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Published 2023-06-21 · Federal Register document 2023-13152

Airworthiness Directives; The Boeing Company Airplanes

Publication summary

The FAA is superseding Airworthiness Directive (AD) 2022-03- 20, which applied to all The Boeing Company Model 737-8, 737-9, and 737-8200 airplanes. AD 2022-03-20 required revising the limitations and operating procedures sections of the existing airplane flight manual (AFM) to incorporate limitations prohibiting the use of certain minimum equipment list (MEL) items, and to incorporate operating procedures for calculating takeoff and landing distances, when in the presence of interference from wireless broadband operations in the 3.7-3.98 GHz frequency band (5G C-Band) as identified by Notices to Air Missions (NOTAMs). Since the FAA issued AD 2022-03-20, the FAA determined that additional limitations are needed due to the continued deployment of new 5G C-Band base 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 prohibiting the use of certain MEL items, and would retain the operating procedures from AD 2022-03-20 for calculating takeoff and landing distances, due to the presence of 5G C-Band interference. The FAA is issuing this AD to address the unsafe condition on these products.

Why this record is shown

Source: Federal Register annual FAA metadata. Acquired 2026-09-03T22:24:14.395624+00:00. The title, summary and date are source facts.

Source revision
federal_register_ad_metadata_2023-81e907e5105d0f2c
Source row
results[168]
Raw source SHA-256
81e907e5105d0f2c522e15b6fa8c7277117367b7f70b363862619549836b75e8

Final-rule publication

Recorded publication clauses

AD identifier printed in this edition
2023-12-11
Effective date printed in this edition
2023-06-21
Read 13 complete recorded clauses
Effective Date
(a) Effective Date

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

Exact source excerpt. Text positions 12810–12897, end exclusive, in the original decoded publication. SHA-256: 44496e2be8ee81ff755775b439c4ef8e85827c01770f7963d904e5bc8e656149

Affected ADs
(b) Affected ADs

    This AD replaces AD 2022-03-20, Amendment 39-21937 (87 FR 4787, 
January 31, 2022) (AD 2022-03-20).

Exact source excerpt. Text positions 12897–13020, end exclusive, in the original decoded publication. SHA-256: d34d3eb0d4eb4b8ac64ef46035b9a26821e211418d6fedb78739da0058f3731a

Applicability wording · Applicability
(c) Applicability

    This AD applies to all The Boeing Company 737-8, 737-9, and 737-
8200 airplanes, certificated in any category.

Exact source excerpt. Text positions 13020–13155, end exclusive, in the original decoded publication. SHA-256: 9dfe0fb67ca2481b27a8e33d031fbb3707ac3dd6a305fa8582644263563eddf3

Subject
(d) Subject

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

Exact source excerpt. Text positions 13155–13237, end exclusive, in the original decoded publication. SHA-256: 0542bcd80d4296f1663f9c1a9ee6733c7599b54c556ebcd2abd87a0d6015adff

Unsafe Condition
(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 takeoffs and landings, as a result of this interference, 
certain airplane systems may not properly

[[Page 40013]]

function, resulting in longer than normal landing or rejected 
takeoff distances due to the effect on thrust reverser deployment, 
spoilers, speedbrake deployment, and increased idle thrust, 
regardless of the approach type or weather. The FAA is issuing this 
AD to address degraded deceleration performance, which could lead to 
a runway excursion.

Exact source excerpt. Text positions 13237–14003, end exclusive, in the original decoded publication. SHA-256: 3149367ac63c6eb0798d19fe7054dad17cb65714f356aed9097e6b5ae2574de6

Compliance
(f) Compliance

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

Exact source excerpt. Text positions 14003–14105, end exclusive, in the original decoded publication. SHA-256: 00fbfa31932483f627d0ce0a11cbd2e35e15d9231842b91ac85623ce533912d3

Definitions
(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.
BILLING CODE 4910-13-P

Figure 1 to paragraph (g)(2)(i)--Fundamental Effective Isotropic PSD 
at Outside Interface of Aircraft Antenna
[GRAPHIC] [TIFF OMITTED] TR21JN23.108

    (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.


