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Published 2023-10-03 · Federal Register document 2023-21718

Airworthiness Directives; The Boeing Company Airplanes

Publication summary

The FAA is superseding Airworthiness Directive (AD) 2021-02- 15, which applied to certain The Boeing Company Model 747-100, 747- 100B, 747-100B SUD, 747-200B, 747-200C, 747-200F, 747-300, 747-400, 747-400D, 747-400F, and 747SR series airplanes. AD 2021-02-15 required repetitive replacement of certain parts; an inspection to determine production configuration for certain parts; repetitive lubrication of certain parts and a repetitive inspection of certain parts for any exuding grease; repetitive inspections of certain parts for loose or missing attachment bolts, cracks or bushing migration, cracks or gouges, or broken, binding, or missing rollers; repetitive inspections of certain parts for cracks or corrosion; repetitive lubrication; and on-condition actions if necessary. This AD was prompted by the FAA's determination that certain compliance times must be reduced in order to address the unsafe condition. This AD continues to require the actions specified in AD 2021-02-15 with certain reduced compliance times. 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[271]
Raw source SHA-256
81e907e5105d0f2c522e15b6fa8c7277117367b7f70b363862619549836b75e8

Final-rule publication

Recorded publication clauses

AD identifier printed in this edition
2023-18-06
Effective date printed in this edition
2023-11-07
Read 12 complete recorded clauses
Effective Date
(a) Effective Date

    This airworthiness directive (AD) is effective November 7, 2023.

Exact source excerpt. Text positions 11078–11168, end exclusive, in the original decoded publication. SHA-256: b6aa376e29e93040d6fd79983cf6600d24629384c226c2de847296642b090e02

Affected ADs
(b) Affected ADs

    This AD replaces AD 2021-02-15, Amendment 39-21398 (86 FR 10750, 
February 23, 2021) (AD 2021-02-15).

Exact source excerpt. Text positions 11168–11293, end exclusive, in the original decoded publication. SHA-256: c660296cfa9f941f44b06fd486c39189f52bae9909044291ecf0bac902fb4168

Applicability wording · Applicability
(c) Applicability

    This AD applies to The Boeing Company Model 747-100, 747-100B, 
747-100B SUD, 747-200B, 747-200C, 747-200F, 747-300, 747-400, 747-
400D, 747-400F, and 747SR series airplanes, certificated in any 
category, as identified in Boeing Alert Requirements Bulletin 747-
57A2367 RB, Revision 1, dated March 20, 2023.

Exact source excerpt. Text positions 11293–11626, end exclusive, in the original decoded publication. SHA-256: 07921bb0d129cae58e960374b98bfc549c154be2b6074fb29f78be7f153a4db6

Subject
(d) Subject

    Air Transport Association (ATA) of America Code 57, Wings.

Exact source excerpt. Text positions 11626–11703, end exclusive, in the original decoded publication. SHA-256: 52f35cb894eac2144f3b0de7a455ce53cfbcfebe8c2ccd3b1ccbff2308cfe7df

Unsafe Condition
(e) Unsafe Condition

    This AD was prompted by reports of partial and full inboard 
foreflap departures from the airplane. The FAA is issuing this AD to 
address departures of the inboard foreflap assembly from the 
airplane, which could result in damage to the airplane and adversely 
affect the airplane's continued safe flight and landing.

Exact source excerpt. Text positions 11703–12050, end exclusive, in the original decoded publication. SHA-256: a416aed989f511ab9d8d80f714a6bac2e9535e27ef2db51543277db60eb6add1

Compliance
(f) Compliance

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

Exact source excerpt. Text positions 12050–12152, end exclusive, in the original decoded publication. SHA-256: 00fbfa31932483f627d0ce0a11cbd2e35e15d9231842b91ac85623ce533912d3

Retained Actions, With Revised Compliance Times and Service Information
(g) Retained Actions, With Revised Compliance Times and Service 
Information

    This paragraph restates the requirements of paragraph (g) of AD 
2021-02-15, with revised compliance times and service information. 
Except as specified by paragraph (h) of this AD: At the applicable 
times specified in the ``Compliance''

[[Page 67937]]

paragraph of Boeing Alert Requirements Bulletin 747-57A2367 RB, 
Revision 1, dated March 20, 2023, do all applicable actions 
identified in, and in accordance with, the Accomplishment 
Instructions of Boeing Alert Requirements Bulletin 747-57A2367 RB, 
Revision 1, dated March 20, 2023.

