[Federal Register Volume 90, Number 131 (Friday, July 11, 2025)]
[Proposed Rules]
[Pages 30829-30831]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2025-13007]


========================================================================
Proposed Rules
                                                Federal Register
________________________________________________________________________

This section of the FEDERAL REGISTER contains notices to the public of 
the proposed issuance of rules and regulations. The purpose of these 
notices is to give interested persons an opportunity to participate in 
the rule making prior to the adoption of the final rules.

========================================================================


Federal Register / Vol. 90, No. 131 / Friday, July 11, 2025 / 
Proposed Rules

[[Page 30829]]



DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2025-1360; Project Identifier AD-2024-00710-Q,T]
RIN 2120-AA64


Airworthiness Directives; Goodrich Cabin Attendant Seats

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Notice of proposed rulemaking (NPRM).

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

SUMMARY: The FAA proposes to adopt a new airworthiness directive (AD) 
for Goodrich cabin attendant seats installed on Airbus SAS Model A330-
200 series, A330-200 Freighter series, A330-300 series, A330-841, A330-
941, A340-200 series, A340-300 series, A340-541, and A340-642 
airplanes. This proposed AD was prompted by a report that track 
attachments used on certain part-numbered seats are non-compliant. This 
proposed AD would require replacing all seat track attachments and 
hardware and re-identifying the seat with a new part number. The FAA is 
proposing this AD to address the unsafe condition on these products.

DATES: The FAA must receive comments on this proposed AD by August 25, 
2025.

ADDRESSES: You may send comments, using the procedures found in 14 CFR 
11.43 and 11.45, by any of the following methods:
     Federal eRulemaking Portal: Go to regulations.gov. Follow 
the instructions for submitting comments.
     Fax: 202-493-2251.
     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.
     Hand Delivery: Deliver to Mail address above between 9 
a.m. and 5 p.m., Monday through Friday, except Federal holidays.
    AD Docket: You may examine the AD docket at regulations.gov under 
Docket No. FAA-2025-1360; 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 NPRM, any comments received, and other 
information. The street address for Docket Operations is listed above.
    Material Incorporated by Reference:
     For Goodrich material identified in this proposed AD, 
contact Goodrich Aircraft Interior Products, 1275 North Newport Road, 
Colorado Springs, CO 80916-2779; phone: 719-380-0391; email: 
[email protected]; website: collinsaerospace.com.
     You may view this material 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.

FOR FURTHER INFORMATION CONTACT: Thanh-Phuong Ta, Aviation Safety 
Engineer, FAA, 3960 Paramount Boulevard, Lakewood, CA 90712; phone: 
303-342-1095; email: [email protected].

SUPPLEMENTARY INFORMATION:

Comments Invited

    The FAA invites you to send any written relevant data, views, or 
arguments about this proposal. Send your comments using a method listed 
under the ADDRESSES section. Include ``Docket No. FAA-2025-1360; 
Project Identifier AD-2024-00710-Q,T'' at the beginning of your 
comments. The most helpful comments reference a specific portion of the 
proposal, 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 proposal 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 
regulations.gov, including any personal information you provide. The 
agency will also post a report summarizing each substantive verbal 
contact received about this NPRM.

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 NPRM 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 NPRM, 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 NPRM. Submissions containing CBI should be sent to 
Thanh-Phuong Ta, Aviation Safety Engineer, FAA, 3960 Paramount 
Boulevard, Lakewood, CA 90712; phone: 303-342-1095; 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.

Background

    The FAA has received a report from Goodrich Corporation Interiors 
that track attachments used on certain part-numbered cabin attendant 
seats are not compliant with the requirement for the seats to withstand 
a dynamic load of 16 times the force of gravity (16g) in an accident 
per Technical Standard Order TSO-C127(a) and 14 CFR 25.562(b). These 
seats are installed on Airbus SAS Model A330-201, -202, -203, -223, -
243, -223F, -243F, -301, -302, -303, -321, -322, -323, -341, -342, -
343, -841, and -941 airplanes, and Model A340-211, -212, -213, -311, -
312, -313, -541, and -642 airplanes. Due to flawed analysis and 
incomplete testing that did not consider the dynamic strength and 
geometry of the cast track attachments, the cabin attendant seat may 
detach from the airplane. This condition, if not addressed, could 
result in injury to the occupant or a blocked exit during an emergency 
evacuation.