[[Page 40014]]


Figure 2 to paragraph (g)(2)(ii)--Spurious Effective Isotropic PSD 
at Outside Interface of Aircraft Antenna
[GRAPHIC] [TIFF OMITTED] TR21JN23.109

    (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.
    (4) Runway condition codes are defined in figure 3 to paragraph 
(g)(4) of this AD.

Figure 3 to paragraph (g)(4)--Runway Condition Codes

[[Page 40015]]

[GRAPHIC] [TIFF OMITTED] TR21JN23.110

Exact source excerpt. Text positions 14105–15796, end exclusive, in the original decoded publication. SHA-256: 39929950e8ff510de3be62c3063fe1b91021c16adf3c0e71757889ec49c07f76

Retained Airplane Flight Manual (AFM) Revision
(h) Retained Airplane Flight Manual (AFM) Revision

    This paragraph restates the requirements of paragraph (h) of AD 
2022-03-20.
    (1) Within 2 days after January 31, 2022 (the effective date of 
AD 2022-03-20): Revise the Limitations Section of the existing AFM 
to include the information specified in figure 4 to paragraph (h)(1) 
of this AD. This may be done by inserting a copy of figure 4 to 
paragraph (h)(1) of this AD into the existing AFM.

Figure 4 to paragraph (h)(1)--AFM Limitations Revisions
[GRAPHIC] [TIFF OMITTED] TR21JN23.111


[[Page 40016]]


    (2) Within 2 days after January 31, 2022 (the effective date of 
AD 2022-03-20): Revise the Operating Procedures Section of the 
existing AFM to include the information specified in figure 5 to 
paragraph (h)(2) of this AD. This may be done by inserting a copy of 
figure 5 to paragraph (h)(2) of this AD into the existing AFM.

Figure 5 to paragraph (h)(2)--AFM Operating Procedures Revision
[GRAPHIC] [TIFF OMITTED] TR21JN23.112


[[Page 40017]]


[GRAPHIC] [TIFF OMITTED] TR21JN23.113


[[Page 40018]]


[GRAPHIC] [TIFF OMITTED] TR21JN23.114


[[Page 40019]]


[GRAPHIC] [TIFF OMITTED] TR21JN23.115


[[Page 40020]]


[GRAPHIC] [TIFF OMITTED] TR21JN23.116


[[Page 40021]]


[GRAPHIC] [TIFF OMITTED] TR21JN23.117

Exact source excerpt. Text positions 15796–17087, end exclusive, in the original decoded publication. SHA-256: 1b67e957a11c8c0513b81536a4f38a12e74bdded10cfe6d7c18b69d22fdf6f1f

New Requirement: AFM Revision for Non-Radio Altimeter Tolerant Airplanes
(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 6 
to paragraph (i) of this AD. This may be done by inserting a copy of 
figure 6 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 6 to paragraph (i) of this AD, remove the AFM 
revision required by paragraph (h)(1) of this AD.

[[Page 40022]]

Figure 6 to paragraph (i)--AFM Revision for Non-Radio Altimeter 
Tolerant Airplanes
[GRAPHIC] [TIFF OMITTED] TR21JN23.118

Exact source excerpt. Text positions 17087–18002, end exclusive, in the original decoded publication. SHA-256: 2ed850bb220748cac65311bd666c11a5d8f91035306504f8bf09f600e8ed60d8

New Requirement: AFM Revision for 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 7 
to paragraph (j) of this AD. This may be done by inserting a copy of 
figure 7 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 7 to paragraph (j) of this AD, remove the AFM 
revision required by paragraph (h)(1) of this AD.

