAA-2020-0364; Project Identifier MCAI-2019-00119-E.

(a)Effective Date This airworthiness directive

(AD)is effective January 27, 2022.

(b)Affected ADs None.

(c)Applicability This AD applies to Rolls-Royce Deutschland Ltd & Co KG (Type Certificate previously held by Rolls-Royce plc)

(RRD)Trent 1000-A2, Trent 1000-AE2, Trent 1000-C2, Trent 1000-CE2, Trent 1000-D2, Trent 1000-E2, Trent 1000-G2, Trent 1000-H2, Trent 1000-J2, Trent 1000-K2, and Trent 1000-L2 model turbofan engines.

(d)Subject Joint Aircraft System Component

(JASC)Code 7200, Engine (Turbine/Turboprop).

(e)Unsafe Condition This AD was prompted by the manufacturer revising the engine Time Limits Manual life limits of certain critical rotating parts, updating the direct accumulation counting data files, and updating certain maintenance tasks. The FAA is issuing this AD to prevent the failure of critical rotating parts. The unsafe condition, if not addressed, could result in failure of one or more engines, loss of thrust control, and loss of the airplane.

(f)Compliance Comply with this AD within the compliance times specified, unless already done.

(g)Required Actions Except as specified in paragraph

(h)of this AD: Perform all required actions within the compliance times specified in, and in accordance with, European Union Aviation Safety Agency AD 2020-0241, dated November 5, 2020 (EASA AD 2020-0241).

(h)Exceptions to EASA AD 2020-0241

(1)The requirements specified in paragraphs

(1)and

(2)of EASA AD 2020-0241 are not required by this AD.

(2)Where EASA AD 2020-0241 requires compliance from its effective date, this AD requires using the effective date of this AD.

(3)Paragraph

(3)of EASA AD 2020-0241 specifies revising the approved airworthiness maintenance program within 12 months after its effective date, but this AD requires revising the existing approved continuous airworthiness maintenance program within 90 days after the effective date of this AD.

(4)This AD does not mandate compliance with the “Remarks” section of EASA AD 2020-0241.

(i)No Reporting Requirement Although the service information referenced in EASA AD 2020-0241 specifies to submit certain information to the manufacturer, this AD does not include that requirement.

(j)Alternative Methods of Compliance (AMOCs)

(1)The Manager, ECO 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 local Flight Standards District Office, as appropriate. If sending information directly to the manager of the ECO Branch, send it to the attention of the person identified in paragraph

(k)of this AD. Information may be emailed to: *ANE-AD-AMOC@faa.gov* .

(2)Before using any approved AMOC, notify your appropriate principal inspector, or lacking a principal inspector, the manager of the local flight standards district office/certificate holding district office.

(k)Related Information For more information about this AD, contact Kevin M. Clark, Aviation Safety Engineer, ECO Branch, FAA, 1200 District Avenue, Burlington, MA 01803; phone:

(781)238-7088; fax:

(781)238-7199; email: *kevin.m.clark@faa.gov* .

(l)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.

(i)European Union Aviation Safety Agency

(EASA)AD 2020-0241, dated November 5, 2020.

(ii)[Reserved]

(3)For EASA AD 2020-0241, contact EASA, Konrad-Adenauer-Ufer 3, 50668 Cologne, Germany; phone: +49 221 8999 000; email: *ADs@easa.europa.eu* . You may find this EASA AD on the EASA website at *https://ad.easa.europa.eu* .

(4)You may view this service information at the at the FAA, Airworthiness Products Section, Operational Safety Branch, 1200 District Avenue, Burlington, MA 01803. For information on the availability of this material at the FAA, call

(817)222-5110.

(5)You may view this material 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 *https://www.archives.gov/federal-register/cfr/ibr-locations.html* . Issued on December 9, 2021. Lance T. Gant, Director, Compliance & Airworthiness Division, Aircraft Certification Service. [FR Doc. 2021-27628 Filed 12-22-21; 8:45 am]

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