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###### Department of Transportation

###### Federal Aviation Administration

          - 14 CFR Part 39
          - [Docket No. FAA-2022-0086; Project Identifier MCAI-2021-01035-T; Amendment 39-22026; AD 2022-09-06]
          - RIN 2120-AA64

# AGENCY:

Federal Aviation Administration (FAA), Department of Transportation (DOT).

# ACTION:

Final rule.

      ( print page 29655)    

# SUMMARY:

The FAA is superseding Airworthiness Directive (AD) 2021-13-06, which applied to certain Airbus SAS Model A350-941 and -1041 airplanes. AD 2021-13-06 required revising the existing maintenance or inspection program, as applicable, to incorporate new or more restrictive airworthiness limitations. Since the FAA issued AD 2021-13-06, the FAA has determined that new or more restrictive airworthiness limitations are necessary. This AD continues to require the actions in AD 2021-13-06 and requires 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 incorporated by reference. The FAA is issuing this AD to address the unsafe condition on these products.

# DATES:

This AD is effective June 20, 2022.

The Director of the Federal Register approved the incorporation by reference of a certain publication listed in this AD as of June 20, 2022.

The Director of the Federal Register approved the incorporation by reference of certain other publications listed in this AD as of September 3, 2021 (86 FR 40934, July 30, 2021).

# ADDRESSES:

                        For material incorporated by reference (IBR) in this AD, contact EASA, Konrad-Adenauer-Ufer 3, 50668 Cologne, Germany; telephone +49 221 8999 000; email                         *ADs@easa.europa.eu*; internet                         *www.easa.europa.eu*. You may find this IBR 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, 2200 South 216th St., Des Moines, WA. For information on the availability of this material at the FAA, call 206-231-3195. It is also available in the AD docket at                         *https://www.regulations.gov*                         by searching for and locating Docket No. FAA-2022-0086.                    

## Examining the AD Docket

                    You may examine the AD docket at                     *https://www.regulations.gov*                     by searching for and locating Docket No. FAA-2022-0086; 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 mandatory continuing airworthiness information (MCAI), 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:

                        Dan Rodina, Aerospace Engineer, Large Aircraft Section, FAA, International Validation Branch, 2200 South 216th St., Des Moines, WA 98198; telephone and fax 206-231-3225; email                         *dan.rodina@faa.gov*.                    

# SUPPLEMENTARY INFORMATION:

## Background

EASA, which is the Technical Agent for the Member States of the European Union, has issued EASA AD 2021-0208, dated September 15, 2021 (EASA AD 2021-0208) (also referred to as the MCAI), to correct an unsafe condition for all Airbus SAS Model A350-941 and -1041 airplanes.

                    The FAA issued a notice of proposed rulemaking (NPRM) to amend 14 CFR part 39 to supersede AD 2021-13-06, Amendment 39-21611 (86 FR 40934, July 30, 2021) (AD 2021-13-06). AD 2021-13-06 applied to certain Airbus SAS Model A350-941 and -1041 airplanes. The NPRM published in the                     **Federal Register**                     on February 9, 2022 (87 FR 7397). The NPRM was prompted by a determination that new or more restrictive airworthiness limitations are necessary. The NPRM proposed to continue to require the actions in AD 2021-13-06 and require revising the existing maintenance or inspection program, as applicable, to incorporate additional new or more restrictive airworthiness limitations, as specified in EASA AD 2021-0208.                

The FAA is issuing this AD to address hazardous or catastrophic airplane system failures. See the MCAI for additional background information.

## Discussion of Final Airworthiness Directive

## Comments

The FAA received a comment from the Air Line Pilots Association, International (ALPA) who supported the NPRM without change.

## Conclusion

The FAA reviewed the relevant data, considered the comment received, and determined that air safety requires adopting this AD as proposed. Except for minor editorial changes, this AD is adopted as proposed in the NPRM. None of the changes will increase the economic burden on any operator. Accordingly, the FAA is issuing this AD to address the unsafe condition on these products.

