Proposed Rule2024-14521
Airworthiness Directives; The Boeing Company Airplanes
Primary source
Metadata and text below are from the Federal Register, a public-domain U.S. government work. Always verify the official published version before relying on it for any legal matter.
Published
July 2, 2024
Issuing agencies
Transportation DepartmentFederal Aviation Administration
Abstract
The FAA proposes to adopt a new airworthiness directive (AD) for all The Boeing Company Model 737-600, -700, -700C, -800, -900, and -900ER series airplanes. This proposed AD was prompted by a report of a frame web crack at fuselage station (STA) 328 between stringers S-20R and S-21R common to the frame web notch. This proposed AD would require repetitive detailed inspections of the forward and aft sides of the frames and high frequency eddy current (HFEC) inspections of the frames for cracks and repairing any crack found. The FAA is proposing this AD to address the unsafe condition on these products.
Full Text
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<title>Federal Register, Volume 89 Issue 127 (Tuesday, July 2, 2024)</title>
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[Federal Register Volume 89, Number 127 (Tuesday, July 2, 2024)]
[Proposed Rules]
[Pages 54737-54739]
From the Federal Register Online via the Government Publishing Office [<a href="http://www.gpo.gov">www.gpo.gov</a>]
[FR Doc No: 2024-14521]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2024-1880; Project Identifier AD-2023-01149-T]
RIN 2120-AA64
Airworthiness Directives; The Boeing Company Airplanes
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Notice of proposed rulemaking (NPRM).
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SUMMARY: The FAA proposes to adopt a new airworthiness directive (AD)
for all The Boeing Company Model 737-600, -700, -700C, -800, -900, and
-900ER series airplanes. This proposed AD was prompted by a report of a
frame web crack at fuselage station (STA) 328 between stringers S-20R
and S-21R common to the frame web notch. This proposed AD would require
repetitive detailed inspections of the forward and aft sides of the
frames and high frequency eddy current (HFEC) inspections of the frames
for cracks and repairing any crack found. 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 16,
2024.
ADDRESSES: You may send comments, using the procedures found in 14 CFR
11.43 and 11.45, by any of the following methods:
<bullet> Federal eRulemaking Portal: Go to <a href="http://regulations.gov">regulations.gov</a>. Follow
the instructions for submitting comments.
<bullet> Fax: 202-493-2251.
<bullet> Mail: U.S. Department of Transportation, Docket
Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New
Jersey Avenue SE, Washington, DC 20590.
<bullet> Hand Delivery: Deliver to Mail address above between 9
a.m. and 5 p.m., Monday through Friday, except Federal holidays.
AD Docket: You may examine the AD docket at <a href="http://regulations.gov">regulations.gov</a> under
Docket No. FAA-2024-1880; 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:
<bullet> For service information, 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 <a href="http://myboeingfleet.com">myboeingfleet.com</a>.
<bullet> You may view this service information at the FAA,
Airworthiness Products Section, Operational Safety Branch, 2200 South
216th Street, Des Moines, WA. For information on the availability of
this material at the FAA, call 206-231-3195. It is also available at
<a href="http://regulations.gov">regulations.gov</a> under Docket No. FAA-2024-1880.
FOR FURTHER INFORMATION CONTACT: Bill Ashforth, Aviation Safety
Engineer, FAA, 2200 South 216th Street, Des Moines, WA 98198; phone:
206-231-3520; email: <a href="/cdn-cgi/l/email-protection#afcdc6c3c381cedcc7c9c0dddbc7efc9cece81c8c0d9"><span class="__cf_email__" data-cfemail="c4a6ada8a8eaa5b7aca2abb6b0ac84a2a5a5eaa3abb2">[email protected]</span></a>.
SUPPLEMENTARY INFORMATION:
Comments Invited
The FAA invites you to send any written relevant data, views, or
[[Page 54738]]
arguments about this proposal. Send your comments to an address listed
under ADDRESSES. Include ``Docket No. FAA-2024-1880; Project Identifier
AD-2023-01149-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
<a href="http://regulations.gov">regulations.gov</a>, 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 Bill
Ashforth, Aviation Safety Engineer, FAA, 2200 South 216th Street, Des
Moines, WA 98198; phone: 206-231-3520; email: <a href="/cdn-cgi/l/email-protection#197b70757537786a717f766b6d71597f7878377e766f"><span class="__cf_email__" data-cfemail="6b09020707450a18030d04191f032b0d0a0a450c041d">[email protected]</span></a>.
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 that an operator of a Model 737-700
airplane found a frame web crack at fuselage STA 328 between stringers
S-20R and S-21R while performing a visual inspection of the electrical
and electronics compartment during scheduled maintenance. The crack was
common to the frame web notch and was approximately 0.85 inch long. The
crack originated at a notch radius of the lower frame web that is
subject to a load transfer from the inner chord of the upper frame.
Because the load transfer is similar in adjacent areas, the frames at
STA 312, STA 328, and STA 344 from stringers S-20R to S-23R are also
affected. Model 737-600, -700C, -800, -900, and -900ER series airplanes
have similar structure in the affected area and are also subject to
this unsafe condition. Undetected cracks in the frame could lead to the
inability of the principal structural element to sustain limit loads,
which could result in the subsequent loss of structural integrity of
the airplane.
FAA's Determination
The FAA is issuing this NPRM after determining that the unsafe
condition described previously is likely to exist or develop on other
products of the same type design.
Related Service Information Under 1 CFR Part 51
The FAA reviewed Boeing Alert Requirements Bulletin 737-53A1410 RB,
dated October 11, 2023. This service information specifies procedures
for repetitive detailed inspections of the forward and aft sides of the
frames, and surface and open hole HFEC inspections of the frames, at
STA 312 from S-20R to S-23R, STA 328 from S-19R to S-22R, and STA 344
from S-20R to S-23R for cracks. This service information also specifies
repairing any crack found.
