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Published 2022-01-27 · Federal Register document 2022-01695

Airworthiness Directives; The Boeing Company Airplanes

Publication summary

The FAA is adopting a new airworthiness directive (AD) for all The Boeing Company Model 747-8F and 747-8 series airplanes and Model 777 airplanes. 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 recent determination that this interference may affect multiple airplane systems using radio altimeter data, including the pitch control laws, including those that provide tail strike protection, regardless of the approach type or weather. This AD requires revising the limitations section of the existing airplane flight manual (AFM) to incorporate limitations prohibiting dispatching or releasing to airports, and approaches or landings on runways, when in the presence of 5G C-Band interference as identified by Notices to Air Missions (NOTAMs). 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 2026-09-03T22:24:11.345539+00:00. The title, summary and date are source facts.

Source revision
federal_register_ad_metadata_2022-c0cc5a172b1306fa
Source row
results[35]
Raw source SHA-256
c0cc5a172b1306fa2cd8dc66863122ada13332e685d87687bd0becf2dab37a5e

Final-rule publication

Recorded publication clauses

AD identifier printed in this edition
2022-03-05
Effective date printed in this edition
2022-01-27
Read 10 complete recorded clauses
Effective Date
(a) Effective Date

    This airworthiness directive (AD) is effective January 27, 2022.

Exact source excerpt. Text positions 17210–17300, end exclusive, in the original decoded publication. SHA-256: 6851f62bfe7e40ffb9bdc3b5a48ef31e4b629bbf70d1d2e00b4f4b84f1328db0

Affected ADs
(b) Affected ADs

    None.

Exact source excerpt. Text positions 17300–17329, end exclusive, in the original decoded publication. SHA-256: 871a4afc60ceeae06e8010585055188633d616078500c45937092bfe892239c0

Applicability wording · Applicability
(c) Applicability

    This AD applies to The Boeing Company airplanes identified in 
paragraphs (c)(1) and (2) of this AD, certificated in any category.
    (1) Model 747-8F and 747-8 series airplanes.
    (2) Model 777-200, -200LR, -300, -300ER, and 777F series 
airplanes.

Exact source excerpt. Text positions 17329–17606, end exclusive, in the original decoded publication. SHA-256: 1a125b911529bc5ccad7d0878c112220eb81bb05349781252abb41ada64d370b

Subject
(d) Subject

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

Exact source excerpt. Text positions 17606–17688, 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 
this interference may affect other airplane systems using radio 
altimeter data, including the pitch control laws, including those 
that provide tail strike protection, regardless of the approach type 
or weather. The FAA is issuing this AD to address missing or 
erroneous radio altimeter data, which, in combination with multiple 
flight deck effects, could lead to loss of continued safe flight and 
landing.

Exact source excerpt. Text positions 17688–18390, end exclusive, in the original decoded publication. SHA-256: 437c36fd1143530eac3d82d4dc8a1cf8f6bab5612adbe4126f1ca0255d4acff1

Compliance
(f) Compliance

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

Exact source excerpt. Text positions 18390–18492, end exclusive, in the original decoded publication. SHA-256: 00fbfa31932483f627d0ce0a11cbd2e35e15d9231842b91ac85623ce533912d3

Airplane Flight Manual (AFM) Revision
(g) Airplane Flight Manual (AFM) Revision

    Within 2 days after the effective date of this AD: Revise the 
Limitations Section of the existing AFM to include the information 
specified in figure 1 to paragraph (g) of this AD. This may be done 
by inserting a copy of figure 1 to paragraph (g) of this AD into the 
existing AFM.
[GRAPHIC] [TIFF OMITTED] TR27JA22.007

    Note 1 to paragraph (g): Additional information about the unsafe 
condition identified in this AD can be found in Boeing Multi 
Operator Messages MOM-MOM-22-0024-01B(R2), dated January 18, 2022, 
and MOM-MOM-22-0039-01B(R1), dated January 18, 2022, for Boeing 
Model 777 airplanes and Model 747-8F and 747-8 series airplanes, 
respectively.