## Related Service Information Under 1 CFR Part 51

EASA AD 2021-0208 describes new or more restrictive airworthiness limitations for airplane structures and safe life limits.

This AD also requires EASA AD 2020-0211, dated October 5, 2020, and EASA AD 2021-0026, dated January 20, 2021, which the Director of the Federal Register approved for incorporation by reference as of September 3, 2021 (86 FR 40934, July 30, 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 the                     **ADDRESSES**                     section.                

## Costs of Compliance

The FAA estimates that this AD affects 27 airplanes of U.S. registry. The FAA estimates the following costs to comply with this AD:

The FAA estimates the total cost per operator for the retained actions from AD 2021-13-06 to be $7,650 (90 work-hours × $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. 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).

## 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.                          ( print page 29656)    

## 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 

2. The FAA amends § 39.13 by: 

a. Removing Airworthiness Directive (AD) 2021-13-06, Amendment 39-21611 ( 86 FR 40934, July 30, 2021); and

b. Adding the following new AD: 

**2022-09-06 Airbus SAS:**                             Amendment 39-22026; Docket No. FAA-2022-0086; Project Identifier MCAI-2021-01035-T.                        

## (a) Effective Date

This airworthiness directive (AD) is effective June 20, 2022.

## (b) Affected ADs

(1) This AD replaces AD 2021-13-06, Amendment 39-21611 (86 FR 40934, July 30, 2021) (AD 2021-13-06).

(2) This AD affects AD 2019-20-01, Amendment 39-19754 (84 FR 55495, October 17, 2019) (AD 2019-20-01).

## (c) Applicability

This AD applies to Airbus SAS Model A350-941 and -1041 airplanes, certificated in any category, with an original airworthiness certificate or original export certificate of airworthiness issued on or before July 20, 2021.

## (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 hazardous or catastrophic airplane system failures.

## (f) Compliance

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

## (g) Retained Maintenance or Inspection Program Revision, With No Changes

This paragraph restates the requirements of paragraph (g) of AD 2021-13-06, with no changes. For airplanes with an original airworthiness certificate or original export certificate of airworthiness issued on or before July 22, 2020: 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 2020-0211, dated October 5, 2020 (EASA AD 2020-0211); and EASA AD 2021-0026, dated January 20, 2021 (EASA AD 2021-0026). Where EASA AD 2021-0026 affects the same airworthiness limitations (tasks and life limits) as those in EASA AD 2020-0211, the airworthiness limitations referenced in EASA AD 2021-0026 prevail. 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 2020-0211 and EASA AD 2021-0026, With No Changes

This paragraph restates the requirements of paragraph (h) of AD 2021-13-06, with no changes. For airplanes with an original airworthiness certificate or original export certificate of airworthiness issued on or before July 22, 2020:

(1) Where EASA AD 2020-0211 and EASA AD 2021-0026 refers to its effective date, this AD requires using September 3, 2021 (the effective date of AD 2021-13-06).

(2) The requirements specified in paragraphs (1) and (2) of EASA AD 2020-0211 and EASA AD 2021-0026 do not apply to this AD.

(3) Paragraph (3) of EASA AD 2020-0211 and EASA AD 2021-0026 specifies revising “the approved AMP [aircraft maintenance program]” 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 AD 2020-0211 and EASA AD 2021-0026 within 90 days after September 3, 2021 (the effective date of AD 2021-13-06).

(4) The initial compliance time for doing the tasks specified in paragraph (3) of EASA AD 2020-0211 and EASA AD 2021-0026 is at the applicable “thresholds” as incorporated by the requirements of paragraph (3) of EASA AD 2020-0211 and EASA AD 2021-0026, or within 90 days after September 3, 2021 (the effective date of AD 2021-13-06), whichever occurs later.

(5) The provisions specified in paragraphs (4) and (5) of EASA AD 2020-0211 do not apply to this AD.

(6) The provisions specified in paragraph (4) of EASA AD 2021-0026 do not apply to this AD.