FAA's Determination

    The FAA is issuing this NPRM after determining that the unsafe 
condition described previously is likely to exist or

[[Page 30830]]

develop on other products of the same type design.

Material Incorporated by Reference Under 1 CFR Part 51

    The FAA reviewed the following material:
     Goodrich Service Bulletin 2057-25-071, Revision A, dated 
November 27, 2017;
     Goodrich Service Bulletin 2071-25-046, Revision C, dated 
January 14, 2020;
     Goodrich Service Bulletin 2157-25-092, Revision C, dated 
May 18, 2022; and
     Goodrich Service Bulletin 2201-25-013, Revision E, dated 
May 20, 2024.
    This material specifies procedures for replacing all seat track 
attachments and hardware and then re-identifying the seat with a new 
part number. These documents are distinct since they apply to different 
airplane configurations.
    This material 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.

Proposed AD Requirements in This NPRM

    This proposed AD would require accomplishing the actions specified 
in the material already described, except for any differences 
identified as exceptions in the regulatory text of this proposed AD. 
See ``Differences Between this Proposed AD and the Referenced 
Material'' for a discussion of these differences.

Difference Between This Proposed AD and the Referenced Material

    Although Goodrich Service Bulletins 2057-25-071, 2071-25-046, 2157-
25-092, and 2201-25-013 recommend replacing the seat track attachments 
within 4 years, this proposed AD would require replacing them within 2 
years. The FAA has determined that replacement within 4 years would not 
ensure an adequate level of safety for the affected fleet. In 
developing an appropriate compliance time for this AD, the FAA 
considered the manufacturer's recommendation, the degree of urgency 
associated with the subject unsafe condition, the average utilization 
of the affected fleet, and the time necessary to replace the seat track 
attachments. In light of these factors, the FAA finds a 2-year 
compliance time appropriate for affected airplanes to continue to 
operate without compromising safety.

Costs of Compliance

    The FAA estimates that this AD, if adopted as proposed, would 
affect 59 airplanes of U.S. registry. The FAA estimates the following 
costs to comply with this proposed AD:

                                                 Estimated Costs
----------------------------------------------------------------------------------------------------------------
                                                                                     Cost per      Cost on U.S.
                Action                         Labor cost           Parts cost        product        operators
----------------------------------------------------------------------------------------------------------------
Replacement and seat reidentification.  15 work-hours x $85 per           $1,500          $2,775        $163,725
                                         hour = $1,275.
----------------------------------------------------------------------------------------------------------------

    The FAA has included all known costs in its cost estimate. 
According to the manufacturer, however, some or all of the costs of 
this proposed AD may be covered under warranty, thereby reducing the 
cost impact on affected operators.

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

    The FAA determined that this proposed AD would not have federalism 
implications under Executive Order 13132. This proposed AD would 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 this proposed 
regulation:
    (1) Is not a ``significant regulatory action'' under Executive 
Order 12866,
    (2) Would not affect intrastate aviation in Alaska, and
    (3) Would 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 Proposed Amendment

    Accordingly, under the authority delegated to me by the 
Administrator, the FAA proposes to amend 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:

Goodrich: Docket No. FAA-2025-1360; Project Identifier AD-2024-
00710-Q,T.

(a) Comments Due Date

    The FAA must receive comments on this airworthiness directive 
(AD) by August 25, 2025.

(b) Affected ADs

    None.

(c) Applicability

    This AD applies to Goodrich cabin attendant seats, part numbers 
2057-11XXXXXX with floor seating option, except for 2057-1 hard 
point mounted seats; 2201-1XXYY and -2XXYY; 2157-7XXXXXXX and -
9XXXXXXX; and 2071-2XXXX and -A2XXXX. These seats are installed on 
the Airbus SAS airplanes, certificated in any category, listed in 
paragraphs (c)(1) and (2) of this AD.
    (1) Model A330-201, -202, -203, -223, -243, -223F, -243F, -301, 
-302, -303, -321, -322, -323, -341, -342, -343, -841, and -941 
airplanes.