Exact source excerpt. Text positions 18492–19208, end exclusive, in the original decoded publication. SHA-256: 8bdf1ca379171fd99af77060b574a765c2a8b6e7a825717fe04297e1d400f131

Alternative Methods of Compliance (AMOCs)
(h) 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 paragraph (i)(1) 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 provisions of 
this AD.

Exact source excerpt. Text positions 19208–20143, end exclusive, in the original decoded publication. SHA-256: 1faee9c80eddbcfb3a962c61fa675d2ee8fdd5f3b2080de7cc43ad3263f0f155

Related Information
(i) Related Information

    (1) For more information about this AD, contact Dean Thompson, 
Senior Aerospace Engineer, Systems and Equipment Section, FAA, 
Seattle ACO Branch, 2200 South 216th St., Des Moines, WA 98198; 
phone and fax: 206-231-3165; email: [email protected].
    (2) For service information identified in this AD that is not 
incorporated by reference, 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.

Exact source excerpt. Text positions 20143–20730, end exclusive, in the original decoded publication. SHA-256: 2975523eb98d20b7d3e4b43513d4f8eb7a6465ff2e9eb4952e5357e981b8ca48

Material Incorporated by Reference
(j) Material Incorporated by Reference

    None.

Exact source excerpt. Text positions 20730–20781, end exclusive, in the original decoded publication. SHA-256: 9d583edbcf085b1fae94c8be8274ba3ce59b91db7bf15c5f5fd81fff2816eec7

No replacement link has been established from this edition. The complete historical rule chain and current legal effect remain unknown.

Find all recorded historical references to AD 2022-03-05 · 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: 5cff0f973c2cc63a214103078bfb74fad9bd7b779c8563f9aa63c8cd5c856d8b. Source manifest: 15d5f49f421fc5d02d01aad0fc1968f1c616bbd851e5e1551e78cf45fbc938b6.

Official source · 2022-01-27

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 87, Number 18 (Thursday, January 27, 2022)]
[Rules and Regulations]
[Pages 4150-4153]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2022-01695]


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

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2022-0012; Project Identifier AD-2022-00057-T; 
Amendment 39-21922; AD 2022-03-05]
RIN 2120-AA64


Airworthiness Directives; The Boeing Company Airplanes

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Final rule; request for comments.

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

SUMMARY: The FAA is adopting a new airworthiness directive (AD) for all 
The Boeing Company Model 747-8F and 747-8 series airplanes and Model 
777 airplanes. 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 recent determination 
that this interference may affect multiple airplane systems using radio 
altimeter data, including the pitch control laws, including those that 
provide tail strike protection, regardless of the approach type or 
weather. This AD requires revising the limitations section of the 
existing airplane flight manual (AFM) to incorporate limitations 
prohibiting dispatching or releasing to airports, and approaches or 
landings on runways, when in the presence of 5G C-Band interference as 
identified by Notices to Air Missions (NOTAMs). The FAA is issuing this 
AD to address the unsafe condition on these products.

DATES: This AD is effective January 27, 2022.

[[Page 4151]]

    The FAA must receive comments on this AD by March 14, 2022.

ADDRESSES: You may send comments, using the procedures found in 14 CFR 
11.43 and 11.45, by any of the following methods:
    <bullet> Federal eRulemaking Portal: Go to https://www.regulations.gov. Follow the instructions for submitting comments.
    <bullet> Fax: 202-493-2251.
    <bullet> Mail: U.S. Department of Transportation, Docket 
Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New 
Jersey Avenue SE, Washington, DC 20590.
    <bullet> Hand Delivery: Deliver to Mail address above between 9 
a.m. and 5 p.m., Monday through Friday, except Federal holidays.

Examining the AD Docket

    You may examine the AD docket at https://www.regulations.gov by 
searching for and locating Docket No. FAA-2022-0012; 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 street address for the 
Docket Operations is listed above.

FOR FURTHER INFORMATION CONTACT: Dean Thompson, Senior Aerospace 
Engineer, Systems and Equipment Section, FAA, Seattle ACO Branch, 2200 
South 216th St., Des Moines, WA 98198; phone and fax: 206-231-3165; 
email: [email protected].