    Note 1 to paragraph (g): Guidance for accomplishing the actions 
required by this AD can be found in Boeing Alert Service Bulletin 
747-57A2367, Revision 1, dated March 20, 2023, which is referred to 
in Boeing Alert Requirements Bulletin 747-57A2367 RB, Revision 1, 
dated March 20, 2023.

Exact source excerpt. Text positions 12152–13073, end exclusive, in the original decoded publication. SHA-256: 5f866bf9629a01100466d5a49c7d77983c2e4a8b9010d02cc6cc46130e89b59c

Exceptions to Service Information Specifications
(h) Exceptions to Service Information Specifications

    (1) Where the Compliance Time columns of the tables in the 
``Compliance'' paragraph of Boeing Alert Requirements Bulletin 747-
57A2367 RB, Revision 1, dated March 20, 2023, use the phrase ``the 
original issue date of Requirements Bulletin 747-57A2367 RB,'' this 
AD requires using March 30, 2021 (the effective date of AD 2021-02-
15).
    (2) Where the Compliance Time columns of the tables in the 
``Compliance'' paragraph of Boeing Alert Requirements Bulletin 747-
57A2367 RB, Revision 1, dated March 20, 2023, use the phrase ``the 
Revision 1 date of Requirements Bulletin 747-57A2367 RB,'' this AD 
requires using ``the effective date of this AD.''

Exact source excerpt. Text positions 13073–13788, end exclusive, in the original decoded publication. SHA-256: 2c58e94908aab21bdb78dffcc395af25edbf5df7e472a69df2f4af059ae6ddbb

Credit for Previous Actions
(i) Credit for Previous Actions

    This paragraph provides credit for the actions specified in 
paragraph (g) of this AD, if those actions were performed before the 
effective date of this AD using Boeing Alert Requirements Bulletin 
747-57A2367 RB, dated November 15, 2019.

Exact source excerpt. Text positions 13788–14066, end exclusive, in the original decoded publication. SHA-256: 749b2a2197200fd5db9e586d70278c9e7dea80a00a8f26a69e5ee4c2eec1a34d

Alternative Methods of Compliance (AMOCs)
(j) Alternative Methods of Compliance (AMOCs)

    (1) The Manager, AIR-520 Continued 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 AIR-520 Continued Operational 
Safety Branch, send it to the attention of the person identified in 
paragraph (k)(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) An AMOC that provides an acceptable level of safety may be 
used for any repair, modification, or alteration required by this AD 
if it is approved by The Boeing Company Organization Designation 
Authorization (ODA) that has been authorized by the Manager, AIR-520 
Continued Operational Safety Branch, FAA, to make those findings. To 
be approved, the repair method, modification deviation, or 
alteration deviation must meet the certification basis of the 
airplane, and the approval must specifically refer to this AD.
    (4) AMOCs approved for AD 2021-02-15 are approved as AMOCs for 
the corresponding provisions of Boeing Alert Requirements Bulletin 
747-57A2367 RB, Revision 1, dated March 20, 2023, that are required 
by paragraph (g) of this AD.

Exact source excerpt. Text positions 14066–15600, end exclusive, in the original decoded publication. SHA-256: b4d804ee2d17a901b33795df09b2884bfa0fcb581a2ac64b482475453ce65ab7

Related Information
(k) Related Information

    (1) For more information about this AD, contact Stefanie Roesli, 
Aviation Safety Engineer, FAA, 2200 South 216th St., Des Moines, WA 
98198; phone: 206-231-3964; email: [email protected].
    (2) Service information identified in this AD that is not 
incorporated by reference is available at the addresses specified in 
paragraphs (l)(3) and (4) of this AD.

Exact source excerpt. Text positions 15600–15990, end exclusive, in the original decoded publication. SHA-256: 069c9851a6ff3e12481bc148a973ff3c96f94bb9b7355901ffb272f5c1d581c3

Material Incorporated by Reference
(l) Material Incorporated by Reference

    (1) The Director of the Federal Register approved the 
incorporation by reference (IBR) of the service information listed 
in this paragraph under 5 U.S.C. 552(a) and 1 CFR part 51.
    (2) You must use this service information as applicable to do 
the actions required by this AD, unless the AD specifies otherwise.
    (i) Boeing Alert Requirements Bulletin 747-57A2367 RB, Revision 
1, dated March 20, 2023.
    (ii) [Reserved]
    (3) For service information identified in this AD, contact 
Boeing Commercial Airplanes, Attention: Contractual & Data Services 
(C&DS), 2600 Westminster Blvd., MC 110-SK57, Seal Beach, CA 90740-
5600; telephone 562-797-1717; website myboeingfleet.com.
    (4) You may view this service information at the FAA, 
Airworthiness Products Section, Operational Safety Branch, 2200 
South 216th St., Des Moines, WA. For information on the availability 
of this material at the FAA, call 206-231-3195.
    (5) You may view this service information that is incorporated 
by reference at the National Archives and Records Administration 
(NARA). For information on the availability of this material at 
NARA, email [email protected], or go to: www.archives.gov/federal-register/cfr/ibr-locations.html.

