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Published 2021-12-15 · Federal Register document 2021-27090

Airworthiness Directives; The Boeing Company Airplanes

Publication summary

The FAA is superseding Airworthiness Directive (AD) 2019-01- 08, which applied to certain The Boeing Company Model 777-200, -200LR, -300, and -300ER series airplanes. AD 2019-01-08 required modifications for galley mounted attendant seat fittings. This AD was prompted by a report that showed a non-compliance exists on some in-service galley attendant seat fitting installations, and a determination that additional airplanes are subject to the unsafe condition. This AD requires modifications for galley mounted attendant seat fittings. 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 2026-09-03T22:24:08.106391+00:00. The title, summary and date are source facts.

Source revision
federal_register_ad_metadata_2021-9c919420683447c6
Source row
results[463]
Raw source SHA-256
9c919420683447c683ad0c877cb886e341c11862be32b47c536a001b1d76dcb5

Final-rule publication

Recorded publication clauses

AD identifier printed in this edition
2021-19-15
Effective date printed in this edition
2022-01-19
Read 13 complete recorded clauses
Effective Date
(a) Effective Date

    This airworthiness directive (AD) is effective January 19, 2022.

Exact source excerpt. Text positions 8258–8348, end exclusive, in the original decoded publication. SHA-256: c6f4af9257c92c97dc8f6620e3fb9758d790e1f102a0d3ec0f70c28c00411a4e

Affected ADs
(b) Affected ADs

    This AD replaces AD 2019-01-08, Amendment 39-19547 (84 FR 4318, 
February 15, 2019) (AD 2019-01-08).

Exact source excerpt. Text positions 8348–8472, end exclusive, in the original decoded publication. SHA-256: 673eb53b29779b14220a3c364a57c6ed4e0771cdc0d787ba3fa74008eaf96bb0

Applicability wording · Applicability
(c) Applicability

    This AD applies to The Boeing Company Model 777-200, -200LR, -
300, and -300ER series airplanes, certificated in any category, as 
identified in Boeing Special Attention Service Bulletin 777-25-0649, 
Revision 2, dated October 8, 2020.

Exact source excerpt. Text positions 8472–8732, end exclusive, in the original decoded publication. SHA-256: 2f50d7098e8bd94ede1b9b3c32465106749e0485c03065d023bc8b864ed2c79d

Subject
(d) Subject

    Air Transport Association (ATA) of America Code 25, Equipment/
furnishings.

Exact source excerpt. Text positions 8732–8826, end exclusive, in the original decoded publication. SHA-256: cd842d64513c20d1d1bce522de9bad2824ec75abe7ad967bbaaaf7decc400437

Unsafe Condition
(e) Unsafe Condition

    This AD was prompted by a report that showed a non-compliance 
exists on some in-service galley attendant seat fitting 
installations, and a determination that additional airplanes are 
subject to the unsafe condition. The FAA is issuing this AD to 
address non-compliant flight attendant seats, which could fail in a 
high-G crash and result in potential injury to flight attendants and 
consequent inability of the flight attendants to assist with 
passenger evacuation in a timely manner.

Exact source excerpt. Text positions 8826–9345, end exclusive, in the original decoded publication. SHA-256: 635114dfcf7eeada079027d741aaab1efa81ded0eb9f5d9a26a06bceeddddb4a

Compliance
(f) Compliance

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

Exact source excerpt. Text positions 9345–9447, end exclusive, in the original decoded publication. SHA-256: 00fbfa31932483f627d0ce0a11cbd2e35e15d9231842b91ac85623ce533912d3

Required Actions
(g) Required Actions

    Except as specified by paragraph (h) of this AD: At the 
applicable times specified in paragraph 1.E., ``Compliance,'' of 
Boeing Special Attention Service Bulletin 777-25-0649, Revision 2, 
dated October 8, 2020, do all applicable actions identified as 
``RC'' (required for compliance) in, and in accordance with, the 
Accomplishment Instructions of Boeing Special Attention Service 
Bulletin 777-25-0649, Revision 2, dated October 8, 2020.

