Published 2023-06-21 · Federal Register document 2023-13149
Airworthiness Directives; The Boeing Company Airplanes
Publication 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 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.
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[166]
- Raw source SHA-256
- 81e907e5105d0f2c522e15b6fa8c7277117367b7f70b363862619549836b75e8
Final-rule publication
Recorded publication clauses
- AD identifier printed in this edition
- 2023-12-14
- 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 11715–11802, end exclusive, in the original decoded publication. SHA-256: 44496e2be8ee81ff755775b439c4ef8e85827c01770f7963d904e5bc8e656149
Affected ADs
(b) Affected ADs
This AD replaces AD 2022-06-16, Amendment 39-21982 (87 FR 14780,
March 16, 2022) (AD 2022-06-16).
Exact source excerpt. Text positions 11802–11924, end exclusive, in the original decoded publication. SHA-256: 8dcbb4afd6fc35cac720c2840e625d6cbfb8c97b7b3fa380c2e3a21e4b434e5f
Applicability wording · Applicability
(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.
Exact source excerpt. Text positions 11924–12151, end exclusive, in the original decoded publication. SHA-256: 12709fa708a0949b998f9e260f76e2e96588836eb30782628332bb368abf2064
Subject
(d) Subject
Air Transport Association (ATA) of America Code 34, Navigation.
Exact source excerpt. Text positions 12151–12233, 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 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.
Exact source excerpt. Text positions 12233–13008, end exclusive, in the original decoded publication. SHA-256: 2a9cf17b14cb7b604eaf3ea038e963a53b101ba4434505c3f3e7ec318c8c4ed6
Compliance
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
Exact source excerpt. Text positions 13008–13110, 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
[[Page 40006]]
Figure 1 to paragraph (g)(2)(i)--Fundamental Effective Isotropic PSD
at Outside Interface of Aircraft Antenna
[GRAPHIC] [TIFF OMITTED] TR21JN23.072
(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 40007]]
Figure 2 to paragraph (g)(2)(ii)--Spurious Effective Isotropic PSD
at Outside Interface of Aircraft Antenna
[GRAPHIC] [TIFF OMITTED] TR21JN23.073
(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.
Exact source excerpt. Text positions 13110–14622, end exclusive, in the original decoded publication. SHA-256: edcf4f18daa281575086515f6b9d631a0475b8aedf410db6d229de95558c9f3e
Retained Airplane Flight Manual (AFM) Revision
(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.
[[Page 40008]]
Figure 3 to paragraph (h)(1)--AFM Limitations Revision
[GRAPHIC] [TIFF OMITTED] TR21JN23.074
(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.
[[Page 40009]]
Figure 4 to paragraph (h)(2)--AFM Operating Procedures Revision
[GRAPHIC] [TIFF OMITTED] TR21JN23.075
Exact source excerpt. Text positions 14622–15641, end exclusive, in the original decoded publication. SHA-256: 976fe3d169df0624bfa6cf3e7fda9ac987d51967648840492ddc2dafdaa34e07
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 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.
[[Page 40010]]
Figure 5 to paragraph (i)--AFM Revision for Non-Radio Altimeter
Tolerant Airplanes
[GRAPHIC] [TIFF OMITTED] TR21JN23.076
Exact source excerpt. Text positions 15641–16558, end exclusive, in the original decoded publication. SHA-256: 91b24551fd9123be458074a4ae23fe67f575b5b27d97837b0ba1819f232d7f5d
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 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
[GRAPHIC] [TIFF OMITTED] TR21JN23.077
Exact source excerpt. Text positions 16558–17445, end exclusive, in the original decoded publication. SHA-256: a87832d0a3be5048864b1dc25c2d5f1e670a7e37f2517e46a71a96b40a8aa8ad
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 17445–18439, end exclusive, in the original decoded publication. SHA-256: 7f5129eacff58562b5dd9e0d3d6cb679c3ad606c725fb4a19c776e9f765d02f8
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 18439–18743, 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 18743–18794, end exclusive, in the original decoded publication. SHA-256: cffe37e8221668106206d572d73e6b4dfd97b02ec8d7400d43c985459042d6b5
Explicit historical replacement wording
Find all recorded historical references to AD 2023-12-14 · 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: 5bff044af0a0aca293aa49d8bf61b5dfe7e265ab7e57992bd8fb970173f52862. Source manifest: 9d88c21945617ecd5942707838be00343da785d51b00183c69cc60d13f64a4f5.
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 40003-40010]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2023-13149]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2023-0922; Project Identifier AD-2022-01431-T;
Amendment 39-22472; AD 2023-12-14]
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) 2022-06-
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
[[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.
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 2022-06-16, 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:
[[Page 40005]]
Estimated Costs
----------------------------------------------------------------------------------------------------------------
Cost per Cost on U.S.
Action Labor cost Parts cost product operators
----------------------------------------------------------------------------------------------------------------
AFM revision (retained actions from AD 1 work-hour x $85 per $0 $85 $11,645
2022-02-16). hour \1\ = $85.
New AFM revisions (new action)........ 1 work-hour x $85 per 0 85 \2\ 11,645
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 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.
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) 2022-06-16, Amendment 39-21982
(87 FR 14780, March 16, 2022), and
0
b. Adding the following new AD:
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.
BILLING CODE 4910-13-P
[[Page 40006]]
Figure 1 to paragraph (g)(2)(i)--Fundamental Effective Isotropic PSD
at Outside Interface of Aircraft Antenna
[GRAPHIC] [TIFF OMITTED] TR21JN23.072
(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 40007]]
Figure 2 to paragraph (g)(2)(ii)--Spurious Effective Isotropic PSD
at Outside Interface of Aircraft Antenna
[GRAPHIC] [TIFF OMITTED] TR21JN23.073
(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.
[[Page 40008]]
Figure 3 to paragraph (h)(1)--AFM Limitations Revision
[GRAPHIC] [TIFF OMITTED] TR21JN23.074
(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.
[[Page 40009]]
Figure 4 to paragraph (h)(2)--AFM Operating Procedures Revision
[GRAPHIC] [TIFF OMITTED] TR21JN23.075
(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.
[[Page 40010]]
Figure 5 to paragraph (i)--AFM Revision for Non-Radio Altimeter
Tolerant Airplanes
[GRAPHIC] [TIFF OMITTED] TR21JN23.076
(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
[GRAPHIC] [TIFF OMITTED] TR21JN23.077
(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. 2023-13149 Filed 6-16-23; 11:15 am]
BILLING CODE 4910-13-C
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