(7) The “Remarks” section of EASA AD 2020-0211 and EASA AD 2021-0026 does not apply to this AD.

## (i) Retained Provisions for Alternative Actions and Intervals, With a New Exception

                            This paragraph restates the requirements of paragraph (i) of AD 2021-13-06, with a new exception. For airplanes with an original airworthiness certificate or original export certificate of airworthiness issued on or before July 22, 2020: 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) and intervals are allowed unless they are approved as specified in the provisions of the “Ref. Publications” section of EASA AD 2020-0211 or EASA AD 2021-0026.                        

## (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 2021-0208, dated September 15, 2021. Accomplishing the revision of the existing maintenance or inspection program required by this paragraph terminates the requirements of paragraph (g) of this AD.

## (k) Exceptions to EASA AD 2021-0208

(1) Where EASA AD 2021-0208 refers to its effective date, this AD requires using the effective date of this AD.

(2) The requirements specified in paragraphs (1) and (2) of EASA AD 2021-0208 do not apply to this AD.

(3) Paragraph (3) of EASA AD 2021-0208 specifies to revise “the 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.

(4) The initial compliance time for doing the tasks specified in paragraph (3) of EASA AD 2021-0208 is at the applicable “limitations” as incorporated by the requirements of paragraph (3) of EASA AD 2021-0208, or within 90 days after the effective date of this AD, whichever occurs later.

(5) The provisions specified in paragraphs (4) and (5) of EASA AD 2021-0208 do not apply to this AD.

(6) The “Remarks” section of EASA AD 2021-0208 does not apply to this AD.

                            (7) Where EASA AD 2021-0208 refers to Airbus A350 Airworthiness Limitations Section (ALS) Part 4, Revision 6 and Variation 6.1, replace the text “Airbus A350 Airworthiness Limitations Section (ALS) Part 4, Revision 6 and Variation 6.1,” with “Airbus A350 Airworthiness Limitations Section (ALS) Part 4, Revision 6 and                                   ( print page 29657)                                Variation 6.1; for any airworthiness limitations (tasks and life limits) that are in both documents, the airworthiness limitations (tasks and life limits) specified in Variation 6.1 prevail.”                        

## (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 2021-0208.                        

## (m) Terminating Action for Certain Requirements of AD 2019-20-01

Accomplishing the actions required by paragraph (g) or (j) of this AD terminates the repetitive greasing task for batch 02 group of affected thrust reverser actuators required by paragraph (g) of AD 2019-20-01.

## (n) Additional AD Provisions

The following provisions also apply to this AD:

                            (1)                             *Alternative Methods of Compliance (AMOCs):*                             The Manager, Large Aircraft Section, 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 Large Aircraft Section, 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, Large Aircraft Section, International Validation Branch, FAA; or EASA; or Airbus SAS's EASA Design Organization Approval (DOA). If approved by the DOA, the approval must include the DOA-authorized signature.                        

## (o) Related Information

                            For more information about this AD, contact Dan Rodina, Aerospace Engineer, Large Aircraft Section, FAA, International Validation Branch, 2200 South 216th St., Des Moines, WA 98198; telephone and fax 206-231-3225; email                             *dan.rodina@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 June 20, 2022.

(i) European Union Aviation Safety Agency (EASA) AD 2021-0208, dated September 15, 2021.

(ii) [Reserved]

(4) The following service information was approved for IBR on September 3, 2021 (86 FR 40934, July 30, 2021).

(i) European Union Aviation Safety Agency (EASA) AD 2020-0211, dated October 5, 2020.

(ii) European Union Aviation Safety Agency (EASA) AD 2021-0026, dated January 20, 2021.

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

(6) 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.

                            (7) 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 April 15, 2022.

Lance T. Gant, 

Director, Compliance & Airworthiness Division, Aircraft Certification Service.

[FR Doc. 2022-10460 Filed 5-13-22; 8:45 am]

BILLING CODE 4910-13-P