Exact source excerpt. Text positions 9447–9917, end exclusive, in the original decoded publication. SHA-256: 032d5bbef4a73da0c6e3390b5cd1a26332c5d0e83c5d7cb8dcd7097c84e05cfc

Exception to Service Information Specifications
(h) Exception to Service Information Specifications

    Where Boeing Special Attention Service Bulletin 777-25-0649, 
Revision 2, dated October 8, 2020, uses the phrase ``the Revision 2 
date of this service bulletin,'' this AD requires using ``the 
effective date of this AD.''

Exact source excerpt. Text positions 9917–10198, end exclusive, in the original decoded publication. SHA-256: 9cb9a69be7273971de6ae25a96f87a2d8dcc64c4f553c33e0c8acc3c4156ca57

No Reporting Requirement
(i) No Reporting Requirement

    Although the service information referenced in Boeing Special 
Attention Service Bulletin 777-25-0649, Revision 2, dated October 8, 
2020, specifies to submit certain information to the manufacturer, 
this AD does not include that requirement.

Exact source excerpt. Text positions 10198–10477, end exclusive, in the original decoded publication. SHA-256: f8691c287adf2e71ac27db5a111806a4e4d1410f8f5057f745b8ed2279e0a1d0

Credit for Previous Actions
(j) 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 Special Attention Service 
Bulletin 777-25-0649, Revision 1, dated October 6, 2017 (which is 
incorporated by reference in AD 2019-01-08).

Exact source excerpt. Text positions 10477–10824, end exclusive, in the original decoded publication. SHA-256: 47e7a7e83f2293cde6a163628bbcf4cfe066208ea7e1fa1b2eb40a14d0c3af2f

Alternative Methods of Compliance (AMOCs)
(k) 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 Related Information. 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, Seattle 
ACO 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 2019-01-08 are approved as AMOCs for 
the corresponding provisions of Boeing Special Attention Service 
Bulletin 777-25-0649, Revision 2, dated October 8, 2020, that are 
required by paragraph (g) of this AD.
    (5) For service information that contains steps that are labeled 
as Required for Compliance (RC), the provisions of paragraphs 
(k)(5)(i) and (ii) of this AD apply.
    (i) The steps labeled as RC, including substeps under an RC step 
and any figures identified in an RC step, must be done to comply 
with the AD. If a step or substep is labeled ``RC Exempt,'' then the 
RC requirement is removed from that step or substep. An AMOC is 
required for any deviations to RC steps, including substeps and 
identified figures.
    (ii) Steps not labeled as RC may be deviated from using accepted 
methods in accordance with the operator's maintenance or inspection 
program without obtaining approval of an AMOC, provided the RC 
steps, including substeps and identified figures, can still be done 
as specified, and the airplane can be put back in an airworthy 
condition.

Exact source excerpt. Text positions 10824–13158, end exclusive, in the original decoded publication. SHA-256: 1ac6ea810f5fc02b9bd467ef9d69e91d2ec8af2e0103d4e350f1a847b409bd3f

Related Information
(l) Related Information

    (1) For more information about this AD, contact Brandon Lucero, 
Aerospace Engineer, Cabin Safety and Environmental Systems Section, 
FAA, Seattle ACO Branch, 2200 South 216th St., Des Moines, WA 98198; 
phone and fax: 206-231-3569; email: [email protected].
    (2) Service information identified in this AD that is not 
incorporated by reference is available at the addresses specified in 
paragraphs (m)(3) and (4) of this AD.

Exact source excerpt. Text positions 13158–13618, end exclusive, in the original decoded publication. SHA-256: 29d0400be788bee4619d7b809b296a783bf2cd44a902311e04b4ed0f6395e150

Material Incorporated by Reference
(m) 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 Special Attention Service Bulletin 777-25-0649, 
Revision 2, dated October 8, 2020.
    (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; internet https://www.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: https://www.archives.gov/federal-register/cfr/ibr-locations.html.

