[Federal Register Volume 89, Number 22 (Thursday, February 1, 2024)]
[Rules and Regulations]
[Pages 6413-6416]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2024-01968]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2023-1041; Project Identifier AD-2022-01223-T;
Amendment 39-22657; AD 2024-01-06]
RIN 2120-AA64
Airworthiness Directives; The Boeing Company Airplanes
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Final rule.
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SUMMARY: The FAA is adopting a new airworthiness directive (AD) for
certain The Boeing Company Model 737-600, 737-700, and 737-800 series
airplanes. This AD was prompted by an evaluation by the design approval
holder (DAH) indicating the fuselage skin repairs at the double row of
fasteners centered on certain stringers have inadequate inspection
requirements for continuing airworthiness following repair
accomplishment. This AD is intended to complete certain programs to
support the airplane reaching its limit of validity (LOV). This AD
requires repetitive inspections for cracks of skin repairs at Stringer
S-17, and corrective actions if necessary. The FAA is issuing this AD
to address the unsafe condition on these products.
DATES: This AD is effective March 7, 2024.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in this AD as of March 7,
2024.
ADDRESSES:
AD Docket: You may examine the AD docket at regulations.gov under
Docket No. FAA-2023-1041; 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:
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.
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-2023-1041.
FOR FURTHER INFORMATION CONTACT: Bill Ashforth, Aviation Safety
Engineer, FAA, 2200 South 216th St., Des Moines, WA 98198; telephone
206-231-3520; email [email protected].
SUPPLEMENTARY INFORMATION:
Background
The FAA issued a notice of proposed rulemaking (NPRM) to amend 14
CFR part 39 by adding an AD that would apply to certain The Boeing
Company (Boeing) Model 737-600, 737-700, and 737-800 series airplanes.
The NPRM was published in the Federal Register on May 25, 2023 (88 FR
33849). The NPRM was prompted by an evaluation by the DAH indicating
the fuselage skin repairs at the double row of fasteners centered on
certain stringers have inadequate inspection requirements for
continuing airworthiness following repair accomplishment, which could
result in fatigue cracking of the repair going undetected.
In the NPRM, the FAA proposed to require repetitive inspections for
cracking of the skin repairs at S-17, and corrective actions if
necessary. The FAA is issuing this AD to address this fatigue cracking,
which, if not addressed, could grow to a critical length and result in
rapid decompression and loss of the airplane's structural integrity.
Discussion of Final Airworthiness Directive
Comments
The FAA received comments from the Air Line Pilots Association,
International (ALPA) who supported the NPRM without change.
The FAA also received comments from Aviation Partners Boeing (APB),
Boeing, Southwest Airlines (Southwest), and SunExpress Airline
(SunExpress).
Compliance With AMOC Procedures
APB determined that the incorporation of supplemental type
certificate (STC) ST00830SE for installation of split scimitar winglets
affects compliance with the mandated actions in the proposed rule, but
the extent of the impact to compliance is not fully known at this time.
APB noted that paragraph (h) of the proposed AD would replace the
provisions in Boeing Service Bulletin 737-53A1217 R1 that specify
contacting Boeing for an alternative method of compliance (AMOC) for
alternative inspections and corrective actions, and instead would
require using a method approved in accordance with paragraph (i) of the
proposed AD. APB stated that for affected airplanes with these
winglets, approval of any alternative inspections and corrective
actions for Zone 3 and Zone 4 repairs must be obtained from the
Manager, AIR-520 Continued Operational Safety Branch, FAA, through the
means described in paragraph (i)(1) of the proposed AD. APB asserted
that Boeing does not have delegation to approve repairs in areas
affected by the configuration of STC ST00830SE and cannot use ODA
approval as specified in paragraph (i)(3) of the proposed AD.
The FAA acknowledges APB's comment. Paragraph (h)(1) of this AD
states that AMOC approval be obtained using a method approved in
accordance with the procedures specified in ``paragraph (i)'' of this
AD, and does not limit approvals to the provisions of paragraph (i)(1)
or (3) of this AD. Therefore, no change to this AD is necessary.
[[Page 6414]]
Request To Correct Service Bulletin Reference
Boeing reported that the Background section of the NPRM incorrectly
identified the original service information as Boeing Service Bulletin
``737-53A1217,'' but that document was not an alert service bulletin
and should have been identified as Service Bulletin ``737-53-1217.''
The FAA agrees; no change to the final rule is necessary because
that reference is not used.
Request To Specify Service Bulletin Revision Level
The NPRM's Background section explained that certain existing post-
repair inspections are inadequate to address the unsafe condition, and
that the actions in paragraph (g) of the proposed AD would apply only
to airplanes on which a repair has been done as specified in ``Boeing
Alert Service Bulletin 737-53A1217.'' Boeing requested that the
statement be clarified by adding the revision level and date of the
service bulletin. Boeing further stated that Boeing Alert Service
Bulletin 737-53A1217, Revision 1, dated September 8, 2022, was issued
to add the post-repair inspections to airplanes on which a repair has
been done.
The FAA disagrees. In this context, the revision level and date of
the service bulletin were intentionally omitted so the Background
section of the NPRM would refer to any repair-including a repair done
using a method other than the service bulletin (at any revision level).
No change is necessary to this final rule.
Request To Revise Unsafe Condition
Boeing requested changes to paragraph (e) of the proposed AD, which
implied the unsafe condition is the potential for cracking. Boeing
stated that the proposed AD would require only post-repair inspections,
and asserted that the unsafe condition is actually the lack of post-
repair inspections because it could result in undetected post-repair
fatigue cracks.
The FAA agrees and has incorporated the relevant changes.