Exact source excerpt. Text positions 15990–17263, end exclusive, in the original decoded publication. SHA-256: 1a40b6ab4f0bec350238191a6b0c5cd08c9161f753959e3317b183593843005a

Explicit historical replacement wording

Find all recorded historical references to AD 2023-18-06 · 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: 3c3b537f41eb44d29c992aa4177349868ef4323a2bdbbc2584d19825f55e5aba. Source manifest: ba82165816afb33cfe6d92d0cc7d4e9137d7d73711932025267af8b0716ca9dc.

Official source · 2023-10-03

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 190 (Tuesday, October 3, 2023)]
[Rules and Regulations]
[Pages 67935-67937]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2023-21718]



[[Page 67935]]

=======================================================================
-----------------------------------------------------------------------

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2023-1222; Project Identifier AD-2023-00574-T; 
Amendment 39-22547; AD 2023-18-06]
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) 2021-02-
15, which applied to certain The Boeing Company Model 747-100, 747-
100B, 747-100B SUD, 747-200B, 747-200C, 747-200F, 747-300, 747-400, 
747-400D, 747-400F, and 747SR series airplanes. AD 2021-02-15 required 
repetitive replacement of certain parts; an inspection to determine 
production configuration for certain parts; repetitive lubrication of 
certain parts and a repetitive inspection of certain parts for any 
exuding grease; repetitive inspections of certain parts for loose or 
missing attachment bolts, cracks or bushing migration, cracks or 
gouges, or broken, binding, or missing rollers; repetitive inspections 
of certain parts for cracks or corrosion; repetitive lubrication; and 
on-condition actions if necessary. This AD was prompted by the FAA's 
determination that certain compliance times must be reduced in order to 
address the unsafe condition. This AD continues to require the actions 
specified in AD 2021-02-15 with certain reduced compliance times. The 
FAA is issuing this AD to address the unsafe condition on these 
products.

DATES: This AD is effective November 7, 2023.
    The Director of the Federal Register approved the incorporation by 
reference of a certain publication listed in this AD as of November 7, 
2023.

ADDRESSES: 
    AD Docket: You may examine the AD docket at regulations.gov under 
Docket No. FAA-2023-1222; 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.
    Material Incorporated by Reference:
    <bullet> For service information identified in this final rule, 
contact Boeing Commercial Airplanes, Attention: Contractual & Data 
Services (C&DS), 2600 Westminster Blvd., MC 110-SK57, Seal Beach, CA 
90740-5600; telephone 562-797-1717; website myboeingfleet.com.
    <bullet> You may view this service information at the FAA, 
Airworthiness Products Section, Operational Safety Branch, 2200 South 
216th St., Des Moines, WA. For information on the availability of this 
material at the FAA, call 206-231-3195. It is also available at 
regulations.gov under Docket No. FAA-2023-1222.

FOR FURTHER INFORMATION CONTACT: Stefanie Roesli, Aviation Safety 
Engineer, FAA, 2200 South 216th St., Des Moines, WA 98198; phone: 206-
231-3964; email: [email protected].

SUPPLEMENTARY INFORMATION: 

Background

    The FAA issued a notice of proposed rulemaking (NPRM) to amend 14 
CFR part 39 to supersede AD 2021-02-15, Amendment 39-21398 (86 FR 
10750, February 23, 2021) (AD 2021-02-15). AD 2021-02-15 applied to 
certain The Boeing Company Model 747-100, 747-100B, 747-100B SUD, 747-
200B, 747-200C, 747-200F, 747-300, 747-400, 747-400D, 747-400F, and 
747SR series airplanes. The NPRM published in the Federal Register on 
July 10, 2023 (88 FR 43479). The NPRM was prompted by the FAA's 
determination that certain compliance times must be reduced in order to 
address the unsafe condition. In the NPRM, the FAA proposed to continue 
to require the actions specified in AD 2021-02-15 with certain reduced 
compliance times. The FAA is issuing this AD to address departures of 
the inboard foreflap assembly from the airplane, which could result in 
damage to the airplane and adversely affect the airplane's continued 
safe flight and landing.

Discussion of Final Airworthiness Directive

Comments

    The FAA received comments from Air Line Pilots Association, 
International (ALPA) and Boeing, who supported the NPRM without change.