[[Page 40023]]

Figure 7 to paragraph (j)--AFM Revision for Radio Altimeter Tolerant 
Airplanes
[GRAPHIC] [TIFF OMITTED] TR21JN23.119

Exact source excerpt. Text positions 18002–18905, end exclusive, in the original decoded publication. SHA-256: f4ebb7b7e404ede4e90b2afea34bf5e684762e05e97fa6d9182efee8537d6e87

Alternative Methods of Compliance (AMOCs)
(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: [email protected].
    (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.

Exact source excerpt. Text positions 18905–19898, end exclusive, in the original decoded publication. SHA-256: c79910803d607f866fd97662e3c70fa5dc27ea9de5468755169e82708f1f67dc

Related Information
(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: 
[email protected].

Exact source excerpt. Text positions 19898–20202, end exclusive, in the original decoded publication. SHA-256: 8499219395f559bb5610fc192a6a3e2c2b18dd89126f3bb18b0bcbefef651ce4

Material Incorporated by Reference
(m) Material Incorporated by Reference

    None.

Exact source excerpt. Text positions 20202–20253, end exclusive, in the original decoded publication. SHA-256: cffe37e8221668106206d572d73e6b4dfd97b02ec8d7400d43c985459042d6b5

Explicit historical replacement wording

Find all recorded historical references to AD 2023-12-11 · 0 printed reference observations in this pinned collection.

These are observations from one dated publication. Current legal status is unknown; aircraft applicability, installed configuration, compliance and burden require separate evidence. Missing or unparsed conditions remain unknown.

Why these observations are shown

They were extracted offline from the same immutable official HTML source as the complete recorded text. The dated source wording, original text coordinates and exact quote digests are retained. PDF/text agreement and current regulatory effect have not been qualified.

Observation revision: whole-ad-publication-clause-observations-1.0.1. Text SHA-256: 456533e800817908f414a0c7ad608ed3a672ac8df6ebbb8bbec8015f0cf189a3. Source manifest: 1a6896f88a10cd66585bb6c464a0c702b3d4cbef2974f71b9fd0a0f89af26fbf.

Official source · 2023-06-21

Publication text

This is the complete recorded text of this dated publication.

Current legal effect is unknown. Aircraft applicability, installed configuration and compliance require separate evidence. PDF/text agreement has not been evaluated.

Read the complete official publication text
[Federal Register Volume 88, Number 118 (Wednesday, June 21, 2023)]
[Rules and Regulations]
[Pages 40011-40023]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2023-13152]



[[Page 40011]]

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

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2023-0671; Project Identifier AD-2022-01428-T; 
Amendment 39-22469; AD 2023-12-11]
RIN 2120-AA64


Airworthiness Directives; The Boeing Company Airplanes

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Final rule.

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

SUMMARY: The FAA is superseding Airworthiness Directive (AD) 2022-03-
20, which applied to all The Boeing Company Model 737-8, 737-9, and 
737-8200 airplanes. AD 2022-03-20 required revising the limitations and 
operating procedures sections of the existing airplane flight manual 
(AFM) to incorporate limitations prohibiting the use of certain minimum 
equipment list (MEL) items, and to incorporate operating procedures for 
calculating takeoff and landing distances, when in the presence of 
interference from wireless broadband operations in the 3.7-3.98 GHz 
frequency band (5G C-Band) as identified by Notices to Air Missions 
(NOTAMs). Since the FAA issued AD 2022-03-20, the FAA determined that 
additional limitations are needed due to the continued deployment of 
new 5G C-Band base 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 prohibiting the use of certain 
MEL items, and would retain the operating procedures from AD 2022-03-20 
for calculating takeoff and landing distances, 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-2023-0671; 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.

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: [email protected].