Exact source excerpt. Text positions 13618–14917, end exclusive, in the original decoded publication. SHA-256: 0b6e3c7acd61debe035533d75e96ab409e74c4cbab9e16a691feed455709af9c

Explicit historical replacement wording

Find all recorded historical references to AD 2021-19-15 · 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: 7781070a94ba5cc40f382a70449157c55d659be01458a8e6653d21882e279fd3. Source manifest: 5c38c0dd8d0b6f1e143826335a8c3838edad97a53c917859352c6e64fd110f3f.

Official source · 2021-12-15

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 86, Number 238 (Wednesday, December 15, 2021)]
[Rules and Regulations]
[Pages 71131-71133]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2021-27090]


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

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2021-0451; Project Identifier AD-2021-00007-T; 
Amendment 39-21733; AD 2021-19-15]
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) 2019-01-
08, which applied to certain The Boeing Company Model 777-200, -200LR, 
-300, and -300ER series airplanes. AD 2019-01-08 required modifications 
for galley mounted attendant seat fittings. This AD was prompted by a 
report that showed a non-compliance exists on some in-service galley 
attendant seat fitting installations, and a determination that 
additional airplanes are subject to the unsafe condition. This AD 
requires modifications for galley mounted attendant seat fittings. The 
FAA is

[[Page 71132]]

issuing this AD to address the unsafe condition on these products.

DATES: This AD is effective January 19, 2022.
    The Director of the Federal Register approved the incorporation by 
reference of a certain publication listed in this AD as of January 19, 
2022.

ADDRESSES: 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; internet https://www.myboeingfleet.com. 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 
https://www.regulations.gov by searching for and locating Docket No. 
FAA-2021-0451.

Examining the AD Docket

    You may examine the AD docket at https://www.regulations.gov by 
searching for and locating Docket No. FAA-2021-0451; 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: Brandon Lucero, Aerospace Engineer, 
Cabin Safety and Environmental Systems Section, FAA, Seattle ACO 
Branch, 2200 South 216th St., Des Moines, WA 98198; phone and fax: 206-
231-3569; email: [email protected].

SUPPLEMENTARY INFORMATION:

Background

    The FAA issued a notice of proposed rulemaking (NPRM) to amend 14 
CFR part 39 to supersede AD 2019-01-08, Amendment 39-19547 (84 FR 4318, 
February 15, 2019) (AD 2019-01-08). AD 2019-01-08 applied to certain 
The Boeing Company Model 777-200, -200LR, -300, and -300ER series 
airplanes. The NPRM published in the Federal Register on June 25, 2021 
(86 FR 33574). The NPRM was prompted by a report that showed a non-
compliance exists on some in-service galley attendant seat fitting 
installations, and a determination that additional airplanes are 
subject to the unsafe condition. In the NPRM, the FAA proposed to 
continue to require modifications for galley mounted attendant seat 
fittings and expand the applicability to include additional airplanes. 
The FAA is issuing this AD to address non-compliant flight attendant 
seats, which could fail in a high-G crash and result in potential 
injury to flight attendants and consequent inability of the flight 
attendants to assist with passenger evacuation in a timely manner.

Discussion of Final Airworthiness Directive

Comments

    The FAA received comments from Boeing and United Airlines, 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. 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 Special Attention Service Bulletin 777-25-
0649, Revision 2, dated October 8, 2020. This service information 
specifies procedures for modifying galley mounted attendant seat 
fittings. 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 the ADDRESSES section.

Costs of Compliance

    The FAA estimates that this AD affects 50 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
----------------------------------------------------------------------------------------------------------------
Modification..........................  7 work-hours x $85 per                $0            $595         $29,750
                                         hour = $595.
----------------------------------------------------------------------------------------------------------------

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:

[[Page 71133]]

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 2019-01-08, Amendment 39-19547 (84 
FR 4318, February 15, 2019), and
0
b. Adding the following new airworthiness directive:

2021-19-15 The Boeing Company: Amendment 39-21733; Docket No. FAA-
2021-0451; Project Identifier AD-2021-00007-T.

(a) Effective Date

    This airworthiness directive (AD) is effective January 19, 2022.

(b) Affected ADs

    This AD replaces AD 2019-01-08, Amendment 39-19547 (84 FR 4318, 
February 15, 2019) (AD 2019-01-08).