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.
Proposed AD Requirements in This NPRM
This proposed AD would require accomplishing the actions specified
in the service information already described, except for any
differences identified as exceptions in the regulatory text of this
proposed AD. For information on the procedures and compliance times,
see this service information at <a href="http://regulations.gov">regulations.gov</a> under Docket No. FAA-
2024-1880.
Costs of Compliance
The FAA estimates that this AD, if adopted as proposed, would
affect 1,583 airplanes of U.S. registry. The FAA estimates the
following costs to comply with this proposed AD:
Estimated Costs
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Cost on U.S.
Action Labor cost Parts cost Cost per product operators
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Inspections...................... 9 work-hours x $85 $0 $765 per inspection $1,210,995 per
per hour = $765 per cycle. inspection cycle.
inspection cycle.
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Estimated Costs of On-Condition Actions
The extent of damage/cracking found during the proposed inspections
could vary significantly from airplane to airplane. The FAA has no way
of determining the type of repair or cost to repair any cracks on each
airplane or the number of airplanes that may require repair.
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.
[[Page 54739]]
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:
The Boeing Company: Docket No. FAA-2024-1880; Project Identifier AD-
2023-01149-T.
(a) Comments Due Date
The FAA must receive comments on this airworthiness directive
(AD) by August 16, 2024.
(b) Affected ADs
None.
(c) Applicability
This AD applies to all The Boeing Company (Boeing) Model 737-
600, -700, -700C, -800, -900, and -900ER series airplanes,
certificated in any category.
(d) Subject
Air Transport Association (ATA) of America Code 53, Fuselage.
(e) Unsafe Condition
This AD was prompted by a report of a frame web crack at
fuselage station 328 between stringers S-20R and S-21R common to the
frame web notch. The FAA is issuing this AD to address undetected
cracks in the frame. The unsafe condition, if not addressed, could
lead to the inability of the principal structural element to sustain
limit loads, which could result in the subsequent loss of structural
integrity of the airplane.
(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 the ``Compliance'' paragraph of Boeing
Alert Requirements Bulletin 737-53A1410 RB, dated October 11, 2023,
do all applicable actions identified in, and in accordance with, the
Accomplishment Instructions of Boeing Alert Requirements Bulletin
737-53A1410 RB, dated October 11, 2023.
Note 1 to paragraph (g): Guidance for accomplishing the actions
required by this AD can be found in Boeing Alert Service Bulletin
737-53A1410, dated October 11, 2023, which is referred to in Boeing
Alert Requirements Bulletin 737-53A1410 RB, dated October 11, 2023.
(h) Exceptions to Service Information Specifications
(1) Where the ``Boeing Recommended Compliance Time'' column in
the table under the ``Compliance'' paragraph of Boeing Alert
Requirements Bulletin 737-53A1410 RB, dated October 11, 2023, refers
to ``the Original Issue date of Requirements Bulletin 737-53A1410
RB,'' this AD requires using the effective date of this AD.
(2) Where Boeing Alert Requirements Bulletin 737-53A1410 RB,
dated October 11, 2023, specifies contacting Boeing for repair
instructions, this AD requires doing the repair using a method
approved in accordance with the procedures in paragraph (i) of this
AD.
(i) 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 the certification office,
send it to the attention of the person identified in paragraph
(j)(1) of this AD. Information may be emailed to: <a href="/cdn-cgi/l/email-protection#7435393b37341215155a131b02"><span class="__cf_email__" data-cfemail="8bcac6c4c8cbedeaeaa5ece4fd">[email protected]</span></a>.
(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 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.
(j) Related Information
(1) For more information about this AD, contact Bill Ashforth,
Aviation Safety Engineer, FAA, 2200 South 216th Street, Des Moines,
WA 98198; phone: 206-231-3520; email: <a href="/cdn-cgi/l/email-protection#492b20252567283a212f263b3d21092f2828672e263f"><span class="__cf_email__" data-cfemail="5f3d363333713e2c3739302d2b371f393e3e71383029">[email protected]</span></a>.
(2) Service information identified in this AD that is not
incorporated by reference is available at the address specified in
paragraph (k)(3) this AD.
(k) Material Incorporated by Reference
(1) The Director of the Federal Register approved the
incorporation by reference 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 737-53A1410 RB, dated
October 11, 2023.
(ii) [Reserved]
(3) For service information, 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 <a href="http://myboeingfleet.com">myboeingfleet.com</a>.
(4) You may view this material at the FAA, Airworthiness
Products Section, Operational Safety Branch, 2200 South 216th
Street, 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 <a href="/cdn-cgi/l/email-protection#447825642c36212279" http: www.archives.gov federal-register cfr ibr-locationsoremailfr.inspection@nara.gov">www.archives.gov/federal-register/cfr/<span class="__cf_email__" data-cfemail="375e55451a5b585456435e5859445845525a565e5b5145195e5944475254435e5859775956455619505841">[email protected]</span></a>"><a href="http://www.archives.gov/federal-register/cfr/ibr-locationsoremailfr.inspection@nara.gov">www.archives.gov/federal-register/cfr/<span class="__cf_email__" data-cfemail="94fdf6e6b9f8fbf7f5e0fdfbfae7fbe6f1f9f5fdf8f2e6bafdfae7e4f1f7e0fdfbfad4faf5e6f5baf3fbe2">[email protected]</span></a></a>.
Issued on June 26, 2024.
Suzanne Masterson,
Deputy Director, Integrated Certificate Management Division, Aircraft
Certification Service.
[FR Doc. 2024-14521 Filed 7-1-24; 8:45 am]
BILLING CODE 4910-13-P
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