SUPPLEMENTARY INFORMATION:

Background

    In March 2020, the United States Federal Communications Commission 
(FCC) adopted final rules authorizing flexible use of the 3.7-3.98 GHz 
band for next generation services, including 5G and other advanced 
spectrum-based services.\1\ Pursuant to these rules, C-Band wireless 
broadband deployment is permitted to occur in phases with the 
opportunity for operations in the lower 0.1 GHz of the band (3.7-3.8 
GHz) in certain markets as early as January 19, 2022. This AD refers to 
``5G C-Band'' interference, but wireless broadband technologies, other 
than 5G, may use the same frequency band.\2\ These other uses of the 
same frequency band are within the scope of this AD since they would 
introduce the same risk of radio altimeter interference as 5G C-Band.
---------------------------------------------------------------------------

    \1\ The FCC's rules did not make C-Band wireless broadband 
available in Alaska, Hawaii, and the U.S. Territories.
    \2\ The regulatory text of the AD uses the term ``5G C-Band'' 
which, for purposes of this AD, has the same meaning as ``5G'', ``C-
Band'' and ``3.7-3.98 GHz.''
---------------------------------------------------------------------------

    The radio altimeter is an important aircraft instrument, and its 
intended function is to provide direct height-above-terrain/water 
information to a variety of aircraft systems. Commercial aviation radio 
altimeters operate in the 4.2-4.4 GHz band, which is separated by 0.22 
GHz from the C-Band telecommunication systems in the 3.7-3.98 GHz band. 
The radio altimeter is more precise than a barometric altimeter and for 
that reason is used where aircraft height over the ground needs to be 
precisely measured, such as autoland, manual landings, or other low 
altitude operations. The receiver on the radio altimeter is typically 
highly accurate, however it may deliver erroneous results in the 
presence of out-of-band radio frequency emissions from other frequency 
bands. The radio altimeter must detect faint signals reflected off the 
ground to measure altitude, in a manner similar to radar. Out-of-band 
signals could significantly degrade radio altimeter functions during 
critical phases of flight, if the altimeter is unable to sufficiently 
reject those signals.
    The FAA issued AD 2021-23-12, Amendment 39-21810 (86 FR 69984, 
December 9, 2021) (AD 2021-23-12) to address the effect of 5G C-Band 
interference on all transport and commuter category airplanes equipped 
with a radio (also known as radar) altimeter. AD 2021-23-12 requires 
revising the limitations section of the existing AFM to incorporate 
limitations prohibiting certain operations, which require radio 
altimeter data to land in low visibility conditions, when in the 
presence of 5G C-Band interference as identified by NOTAM. The FAA 
issued AD 2021-23-12 because radio altimeter anomalies that are 
undetected by the automation or pilot, particularly close to the ground 
(e.g., landing flare), could lead to loss of continued safe flight and 
landing.
    Since the FAA issued AD 2021-23-12, Boeing has continued to 
evaluate potential 5G C-band interference on aircraft systems that rely 
on radio altimeter inputs. As a result of this ongoing evaluation, 
Boeing issued Boeing Multi Operator Messages MOM-MOM-22-0024-01B(R2), 
dated January 18, 2022, and MOM-MOM-22-0039-01B(R1), dated January 18, 
2022, for Boeing Model 777 airplanes and Model 747-8F and 747-8 series 
airplanes, respectively.
    Based on Boeing's data, the FAA identified an additional hazard 
presented by 5G C-band interference on The Boeing Company Model 747-8F 
and 747-8 series airplanes and Model 777 airplanes. The FAA determined 
that anomalies due to 5G C-Band interference may affect multiple 
airplane systems using radio altimeter data, including the pitch 
control laws, including control laws that provide tail strike 
protection, regardless of the approach type or weather. These anomalies 
may not be evident until very low altitudes. Due to 5G C-Band 
interference, missing or erroneous radio altimeter data used by the 
flight control system may result in uncommanded, inappropriate pitch 
inputs, adversely affecting controllability. This interference could 
also cause multiple erroneous flight deck effects, including misleading 
flight director information and erroneous autothrottle behavior and 
Flight Mode Annunciations. These flight deck effects, when combined 
with the effects of the uncommanded, inappropriate pitch inputs, could 
affect the flightcrew's ability to accomplish continued safe flight and 
landing. Other systems that could be impacted by this missing or 
erroneous data, and contribute to this hazard, include, but are not 
limited to: Autopilot flight director system; autothrottle system; 
engines; flight controls; flight instruments; traffic alert and 
collision avoidance system (TCAS); ground proximity warning system 
(GPWS); and configuration warnings.
    In sum, 5G C-Band interference, which may result in missing or 
erroneous radio altimeter data provided to the airplane's flight 
control computers where pitch control and other laws reside, in 
combination with multiple flight deck effects, could result in 
uncommanded, inappropriate pitch inputs, which are especially hazardous 
at low altitudes, and loss of continued safe flight and landing. This 
is an unsafe condition.
    This AD requires revising the limitations section of the existing 
AFM to incorporate limitations prohibiting dispatching or releasing to 
airports, and approaches or landings on runways, when in the presence 
of 5G C-Band interference as identified by NOTAMs.
    The FAA is issuing this AD to address the unsafe condition on these 
products.

