2021-27090. Airworthiness Directives; The Boeing Company Airplanes  

  • Start Preamble

    AGENCY:

    Federal Aviation Administration (FAA), DOT.

    ACTION:

    Final rule.

    SUMMARY:

    The FAA is superseding Airworthiness Directive (AD) 2019-01-08, which applied to certain The Boeing Company Model 777-200, -200LR, -300, and -300ER series airplanes. AD 2019-01-08 required modifications for galley mounted attendant seat fittings. This AD was prompted by a report that showed a non-compliance exists on some in-service galley attendant seat fitting installations, and a determination that additional airplanes are subject to the unsafe condition. This AD requires modifications for galley mounted attendant seat fittings. The FAA is Start Printed Page 71132 issuing this AD to address the unsafe condition on these products.

    DATES:

    This AD is effective January 19, 2022.

    The Director of the Federal Register approved the incorporation by reference of a certain publication listed in this AD as of January 19, 2022.

    ADDRESSES:

    For service information identified in this final rule, contact Boeing Commercial Airplanes, Attention: Contractual & Data Services (C&DS), 2600 Westminster Blvd., MC 110-SK57, Seal Beach, CA 90740-5600; telephone 562-797-1717; internet https://www.myboeingfleet.com. 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. It is also available at https://www.regulations.gov by searching for and locating Docket No. FAA-2021-0451.

    Examining the AD Docket

    You may examine the AD docket at https://www.regulations.gov by searching for and locating Docket No. FAA-2021-0451; 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, 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.

    Start Further Info

    FOR FURTHER INFORMATION CONTACT:

    Brandon Lucero, Aerospace Engineer, Cabin Safety and Environmental Systems Section, FAA, Seattle ACO Branch, 2200 South 216th St., Des Moines, WA 98198; phone and fax: 206-231-3569; email: brandon.lucero@faa.gov.

    End Further Info End Preamble Start Supplemental Information

    SUPPLEMENTARY INFORMATION:

    Background

    The FAA issued a notice of proposed rulemaking (NPRM) to amend 14 CFR part 39 to supersede AD 2019-01-08, Amendment 39-19547 (84 FR 4318, February 15, 2019) (AD 2019-01-08). AD 2019-01-08 applied to certain The Boeing Company Model 777-200, -200LR, -300, and -300ER series airplanes. The NPRM published in the Federal Register on June 25, 2021 (86 FR 33574). The NPRM was prompted by a report that showed a non-compliance exists on some in-service galley attendant seat fitting installations, and a determination that additional airplanes are subject to the unsafe condition. In the NPRM, the FAA proposed to continue to require modifications for galley mounted attendant seat fittings and expand the applicability to include additional airplanes. The FAA is issuing this AD to address non-compliant flight attendant seats, which could fail in a high-G crash and result in potential injury to flight attendants and consequent inability of the flight attendants to assist with passenger evacuation in a timely manner.

    Discussion of Final Airworthiness Directive

    Comments

    The FAA received comments from Boeing and United Airlines, who supported the NPRM without change.

    Conclusion

    The FAA reviewed the relevant data, considered any comments 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.

    Related Service Information Under 1 CFR Part 51

    The FAA reviewed Boeing Special Attention Service Bulletin 777-25-0649, Revision 2, dated October 8, 2020. This service information specifies procedures for modifying galley mounted attendant seat fittings. 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.

    Costs of Compliance

    The FAA estimates that this AD affects 50 airplanes of U.S. registry. The FAA estimates the following costs to comply with this AD:

    Estimated Costs

    ActionLabor costParts costCost per productCost on U.S. operators
    Modification7 work-hours × $85 per hour = $595$0$595$29,750

    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.

    Start List of Subjects

    List of Subjects in 14 CFR Part 39

    • Air transportation
    • Aircraft
    • Aviation safety
    • Incorporation by reference
    • Safety
    End List of Subjects

    The Amendment

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

    Start Part Start Printed Page 71133

    PART 39—AIRWORTHINESS DIRECTIVES

    End Part Start Amendment Part

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

    End Amendment Part Start Authority

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

    End Authority
    [Amended]
    Start Amendment Part

    2. The FAA amends § 39.13 by:

    End Amendment Part Start Amendment Part

    a. Removing Airworthiness Directive 2019-01-08, Amendment 39-19547 ( 84 FR 4318, February 15, 2019), and

    End Amendment Part Start Amendment Part

    b. Adding the following new airworthiness directive:

    End Amendment Part

    2021-19-15 The Boeing Company: Amendment 39-21733; Docket No. FAA-2021-0451; Project Identifier AD-2021-00007-T.

    (a) Effective Date

    This airworthiness directive (AD) is effective January 19, 2022.

    (b) Affected ADs

    This AD replaces AD 2019-01-08, Amendment 39-19547 (84 FR 4318, February 15, 2019) (AD 2019-01-08).

    (c) Applicability

    This AD applies to The Boeing Company Model 777-200, -200LR, -300, and -300ER series airplanes, certificated in any category, as identified in Boeing Special Attention Service Bulletin 777-25-0649, Revision 2, dated October 8, 2020.

    (d) Subject

    Air Transport Association (ATA) of America Code 25, Equipment/furnishings.

    (e) Unsafe Condition

    This AD was prompted by a report that showed a non-compliance exists on some in-service galley attendant seat fitting installations, and a determination that additional airplanes are subject to the unsafe condition. The FAA is issuing this AD to address non-compliant flight attendant seats, which could fail in a high-G crash and result in potential injury to flight attendants and consequent inability of the flight attendants to assist with passenger evacuation in a timely manner.

