2023-13149. Airworthiness Directives; The Boeing Company Airplanes  

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    AGENCY:

    Federal Aviation Administration (FAA), DOT.

    ACTION:

    Final rule.

    SUMMARY:

    The FAA is superseding Airworthiness Directive (AD) 2022–06–16, which applied to all The Boeing Company Model 747–100, 747–100B, 747–100B SUD, 747–200B, 747–200C, 747–200F, 747–300, 747–400, 747–400D, and 747–400F series airplanes. AD 2022–06–16 required revising the limitations and operating procedures sections of the existing airplane flight manual (AFM) to incorporate specific operating procedures for takeoff, instrument landing system (ILS) approaches, non-precision approaches, and go around and missed approaches, when in the presence of interference from wireless broadband operations in the 3.7–3.98 GHz frequency band (5G C-Band) interference as identified by Notices to Air Missions (NOTAMs). Since the FAA issued AD 2022–06–16, the FAA determined that additional limitations are needed due to the continued deployment of new 5G C-Band stations whose signals are expected to cover most of the contiguous United States at transmission frequencies between 3.7–3.98 GHz. This AD requires revising the limitations section of the existing AFM to incorporate limitations requiring Start Printed Page 40004 specific operating procedures, and retains the operating procedures for takeoff, ILS approaches, non-precision approaches, and go-around and missed approaches from AD 2022–06–16, due to the presence of 5G C-Band interference. The FAA is issuing this AD to address the unsafe condition on these products.

    DATES:

    This AD is effective June 21, 2023.

    ADDRESSES:

    AD Docket: You may examine the AD docket at regulations.gov under Docket No. FAA–2023–0922; 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.

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    FOR FURTHER INFORMATION CONTACT:

    Brett Portwood, Continued Operational Safety Technical Advisor, COS Program Management Section, Operational Safety Branch, FAA, 3960 Paramount Boulevard, Lakewood, CA 90712–4137; phone: 817–222–5390; email: operationalsafety@faa.gov.

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    SUPPLEMENTARY INFORMATION:

    Background

    The FAA issued a notice of proposed rulemaking (NPRM) to amend 14 CFR part 39 to supersede AD 2022–06–16, Amendment 39–21982 (87 FR 14780, March 16, 2022) (AD 2022–06–16). AD 2022–06–16 applied to all The Boeing Company (Boeing) Model 747–100, 747–100B, 747–100B SUD, 747–200B, 747–200C, 747–200F, 747–300, 747–400, 747–400D, and 747–400F series airplanes. The NPRM published in the Federal Register on May 3, 2023 (88 FR 27734). The NPRM was prompted by a determination that radio altimeters cannot be relied upon to perform their intended function if they experience 5G C-Band interference, and a determination that during takeoff, approach, landings, and go-arounds, as a result of this interference, certain airplane systems may not properly function, resulting in increased flightcrew workload while on approach with the flight director, autothrottle, or autopilot engaged.

    In the NPRM, the FAA proposed to retain the AFM revisions required by AD 2022–06–16 until June 30, 2023. On or before June 30, 2023, the FAA proposed to require replacing those AFM revisions with limitations requiring the same procedures for dispatch or release to airports, and takeoff, approach, landing, and go-around on runways at all airports for non-radio altimeter tolerant airplanes. For radio altimeter tolerant airplanes, the FAA proposed that the procedures would not be required at 5G C-Band mitigated airports (5G CMAs) as identified in an FAA Domestic Notice. The FAA proposed this AD to address 5G C-Band interference that could result in increased flightcrew workload and could lead to reduced ability of the flightcrew to maintain safe flight and landing of the airplane.

    Discussion of Final Airworthiness Directive

    Comments

    The FAA provided the public with an opportunity to comment on the proposed AD and received comments from two commenters. Boeing and the Air Line Pilots Association, International (ALPA), supported the NPRM without change. The supportive comments from ALPA included additional viewpoints without a suggestion specific to the AD or a request the FAA can act on. These comments are outside the scope of this final rule.

    Conclusion

    The FAA reviewed the relevant data, considered any comments 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. This AD is adopted as proposed in the NPRM.

    Interim Action

    The FAA considers this AD to be an interim action. Once the Technical Standard Order (TSO) standard for radio altimeters is established, which will follow the existing international technical consensus on the establishment of the minimum operational performance standards (MOPS), the FAA anticipates that the MOPS will be incorporated into the TSO. Once a new radio altimeter TSO is developed, approved, and available, the FAA might consider additional rulemaking.