FAA's Determination

    The FAA is issuing this AD because the agency has determined the 
unsafe condition described previously is likely to exist or develop in 
other products of the same type design.

AD Requirements

    This AD requires revising the limitations section of the existing 
AFM to incorporate limitations prohibiting dispatching or releasing to 
airports, and approaches or landings on runways,

[[Page 4152]]

when in the presence of 5G C-Band interference as identified by NOTAMs.

Compliance With AFM Revisions

    Section 91.9 prohibits any person from operating a civil aircraft 
without complying with the operating limitations specified in the AFM. 
FAA regulations also require operators to furnish pilots with any 
changes to the AFM (14 CFR 121.137) and pilots in command to be 
familiar with the AFM (14 CFR 91.505).

Interim Action

    The FAA considers this AD to be an interim action. If final action 
is later identified, the FAA might consider further rulemaking.

Justification for Immediate Adoption and Determination of the Effective 
Date

    Section 553(b)(3)(B) of the Administrative Procedure Act (APA) (5 
U.S.C. 551 et seq.) authorizes agencies to dispense with notice and 
comment procedures for rules when the agency, for ``good cause,'' finds 
that those procedures are ``impracticable, unnecessary, or contrary to 
the public interest.'' Under this section, an agency, upon finding good 
cause, may issue a final rule without providing notice and seeking 
comment prior to issuance. Further, section 553(d) of the APA 
authorizes agencies to make rules effective in less than thirty days, 
upon a finding of good cause.
    An unsafe condition exists that requires the immediate adoption of 
this AD without providing an opportunity for public comments prior to 
adoption. The FAA has found that the risk to the flying public 
justifies forgoing notice and comment prior to adoption of this rule 
because missing or erroneous radio altimeter data provided (as a result 
of 5G C-Band interference) to the airplane's pitch control laws, in 
combination with multiple flight deck effects, could lead to 
uncommanded, inappropriate pitch inputs, and the loss of continued safe 
flight and landing. The urgency is based on the hazard presented by 
such pitch inputs occurring at low altitudes, and on C-Band wireless 
broadband deployment, which is expected to occur in phases with 
operations beginning as soon as January 19, 2022. Accordingly, notice 
and opportunity for prior public comment are impracticable and contrary 
to the public interest pursuant to 5 U.S.C. 553(b)(3)(B).
    In addition, the FAA finds that good cause exists pursuant to 5 
U.S.C. 553(d) for making this amendment effective in less than 30 days, 
for the same reasons the FAA found good cause to forgo notice and 
comment.

Comments Invited

    The FAA invites you to send any written data, views, or arguments 
about this final rule. Send your comments to an address listed under 
ADDRESSES. Include Docket No. FAA-2022-0012 and Project Identifier AD-
2022-00057-T at the beginning of your comments. The most helpful 
comments reference a specific portion of the final rule, explain the 
reason for any recommended change, and include supporting data. The FAA 
will consider all comments received by the closing date and may amend 
this final rule because of those comments.
    Except for Confidential Business Information (CBI) as described in 
the following paragraph, and other information as described in 14 CFR 
11.35, the FAA will post all comments received, without change, to 
https://www.regulations.gov, including any personal information you 
provide. The agency will also post a report summarizing each 
substantive verbal contact received about this final rule.