Conclusion

    The FAA reviewed the relevant data, considered any comments 
received, and determined that air safety requires adopting this AD as 
proposed. Accordingly, the FAA is issuing this AD to address the unsafe 
condition on these products. Except for minor editorial changes, this 
AD is adopted as proposed in the NPRM. None of the changes will 
increase the economic burden on any operator.

Related Service Information Under 1 CFR Part 51

    The FAA reviewed Boeing Alert Requirements Bulletin 747-57A2367 RB, 
Revision 1, dated March 20, 2023. This service information specifies 
procedures for repetitive replacement of certain parts; a general 
visual inspection to determine production configuration for certain 
parts; a repetitive lubrication of certain parts and a repetitive 
general visual inspection of certain parts for any exuding grease; 
repetitive detailed inspections of certain parts for loose or missing 
attachment bolts, cracks or bushing migration, cracks or gouges, or 
broken, binding, or missing rollers; repetitive detailed inspections of 
certain parts for cracks or corrosion; repetitive lubrication; and on-
condition actions if necessary. On-condition actions include 
replacements and repair.
    This service information is reasonably available because the 
interested parties have access to it through their normal course of 
business or by the means identified in ADDRESSES.

Costs of Compliance

    The FAA estimates that this AD affects 134 airplanes of U.S. 
registry. The FAA estimates the following costs to comply with this AD:

[[Page 67936]]



                                                 Estimated Costs
----------------------------------------------------------------------------------------------------------------
                                                                                                 Cost on U.S.
              Action                    Labor cost        Parts cost      Cost per product        operators
----------------------------------------------------------------------------------------------------------------
Repetitive replacement (retained   Up to 10 work-hours         $35,719  Up to $36,569 per    Up to $4,900,246
 actions from AD 2021-02-15).       x $85 per hour =                     replacement cycle.   per replacement
                                    Up to $850 per                                            cycle.
                                    replacement cycle.
General visual inspection for      1 work-hour x $85                 0  $85................  $11,390.
 parts production configuration     per hour = $85.
 (retained actions from AD 2021-
 02-15).
Repetitive detailed inspections    4 work-hours x $85                0  $340 per inspection  $45,560 per
 (retained actions from AD 2021-    per hour = $340                      cycle.               inspection cycle.
 02-15).                            per inspection
                                    cycle.
Repetitive inspection for          1 work-hour x $85                 0  $85 per lubrication  $11,390 per
 lubrication and repetitive         per hour = $85 per                                        lubrication.
 lubrication (retained actions      lubrication.
 from AD 2021-02-15).
----------------------------------------------------------------------------------------------------------------

    The FAA estimates the following costs to do any necessary on-
condition actions that would be required. The FAA has no way of 
determining the number of aircraft that might need these on-condition 
actions:

              Estimated Costs of On-Condition Replacements
------------------------------------------------------------------------
          Labor cost              Parts cost        Cost per product
------------------------------------------------------------------------
Up to 8 work-hour x $85 per    Up to $17,720..  Up to $18,400.
 hour = $680.
------------------------------------------------------------------------

    The FAA has received no definitive data that would enable the FAA 
to provide cost estimates for the on-condition repairs specified in 
this AD.

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) 2021-02-15, Amendment 39-21398 
(86 FR 10750, February 23, 2021); and
0
b. Adding the following new AD:

2023-18-06 The Boeing Company: Amendment 39-22547; Docket No. FAA-
2023-1222; Project Identifier AD-2023-00574-T.

(a) Effective Date

    This airworthiness directive (AD) is effective November 7, 2023.

(b) Affected ADs

    This AD replaces AD 2021-02-15, Amendment 39-21398 (86 FR 10750, 
February 23, 2021) (AD 2021-02-15).

(c) Applicability

    This AD applies to The Boeing Company Model 747-100, 747-100B, 
747-100B SUD, 747-200B, 747-200C, 747-200F, 747-300, 747-400, 747-
400D, 747-400F, and 747SR series airplanes, certificated in any 
category, as identified in Boeing Alert Requirements Bulletin 747-
57A2367 RB, Revision 1, dated March 20, 2023.

(d) Subject

    Air Transport Association (ATA) of America Code 57, Wings.

(e) Unsafe Condition

    This AD was prompted by reports of partial and full inboard 
foreflap departures from the airplane. The FAA is issuing this AD to 
address departures of the inboard foreflap assembly from the 
airplane, which could result in damage to the airplane and adversely 
affect the airplane's continued safe flight and landing.