(c) Applicability

    This AD applies to The Boeing Company Model 777-200, -200LR, -
300, and -300ER series airplanes, certificated in any category, as 
identified in Boeing Special Attention Service Bulletin 777-25-0649, 
Revision 2, dated October 8, 2020.

(d) Subject

    Air Transport Association (ATA) of America Code 25, Equipment/
furnishings.

(e) Unsafe Condition

    This AD was prompted by a report that showed a non-compliance 
exists on some in-service galley attendant seat fitting 
installations, and a determination that additional airplanes are 
subject to the unsafe condition. The FAA is issuing this AD to 
address non-compliant flight attendant seats, which could fail in a 
high-G crash and result in potential injury to flight attendants and 
consequent inability of the flight attendants to assist with 
passenger evacuation in a timely manner.

(f) Compliance

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

(g) Required Actions

    Except as specified by paragraph (h) of this AD: At the 
applicable times specified in paragraph 1.E., ``Compliance,'' of 
Boeing Special Attention Service Bulletin 777-25-0649, Revision 2, 
dated October 8, 2020, do all applicable actions identified as 
``RC'' (required for compliance) in, and in accordance with, the 
Accomplishment Instructions of Boeing Special Attention Service 
Bulletin 777-25-0649, Revision 2, dated October 8, 2020.

(h) Exception to Service Information Specifications

    Where Boeing Special Attention Service Bulletin 777-25-0649, 
Revision 2, dated October 8, 2020, uses the phrase ``the Revision 2 
date of this service bulletin,'' this AD requires using ``the 
effective date of this AD.''

(i) No Reporting Requirement

    Although the service information referenced in Boeing Special 
Attention Service Bulletin 777-25-0649, Revision 2, dated October 8, 
2020, specifies to submit certain information to the manufacturer, 
this AD does not include that requirement.

(j) 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 Special Attention Service 
Bulletin 777-25-0649, Revision 1, dated October 6, 2017 (which is 
incorporated by reference in AD 2019-01-08).

(k) 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 Related Information. 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, Seattle 
ACO 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 2019-01-08 are approved as AMOCs for 
the corresponding provisions of Boeing Special Attention Service 
Bulletin 777-25-0649, Revision 2, dated October 8, 2020, that are 
required by paragraph (g) of this AD.
    (5) For service information that contains steps that are labeled 
as Required for Compliance (RC), the provisions of paragraphs 
(k)(5)(i) and (ii) of this AD apply.
    (i) The steps labeled as RC, including substeps under an RC step 
and any figures identified in an RC step, must be done to comply 
with the AD. If a step or substep is labeled ``RC Exempt,'' then the 
RC requirement is removed from that step or substep. An AMOC is 
required for any deviations to RC steps, including substeps and 
identified figures.
    (ii) Steps not labeled as RC may be deviated from using accepted 
methods in accordance with the operator's maintenance or inspection 
program without obtaining approval of an AMOC, provided the RC 
steps, including substeps and identified figures, can still be done 
as specified, and the airplane can be put back in an airworthy 
condition.

(l) Related Information

    (1) For more information about this AD, contact Brandon Lucero, 
Aerospace Engineer, Cabin Safety and Environmental Systems Section, 
FAA, Seattle ACO Branch, 2200 South 216th St., Des Moines, WA 98198; 
phone and fax: 206-231-3569; email: [email protected].
    (2) Service information identified in this AD that is not 
incorporated by reference is available at the addresses specified in 
paragraphs (m)(3) and (4) of this AD.

(m) 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 Special Attention Service Bulletin 777-25-0649, 
Revision 2, dated October 8, 2020.
    (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; internet https://www.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: https://www.archives.gov/federal-register/cfr/ibr-locations.html.

    Issued on September 8, 2021.
Lance T. Gant,
Director, Compliance & Airworthiness Division, Aircraft Certification 
Service.
[FR Doc. 2021-27090 Filed 12-14-21; 8:45 am]
BILLING CODE 4910-13-P


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Text SHA-256
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