    (f) Compliance

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

    (g) Required Actions

    Except as specified by paragraph (h) of this AD: At the applicable times specified in paragraph 1.E., “Compliance,” of Boeing Special Attention Service Bulletin 777-25-0649, Revision 2, dated October 8, 2020, do all applicable actions identified as “RC” (required for compliance) in, and in accordance with, the Accomplishment Instructions of Boeing Special Attention Service Bulletin 777-25-0649, Revision 2, dated October 8, 2020.

    (h) Exception to Service Information Specifications

    Where Boeing Special Attention Service Bulletin 777-25-0649, Revision 2, dated October 8, 2020, uses the phrase “the Revision 2 date of this service bulletin,” this AD requires using “the effective date of this AD.”

    (i) No Reporting Requirement

    Although the service information referenced in Boeing Special Attention Service Bulletin 777-25-0649, Revision 2, dated October 8, 2020, specifies to submit certain information to the manufacturer, this AD does not include that requirement.

    (j) Credit for Previous Actions

    This paragraph provides credit for the actions specified in paragraph (g) of this AD, if those actions were performed before the effective date of this AD using Boeing Special Attention Service Bulletin 777-25-0649, Revision 1, dated October 6, 2017 (which is incorporated by reference in AD 2019-01-08).

    (k) Alternative Methods of Compliance (AMOCs)

    (1) The Manager, Seattle 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 the attention of the person identified in Related Information. Information may be emailed to: 9-ANM-Seattle-ACO-AMOC-Requests@faa.gov.

    (2) Before using any approved AMOC, notify your appropriate principal inspector, or lacking a principal inspector, the manager of the responsible Flight Standards Office.

    (3) An AMOC that provides an acceptable level of safety may be used for any repair, modification, or alteration required by this AD if it is approved by The Boeing Company Organization Designation Authorization (ODA) that has been authorized by the Manager, Seattle ACO Branch, FAA, to make those findings. To be approved, the repair method, modification deviation, or alteration deviation must meet the certification basis of the airplane, and the approval must specifically refer to this AD.

    (4) AMOCs approved for AD 2019-01-08 are approved as AMOCs for the corresponding provisions of Boeing Special Attention Service Bulletin 777-25-0649, Revision 2, dated October 8, 2020, that are required by paragraph (g) of this AD.

    (5) For service information that contains steps that are labeled as Required for Compliance (RC), the provisions of paragraphs (k)(5)(i) and (ii) of this AD apply.

    (i) The steps labeled as RC, including substeps under an RC step and any figures identified in an RC step, must be done to comply with the AD. If a step or substep is labeled “RC Exempt,” then the RC requirement is removed from that step or substep. An AMOC is required for any deviations to RC steps, including substeps and identified figures.

    (ii) Steps not labeled as RC may be deviated from using accepted methods in accordance with the operator's maintenance or inspection program without obtaining approval of an AMOC, provided the RC steps, including substeps and identified figures, can still be done as specified, and the airplane can be put back in an airworthy condition.

    (l) Related Information

    (1) For more information about this AD, contact Brandon Lucero, Aerospace Engineer, Cabin Safety and Environmental Systems Section, FAA, Seattle ACO Branch, 2200 South 216th St., Des Moines, WA 98198; phone and fax: 206-231-3569; email: brandon.lucero@faa.gov.

    (2) Service information identified in this AD that is not incorporated by reference is available at the addresses specified in paragraphs (m)(3) and (4) of this AD.

    (m) 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 the AD specifies otherwise.

    (i) Boeing Special Attention Service Bulletin 777-25-0649, Revision 2, dated October 8, 2020.

    (ii) [Reserved]

    (3) For service information identified in this AD, contact Boeing Commercial Airplanes, Attention: Contractual & Data Services (C&DS), 2600 Westminster Blvd., MC 110-SK57, Seal Beach, CA 90740-5600; telephone 562-797-1717; internet https://www.myboeingfleet.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: https://www.archives.gov/​federal-register/​cfr/​ibr-locations.html.

    Start Signature

    Issued on September 8, 2021.

    Lance T. Gant,

    Director, Compliance & Airworthiness Division, Aircraft Certification Service.

    End Signature End Supplemental Information

    [FR Doc. 2021-27090 Filed 12-14-21; 8:45 am]

    BILLING CODE 4910-13-P

Document Information

Effective Date:
1/19/2022
Published:
12/15/2021
Department:
Federal Aviation Administration
Entry Type:
Rule
Action:
Final rule.
Document Number:
2021-27090
Dates:
This AD is effective January 19, 2022.
Pages:
71131-71133 (3 pages)
Docket Numbers:
Docket No. FAA-2021-0451, Project Identifier AD-2021-00007-T, Amendment 39-21733, AD 2021-19-15
RINs:
2120-AA64: Airworthiness Directives
RIN Links:
https://www.federalregister.gov/regulations/2120-AA64/airworthiness-directives
Topics:
Air transportation, Aircraft, Aviation safety, Incorporation by reference, Safety
PDF File:
2021-27090.pdf
Supporting Documents:
» Airworthiness Directives: The Boeing Company Airplanes
» U.S. DOT/FAA - Supporting AD Document
» Airworthiness Directives: The Boeing Company Airplanes
CFR: (1)
14 CFR 39.13