(f) Compliance

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

(g) Retained Actions, With Revised Compliance Times and Service 
Information

    This paragraph restates the requirements of paragraph (g) of AD 
2021-02-15, with revised compliance times and service information. 
Except as specified by paragraph (h) of this AD: At the applicable 
times specified in the ``Compliance''

[[Page 67937]]

paragraph of Boeing Alert Requirements Bulletin 747-57A2367 RB, 
Revision 1, dated March 20, 2023, do all applicable actions 
identified in, and in accordance with, the Accomplishment 
Instructions of Boeing Alert Requirements Bulletin 747-57A2367 RB, 
Revision 1, dated March 20, 2023.

    Note 1 to paragraph (g): Guidance for accomplishing the actions 
required by this AD can be found in Boeing Alert Service Bulletin 
747-57A2367, Revision 1, dated March 20, 2023, which is referred to 
in Boeing Alert Requirements Bulletin 747-57A2367 RB, Revision 1, 
dated March 20, 2023.

(h) Exceptions to Service Information Specifications

    (1) Where the Compliance Time columns of the tables in the 
``Compliance'' paragraph of Boeing Alert Requirements Bulletin 747-
57A2367 RB, Revision 1, dated March 20, 2023, use the phrase ``the 
original issue date of Requirements Bulletin 747-57A2367 RB,'' this 
AD requires using March 30, 2021 (the effective date of AD 2021-02-
15).
    (2) Where the Compliance Time columns of the tables in the 
``Compliance'' paragraph of Boeing Alert Requirements Bulletin 747-
57A2367 RB, Revision 1, dated March 20, 2023, use the phrase ``the 
Revision 1 date of Requirements Bulletin 747-57A2367 RB,'' this AD 
requires using ``the effective date of this AD.''

(i) Credit for Previous Actions

    This paragraph provides credit for the actions specified in 
paragraph (g) of this AD, if those actions were performed before the 
effective date of this AD using Boeing Alert Requirements Bulletin 
747-57A2367 RB, dated November 15, 2019.

(j) Alternative Methods of Compliance (AMOCs)

    (1) The Manager, AIR-520 Continued 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 AIR-520 Continued Operational 
Safety Branch, send it to the attention of the person identified in 
paragraph (k)(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) An AMOC that provides an acceptable level of safety may be 
used for any repair, modification, or alteration required by this AD 
if it is approved by The Boeing Company Organization Designation 
Authorization (ODA) that has been authorized by the Manager, AIR-520 
Continued Operational Safety Branch, FAA, to make those findings. To 
be approved, the repair method, modification deviation, or 
alteration deviation must meet the certification basis of the 
airplane, and the approval must specifically refer to this AD.
    (4) AMOCs approved for AD 2021-02-15 are approved as AMOCs for 
the corresponding provisions of Boeing Alert Requirements Bulletin 
747-57A2367 RB, Revision 1, dated March 20, 2023, that are required 
by paragraph (g) of this AD.

(k) Related Information

    (1) For more information about this AD, contact Stefanie Roesli, 
Aviation Safety Engineer, FAA, 2200 South 216th St., Des Moines, WA 
98198; phone: 206-231-3964; email: [email protected].
    (2) Service information identified in this AD that is not 
incorporated by reference is available at the addresses specified in 
paragraphs (l)(3) and (4) of this AD.

(l) Material Incorporated by Reference

    (1) The Director of the Federal Register approved the 
incorporation by reference (IBR) of the service information listed 
in this paragraph under 5 U.S.C. 552(a) and 1 CFR part 51.
    (2) You must use this service information as applicable to do 
the actions required by this AD, unless the AD specifies otherwise.
    (i) Boeing Alert Requirements Bulletin 747-57A2367 RB, Revision 
1, dated March 20, 2023.
    (ii) [Reserved]
    (3) For service information identified in this AD, contact 
Boeing Commercial Airplanes, Attention: Contractual & Data Services 
(C&DS), 2600 Westminster Blvd., MC 110-SK57, Seal Beach, CA 90740-
5600; telephone 562-797-1717; website myboeingfleet.com.
    (4) You may view this service information at the FAA, 
Airworthiness Products Section, Operational Safety Branch, 2200 
South 216th St., Des Moines, WA. For information on the availability 
of this material at the FAA, call 206-231-3195.
    (5) You may view this service information that is incorporated 
by reference at the National Archives and Records Administration 
(NARA). For information on the availability of this material at 
NARA, email [email protected], or go to: www.archives.gov/federal-register/cfr/ibr-locations.html.

    Issued on September 7, 2023.
Caitlin Locke,
Director, Compliance & Airworthiness Division, Aircraft Certification 
Service.
[FR Doc. 2023-21718 Filed 10-2-23; 8:45 am]
BILLING CODE 4910-13-P


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