[[Page 30831]]

    (2) Model A340-211, -212, -213, -311, -312, -313, -541, and -642 
airplanes.

(d) Subject

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

(e) Unsafe Condition

    This AD was prompted by a report that track attachments used on 
certain cabin attendant seats are non-compliant. The FAA is issuing 
this AD to prevent the cabin attendant seat from detaching from the 
airplane. The unsafe condition, if not addressed, could result in 
injury to the occupant or a blocked exit during an emergency 
evacuation.

(f) Compliance

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

(g) Seat Track Attachment Replacement

    Within 2 years after the effective date of this AD, replace the 
seat track attachments and hardware and re-identify the seat with a 
new part number in accordance with the applicable service 
information identified in paragraphs (g)(1) through (4) of this AD, 
except you are not required to discard parts. Instead, remove those 
parts from service.
    (1) Goodrich Service Bulletin 2057-25-071, Revision A, dated 
November 27, 2017.
    (2) Goodrich Service Bulletin 2071-25-046, Revision C, dated 
January 14, 2020.
    (3) Goodrich Service Bulletin 2157-25-092, Revision C, dated May 
18, 2022.
    (4) Goodrich Service Bulletin 2201-25-013, Revision E, dated May 
20, 2024.

(h) Credit for Previous Actions

    This paragraph provides credit for the actions required by 
paragraph (g) of this AD, if those actions were performed before the 
effective date of this AD using Goodrich Service Bulletin 2071-25-
046, Revision B, dated December 10, 2019, or Goodrich Service 
Bulletin 2157-25-092, Revision B, dated January 12, 2021.

(i) Alternative Methods of Compliance (AMOCs)

    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 the Continued Operational Safety Branch, 
send it to the attention of the person identified in paragraph 
(j)(1) of this AD. Information may be emailed to: [email protected]. 
Before using any approved AMOC, notify your appropriate principal 
inspector, or lacking a principal inspector, the manager of the 
responsible Flight Standards Office.

(j) Related Information

    (1) For more information about this AD, contact Thanh-Phuong Ta, 
Aviation Safety Engineer, FAA, 3960 Paramount Boulevard, Lakewood, 
CA 90712; phone: 303-342-1095; email: [email protected].
    (2) Material identified in this AD that is not incorporated by 
reference is available at the address specified in paragraph (k)(3) 
of this AD.

(k) Material Incorporated by Reference

    (1) The Director of the Federal Register approved the 
incorporation by reference of the material listed in this paragraph 
under 5 U.S.C. 552(a) and 1 CFR part 51.
    (2) You must use this material as applicable to do the actions 
required by this AD, unless the AD specifies otherwise.
    (i) Goodrich Service Bulletin 2057-25-071, Revision A, dated 
November 27, 2017.
    (ii) Goodrich Service Bulletin 2071-25-046, Revision C, dated 
January 14, 2020.
    (iii) Goodrich Service Bulletin 2157-25-092, Revision C, dated 
May 18, 2022.
    (iv) Goodrich Service Bulletin 2201-25-013, Revision E, dated 
May 20, 2024.
    (3) For Goodrich material identified in this AD, contact 
Goodrich Aircraft Interior Products, 1275 North Newport Road, 
Colorado Springs, CO 80916-2779; phone: 719-380-0391; email: 
[email protected]; website: collinsaerospace.com.
    (4) You may view this material 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 material at the National Archives and 
Records Administration (NARA). For information on the availability 
of this material at NARA, visit www.archives.gov/federal-register/cfr/ibr-locations or email [email protected].

    Issued on July 9, 2025.
Lona C. Saccomando,
Acting Deputy Director, Integrated Certificate Management Division, 
Aircraft Certification Service.

[FR Doc. 2025-13007 Filed 7-10-25; 8:45 am]
BILLING CODE 4910-13-P