SUPPLEMENTARY INFORMATION: 

Background

    The FAA issued a notice of proposed rulemaking (NPRM) to amend 14 
CFR part 39 to supersede AD 2022-03-20, Amendment 39-21937 (87 FR 4787, 
January 31, 2022) (AD 2022-03-20). AD 2022-03-20 applied to all The 
Boeing Company Model 737-8, 737-9, and 737-8200 airplanes. The NPRM 
published in the Federal Register on May 3, 2023 (88 FR 27786). 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 takeoffs and 
landings, as a result of this interference, certain airplane systems 
may not properly function, resulting in longer than normal landing or 
rejected takeoff distances due to the effect on thrust reverser 
deployment, spoilers, speedbrake deployment, and increased idle thrust, 
regardless of the approach type or weather.
    In the NPRM, the FAA proposed to retain the requirements of AD 
2022-03-20 until June 30, 2023. On or before June 30, 2023, the FAA 
proposed to require replacing those AFM limitations with limitations 
prohibiting the same dispatching or releasing to airports, and takeoff 
or landings on runways, and use of certain MEL items at all airports 
for non-radio altimeter tolerant airplanes. For radio altimeter 
tolerant airplanes, the FAA proposed to allow the prohibited operations 
at 5G C-Band mitigated airports (5G CMAs) as identified in an FAA 
Domestic Notice. The FAA proposed this AD to address degraded 
deceleration performance, which could lead to a runway excursion.

Discussion of Final Airworthiness Directive

Comments

    The FAA provided the public with an opportunity to comment on the 
proposed AD and received comments from four commenters. The following 
presents the comments received on the NPRM and the FAA's response to 
each comment.

Support for NPRM

    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 AD.

Request To Extend Compliance Time

    Comment summary: Southwest Airlines and American Airlines expressed 
concern regarding the compliance time for the proposed actions and 
requested the FAA revise the AD to provide a minimum of 30 days from 
the effective date of the AD.
    FAA response: The FAA understands the commenters' concerns and made 
every effort to publish this AD as soon as possible. After refraining 
from operating at their FCC-authorized levels for a year and a half, 
wireless companies are now able to operate at higher levels, yet still 
not at the levels authorized. Specifically, wireless companies expect 
to operate their networks in urban areas with minimal restrictions due 
to the completion of retrofits. Additionally, the FAA anticipates 19 
additional telecommunication companies will begin transmitting in the 
C-Band after June 30, 2023. Although the FAA continues to work with the 
companies that intend to transmit in the 3.7-3.98-GHz band near 5G 
CMAs, the FAA has no agreement with those companies to provide the FAA 
with tower locations and other information necessary to support the 
current NOTAM/AMOC process. Therefore, the FAA will not be able to 
extend the June 30, 2023, date.

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,

[[Page 40012]]

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 longer 
than normal landing or rejected takeoff distances due to the effect on 
thrust reverser deployment, spoilers, speedbrake deployment, and 
increased idle thrust, regardless of the approach type or weather. 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 2022-03-20, 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 276 airplanes of U.S. 
registry. The FAA estimates the following costs to comply with this AD:

                                                 Estimated Costs
----------------------------------------------------------------------------------------------------------------
                                                                                     Cost per      Cost on U.S.
                Action                         Labor cost           Parts cost        product        operators
----------------------------------------------------------------------------------------------------------------
AFM revision (retained actions from AD  1 work-hour \1\ x $85                 $0             $85         $23,460
 2022-03-20).                            per hour = $85.
New AFM revisions (new action)........  1 work-hour x $85 per                  0              85      \2\ 23,460
                                         hour = $85.
----------------------------------------------------------------------------------------------------------------
\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 737-
  8, 737-9, or 737-8200 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.

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

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) 2022-03-20, Amendment 39-21937 
(87 FR 4787, January 31, 2022), and
0
b. Adding the following new AD:

2023-12-11 The Boeing Company: Amendment 39-22469; Docket No. FAA-
2023-0671; Project Identifier AD-2022-01428-T.