Confidential Business Information

    CBI is commercial or financial information that is both customarily 
and actually treated as private by its owner. Under the Freedom of 
Information Act (FOIA) (5 U.S.C. 552), CBI is exempt from public 
disclosure. If your comments responsive to this AD contain commercial 
or financial information that is customarily treated as private, that 
you actually treat as private, and that is relevant or responsive to 
this AD, it is important that you clearly designate the submitted 
comments as CBI. Please mark each page of your submission containing 
CBI as ``PROPIN.'' The FAA will treat such marked submissions as 
confidential under the FOIA, and they will not be placed in the public 
docket of this AD. Submissions containing CBI should be sent to Dean 
Thompson, Senior Aerospace Engineer, Systems and Equipment Section, 
FAA, Seattle ACO Branch, 2200 South 216th St., Des Moines, WA 98198; 
phone and fax: 206-231-3165; email: [email protected]. Any 
commentary that the FAA receives that is not specifically designated as 
CBI will be placed in the public docket for this rulemaking.

Regulatory Flexibility Act

    The requirements of the Regulatory Flexibility Act (RFA) do not 
apply when an agency finds good cause pursuant to 5 U.S.C. 553 to adopt 
a rule without prior notice and comment. Because the FAA has determined 
that it has good cause to adopt this rule without notice and comment, 
RFA analysis is not required.

Costs of Compliance

    The FAA estimates that this AD affects 336 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..........................  1 work-hour x $85 per                 $0             $85         $28,560
                                         hour = $85.
----------------------------------------------------------------------------------------------------------------

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

[[Page 4153]]

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

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 adding the following new airworthiness 
directive:

2022-03-05 The Boeing Company: Amendment 39-21922 ; Docket No. FAA-
2022-0012; Project Identifier AD-2022-00057-T.

(a) Effective Date

    This airworthiness directive (AD) is effective January 27, 2022.

(b) Affected ADs

    None.

(c) Applicability

    This AD applies to The Boeing Company airplanes identified in 
paragraphs (c)(1) and (2) of this AD, certificated in any category.
    (1) Model 747-8F and 747-8 series airplanes.
    (2) Model 777-200, -200LR, -300, -300ER, and 777F series 
airplanes.

(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 
this interference may affect other airplane systems using radio 
altimeter data, including the pitch control laws, including those 
that provide tail strike protection, regardless of the approach type 
or weather. The FAA is issuing this AD to address missing or 
erroneous radio altimeter data, which, in combination with multiple 
flight deck effects, could lead to loss of continued safe flight and 
landing.

(f) Compliance

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

(g) Airplane Flight Manual (AFM) Revision

    Within 2 days after the effective date of this AD: Revise the 
Limitations Section of the existing AFM to include the information 
specified in figure 1 to paragraph (g) of this AD. This may be done 
by inserting a copy of figure 1 to paragraph (g) of this AD into the 
existing AFM.
[GRAPHIC] [TIFF OMITTED] TR27JA22.007

    Note 1 to paragraph (g): Additional information about the unsafe 
condition identified in this AD can be found in Boeing Multi 
Operator Messages MOM-MOM-22-0024-01B(R2), dated January 18, 2022, 
and MOM-MOM-22-0039-01B(R1), dated January 18, 2022, for Boeing 
Model 777 airplanes and Model 747-8F and 747-8 series airplanes, 
respectively.

(h) 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 paragraph (i)(1) 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 provisions of 
this AD.

(i) Related Information

    (1) For more information about this AD, contact Dean Thompson, 
Senior Aerospace Engineer, Systems and Equipment Section, FAA, 
Seattle ACO Branch, 2200 South 216th St., Des Moines, WA 98198; 
phone and fax: 206-231-3165; email: [email protected].
    (2) For service information identified in this AD that is not 
incorporated by reference, 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.

(j) Material Incorporated by Reference

    None.

    Issued on January 20, 2022.
Gaetano A. Sciortino,
Deputy Director for Strategic Initiatives, Compliance & Airworthiness 
Division, Aircraft Certification Service.
[FR Doc. 2022-01695 Filed 1-25-22; 11:15 am]
BILLING CODE 4910-13-P


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