    Effective Date

    Section 553(d) of the Administrative Procedure Act (APA) (5 U.S.C. 551 et seq.) requires publication of a rule not less than 30 days before its effective date. However, section 553(d) authorizes agencies to make rules effective in less than 30 days when the agency finds “good cause.” Radio altimeters cannot be relied upon to perform their intended function if they experience interference from wireless broadband operations in the 5G C-Band. This interference can cause other airplane systems to not properly function, resulting in increased flightcrew workload and could lead to reduced ability of the flightcrew to maintain safe flight and landing of the airplane. To address this unsafe condition, the actions required by this AD must be accomplished before the compliance date of June 30, 2023. The FAA based this date on the changes to the 5G C-Band environment beginning on July 1, 2023. These changes include increased wireless broadband deployment and transmissions closer to the parameters authorized by the FCC. The earlier operators learn of the requirements in this AD, the earlier they can take action to ensure compliance. An effective date less than 30 days would ensure the AD is codified earlier, thereby increasing awareness of its requirements. Therefore, the FAA finds that good cause exists pursuant to 5 U.S.C. 553(d) for making this amendment immediately effective.

    Costs of Compliance

    The cost information below describes the costs to change the AFM. Although this AD largely maintains the AFM limitations currently required by AD 2022–06–16, the FAA acknowledges that this AD may also impose costs on some aircraft operators from having to change their conduct to comply with the amended AFM. However, the FAA lacks the data necessary to quantify the costs associated with aircraft operators changing their conduct.

    The FAA estimates that this AD affects 137 airplanes of U.S. registry. The FAA estimates the following costs to comply with this AD: Start Printed Page 40005

    Estimated Costs

    ActionLabor costParts costCost per productCost on U.S. operators
    AFM revision (retained actions from AD 2022–02–16)1 work-hour × $85 per hour 1 = $85$0$85$11,645
    New AFM revisions (new action)1 work-hour × $85 per hour = $850852  11,645
    1  The labor rate of $85 per hour is the average wage rate for an aviation mechanic.
    2  The estimated cost for this revision would not constitute a significant economic impact (even for small entities) because $85 is a minimal cost compared to the regular costs of maintaining and operating a Model 747–100, 747–100B, 747–100B SUD, 747–200B, 747–200C, 747–200F, 747–300, 747–400, 747–400D, or 747–400F transport category airplane.

    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.

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    List of Subjects in 14 CFR Part 39

    • Air transportation
    • Aircraft
    • Aviation safety
    • Incorporation by reference
    • Safety
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    The Amendment

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

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    PART 39—AIRWORTHINESS DIRECTIVES

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

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

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    [Amended]
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    2. The FAA amends § 39.13 by:

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    a. Removing Airworthiness Directive (AD) 2022–06–16, Amendment 39–21982 ( 87 FR 14780, March 16, 2022), and

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    b. Adding the following new AD:

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    2023–12–14 The Boeing Company: Amendment 39–22472; Docket No. FAA–2023–0922; Project Identifier AD–2022–01431–T.

    (a) Effective Date

    This airworthiness directive (AD) is effective June 21, 2023.

    (b) Affected ADs

    This AD replaces AD 2022–06–16, Amendment 39–21982 (87 FR 14780, March 16, 2022) (AD 2022–06–16).

    (c) Applicability

    This AD applies to all The Boeing Company Model 747–100, 747–100B, 747–100B SUD, 747–200B, 747–200C, 747–200F, 747–300, 747–400, 747–400D, and 747–400F series airplanes, certificated in any category.

    (d) Subject

    Air Transport Association (ATA) of America Code 34, Navigation.

    (e) Unsafe Condition

    This AD was prompted by a determination that radio altimeters cannot be relied upon to perform their intended function if they experience interference from wireless broadband operations in the 3.7–3.98 GHz frequency band (5G C-Band), and a determination that during takeoff, approach, landings, and go-arounds, as a result of this interference, certain airplane systems may not properly function, resulting in increased flightcrew workload while on approach with the flight director, autothrottle, or autopilot engaged. The FAA is issuing this AD to address 5G C-Band interference that could result in increased flightcrew workload and could lead to reduced ability of the flightcrew to maintain safe flight and landing of the airplane.

    (f) Compliance

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

    (g) Definitions

    (1) For purposes of this AD, a “5G C-Band mitigated airport” (5G CMA) is an airport at which the telecommunications companies have agreed to voluntarily limit their 5G deployment at the request of the FAA, as identified by an FAA Domestic Notice.

    (2) For purposes of this AD, a “radio altimeter tolerant airplane” is one for which the radio altimeter, as installed, demonstrates the tolerances specified in paragraphs (g)(2)(i) and (ii) of this AD, using a method approved by the FAA.

    (i) Tolerance to radio altimeter interference, for the fundamental emissions (3.7–3.98 GHz), at or above the power spectral density (PSD) curve threshold specified in figure 1 to paragraph (g)(2)(i) of this AD.