(a) Effective Date

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

(b) Affected ADs

    This AD replaces AD 2022-03-20, Amendment 39-21937 (87 FR 4787, 
January 31, 2022) (AD 2022-03-20).

(c) Applicability

    This AD applies to all The Boeing Company 737-8, 737-9, and 737-
8200 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 takeoffs and landings, as a result of this interference, 
certain airplane systems may not properly

[[Page 40013]]

function, resulting in longer than normal landing or rejected 
takeoff distances due to the effect on thrust reverser deployment, 
spoilers, speedbrake deployment, and increased idle thrust, 
regardless of the approach type or weather. The FAA is issuing this 
AD to address degraded deceleration performance, which could lead to 
a runway excursion.

(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.
BILLING CODE 4910-13-P

Figure 1 to paragraph (g)(2)(i)--Fundamental Effective Isotropic PSD 
at Outside Interface of Aircraft Antenna
[GRAPHIC] [TIFF OMITTED] TR21JN23.108

    (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.


[[Page 40014]]


Figure 2 to paragraph (g)(2)(ii)--Spurious Effective Isotropic PSD 
at Outside Interface of Aircraft Antenna
[GRAPHIC] [TIFF OMITTED] TR21JN23.109

    (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.
    (4) Runway condition codes are defined in figure 3 to paragraph 
(g)(4) of this AD.

Figure 3 to paragraph (g)(4)--Runway Condition Codes

[[Page 40015]]

[GRAPHIC] [TIFF OMITTED] TR21JN23.110

(h) Retained Airplane Flight Manual (AFM) Revision

    This paragraph restates the requirements of paragraph (h) of AD 
2022-03-20.
    (1) Within 2 days after January 31, 2022 (the effective date of 
AD 2022-03-20): Revise the Limitations Section of the existing AFM 
to include the information specified in figure 4 to paragraph (h)(1) 
of this AD. This may be done by inserting a copy of figure 4 to 
paragraph (h)(1) of this AD into the existing AFM.

Figure 4 to paragraph (h)(1)--AFM Limitations Revisions
[GRAPHIC] [TIFF OMITTED] TR21JN23.111


[[Page 40016]]


    (2) Within 2 days after January 31, 2022 (the effective date of 
AD 2022-03-20): Revise the Operating Procedures Section of the 
existing AFM to include the information specified in figure 5 to 
paragraph (h)(2) of this AD. This may be done by inserting a copy of 
figure 5 to paragraph (h)(2) of this AD into the existing AFM.

Figure 5 to paragraph (h)(2)--AFM Operating Procedures Revision
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[[Page 40017]]


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[[Page 40018]]


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[[Page 40019]]


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[[Page 40020]]


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[[Page 40021]]


[GRAPHIC] [TIFF OMITTED] TR21JN23.117

(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 6 
to paragraph (i) of this AD. This may be done by inserting a copy of 
figure 6 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 6 to paragraph (i) of this AD, remove the AFM 
revision required by paragraph (h)(1) of this AD.

[[Page 40022]]

Figure 6 to paragraph (i)--AFM Revision for Non-Radio Altimeter 
Tolerant Airplanes
[GRAPHIC] [TIFF OMITTED] TR21JN23.118

(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 7 
to paragraph (j) of this AD. This may be done by inserting a copy of 
figure 7 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 7 to paragraph (j) of this AD, remove the AFM 
revision required by paragraph (h)(1) of this AD.

[[Page 40023]]

Figure 7 to paragraph (j)--AFM Revision for Radio Altimeter Tolerant 
Airplanes
[GRAPHIC] [TIFF OMITTED] TR21JN23.119

(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: [email protected].
    (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: 
[email protected].

(m) Material Incorporated by Reference

    None.

    Issued on June 9, 2023.
Michael Linegang,
Acting Director, Compliance & Airworthiness Division, Aircraft 
Certification Service.
[FR Doc. 2023-13152 Filed 6-16-23; 11:15 am]
BILLING CODE 4910-13-C


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