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    Figure 1 to paragraph (g)(2)(i)— Fundamental Effective Isotropic PSD at Outside Interface of Aircraft Antenna

    (ii) Tolerance to radio altimeter interference, for the spurious emissions (3.7–3.98 GHz), at or above the PSD curve threshold specified in figure 2 to paragraph (g)(2)(ii) of this AD.

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    Figure 2 to paragraph (g)(2)(ii)— Spurious Effective Isotropic PSD at Outside Interface of Aircraft Antenna

    (3) For purposes of this AD, a “non-radio altimeter tolerant airplane” is one for which the radio altimeter, as installed, does not demonstrate the tolerances specified in paragraphs (g)(2)(i) and (ii) of this AD.

    (h) Retained Airplane Flight Manual (AFM) Revision

    This paragraph restates the requirements of paragraph (h) of AD 2022–02–16.

    (1) Within 2 days after March 16, 2022 (the effective date of AD 2022–06–16): Revise the Limitations Section of the existing AFM to include the information specified in figure 3 to paragraph (h)(1) of this AD. This may be done by inserting a copy of figure 3 to paragraph (h)(1) of this AD into the existing AFM.

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    Figure 3 to paragraph (h)(1)— AFM Limitations Revision

    (2) Within 2 days after March 16, 2022 (the effective date of AD 2022–06–16): Revise the Operating Procedures Section of the existing AFM to include the information specified in figure 4 to paragraph (h)(2) of this AD. This may be done by inserting a copy of figure 4 to paragraph (h)(2) of this AD into the existing AFM.

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    Figure 4 to paragraph (h)(2)— AFM Operating Procedures Revision

    (i) New Requirement: AFM Revision for Non-Radio Altimeter Tolerant Airplanes

    For non-radio altimeter tolerant airplanes, do the actions specified in paragraphs (i)(1) and (2) of this AD.

    (1) On or before June 30, 2023, revise the Limitations Section of the existing AFM to include the information specified in figure 5 to paragraph (i) of this AD. This may be done by inserting a copy of figure 5 to paragraph (i) of this AD into the existing AFM. Incorporating the AFM revision required by this paragraph terminates the AFM revision required by paragraph (h)(1) of this AD.

    (2) Before further flight after incorporating the limitations specified in figure 5 to paragraph (i) of this AD, remove the AFM revision required by paragraph (h)(1) of this AD.

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    Figure 5 to paragraph (i)— AFM Revision for Non-Radio Altimeter Tolerant Airplanes

    (j) New Requirement: AFM Revision for Radio Altimeter Tolerant Airplanes

    For radio altimeter tolerant airplanes, do the actions specified in paragraphs (j)(1) and (2) of this AD.

    (1) On or before June 30, 2023, revise the Limitations Section of the existing AFM to include the information specified in figure 6 to paragraph (j) of this AD. This may be done by inserting a copy of figure 6 to paragraph (j) of this AD into the existing AFM. Incorporating the AFM revision required by this paragraph terminates the AFM revision required by paragraph (h)(1) of this AD.

    (2) Before further flight after incorporating the limitations specified in figure 6 to paragraph (j) of this AD, remove the AFM revision required by paragraph (h)(1) of this AD.

    Figure 6 to paragraph (j)— AFM Revision for Radio Altimeter Tolerant Airplanes

    (k) Alternative Methods of Compliance (AMOCs)

    (1) The Manager, Operational Safety 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 Operational Safety Branch, send it to the attention of the person identified in paragraph (l) of this AD. Information may be emailed to: AMOC@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) AMOCs approved for AD 2021–23–12, Amendment 39–21810 (86 FR 69984, December 9, 2021), providing relief for specific radio altimeter installations are approved as AMOCs for the requirements specified in paragraph (h) of this AD until June 30, 2023.

    (l) Related Information

    For more information about this AD, contact Brett Portwood, Continued Operational Safety Technical Advisor, COS Program Management Section, Operational Safety Branch, FAA, 3960 Paramount Boulevard, Lakewood, CA 90712–4137; phone: 817–222–5390; email: operationalsafety@faa.gov.

    (m) Material Incorporated by Reference

    None.

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    Issued on June 9, 2023.

    Michael Linegang,

    Acting Director, Compliance & Airworthiness Division, Aircraft Certification Service.

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    BILLING CODE 4910–13–P

    [FR Doc. 2023–13149 Filed 6–16–23; 11:15 am]

    BILLING CODE 4910–13–C

Document Information

Effective Date:
6/21/2023
Published:
06/21/2023
Department:
Federal Aviation Administration
Entry Type:
Rule
Action:
Final rule.
Document Number:
2023-13149
Dates:
This AD is effective June 21, 2023.
Pages:
40003-40010 (8 pages)
Docket Numbers:
Docket No. FAA-2023-0922, Project Identifier AD-2022-01431-T, Amendment 39-22472, AD 2023-12-14
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:
2023-13149.pdf
CFR: (1)
14 CFR 39.13