Request To Revise Compliance Time
Southwest and SunExpress stated that Boeing Alert Service Bulletin
737-53A1217 provides no grace period for airplanes that have exceeded
the threshold, and requested that the proposed AD be revised to provide
a grace period or optional threshold value.
The FAA notes that paragraph (g) of this AD mandates only Tables 3
through 6 of paragraph 1.E., ``Compliance,'' of Boeing Alert Service
Bulletin 737-53A1217, Revision 1, dated September 8, 2022. For those
actions, the service bulletin specifies a compliance time of 50,000
total flight cycles, with a grace period of 4,000 flight cycles after
the repair. Therefore, no change is necessary to the AD.
Request To Clarify Configuration Description
Southwest requested clarification of the affected airplanes and
corresponding requirements for Tables 1 through 3 of Boeing Alert
Service Bulletin 737-53A1217, Revision 1, dated September 8, 2022.
Southwest noted that paragraphs 1.A.1. and 1.D. define Groups 1 through
3, Configuration 3, as ``airplanes that have installed a repair,'' but
tables 1 through 3 of paragraph 1.E list conditions for airplanes that
both have and have not accomplished a repair.
The FAA provides the following clarification. The tables apply to
any airplanes that have performed a repair, whether the repair was done
in accordance with ``SB 737-53-1217 Original Issue'' or in accordance
with some other method. So the condition ``Airplanes that have not
accomplished a repair in accordance with `SB 737-53-1217 Original
Issue' applies to airplanes that have been repaired using some method
other than `SB 737-53-1217 Original Issue.' '' Groups 1 through 3,
Configuration 3, include any airplane on which a repair has been
accomplished in one of the zones specified in the service information.
No changes to this AD are necessary as a result of this comment.
Request To Use BMS 3-35 or BMS 3-23 Compound
Southwest noted that Boeing Alert Service Bulletin 737-53A1217,
Revision 1, dated September 8, 2022, specifies the use of BMS 3-23
corrosion-inhibiting compound (CIC) for repairs. Southwest requested
that the proposed AD be revised to allow the use of BMS 3-35 CIC due to
the faster drying time compared to BMS 3-23 CIC. Southwest stated that
Boeing Corrosion Prevention Manual (CPM) 20-60-00 and Boeing Service
Request (SR) SWA-SWA-10-1232-02B approve BMS 3-35 for use on all Boeing
commercial airplanes including those no longer in production.
The FAA agrees that either BMS 3-35 or BMS 3-23 CIC is acceptable
because both provide an adequate level of safety. Paragraph (h)(2) of
this AD has been added to allow use of either CIC.
Conclusion
The FAA reviewed the relevant data, considered the received
comments, and determined that air safety requires adopting this AD as
proposed, with limited changes as previously stated. Accordingly, the
FAA is issuing this AD to address the unsafe condition on these
products. Except for minor editorial changes, and any other changes
described previously, 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 Service Bulletin 737-53A1217,
Revision 1, dated September 8, 2022. This service information specifies
procedures for, among other actions, repetitive internal and external
detailed inspections, low frequency eddy current (LFEC) inspections,
and medium frequency eddy current (MFEC) inspections for cracks of the
skin repair of S-17, station (STA) 360 to STA 380, and STA 888 to STA
907, left and right sides of the airplane. Corrective actions include
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 106 airplanes of U.S.
registry. The FAA estimates the following costs to comply with this AD:
Estimated Costs
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Parts
Action Labor cost cost Cost per product Cost on U.S. operators
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External Post Repair 56 work-hours x $0 $4,760 per inspection $504,560 per inspection
Inspection. $85 per hour = cycle. cycle.
$4,760 per
inspection
cycle.
[[Page 6415]]
Internal Post Repair 52 work-hours x 0 $4,420 per inspection $468,520 per inspection
Inspections. $85 per hour = cycle. cycle.
$4,420 per
inspection
cycle.
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The FAA has received no definitive data on which to base the cost
estimates for the 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 adding the following new airworthiness
directive:
2024-01-06 The Boeing Company: Amendment 39-22657; Docket No. FAA-
2023-1041; Project Identifier AD-2022-01223-T.
(a) Effective Date
This airworthiness directive (AD) is effective March 7, 2024.
(b) Affected ADs
None.
(c) Applicability
This AD applies to The Boeing Company Model 737-600, 737-700,
and 737-800 series airplanes, certificated in any category, as
identified in Boeing Alert Service Bulletin 737-53A1217, Revision 1,
dated September 8, 2022.
(d) Subject
Air Transport Association (ATA) of America Code 53, Fuselage.
(e) Unsafe Condition
This AD was prompted by an evaluation by the design approval
holder (DAH) indicating the fuselage skin repairs at the double row
of fasteners centered on certain stringers have inadequate
inspection requirements for continuing airworthiness following
repair accomplishment, which could result in fatigue cracking of the
repair going undetected. The FAA is issuing this AD to address the
inadequacy of post-repair inspection requirements at certain repair
fastener locations centered on stringer S-17L and S-17R, at station
(STA) 360 to STA 380 and at STA 888 to STA 907. Such inspection
inadequacy could result in post-repair fatigue cracks going
undetected. Fatigue cracking, if not addressed, could grow to a
critical length, which could result in rapid decompression and 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 in paragraph (h) of this AD: For Group 1
through 3, Configuration 3 airplanes as identified in Boeing Alert
Service Bulletin 737-53A1217, Revision 1, dated September 8, 2022,
at the applicable times specified in Tables 3 through 6 of paragraph
1.E., ``Compliance,'' of Boeing Alert Service Bulletin 737-53A1217,
Revision 1, dated September 8, 2022, do all applicable actions
identified as ``RC'' (required for compliance) in, and in accordance
with, the Accomplishment Instructions of Boeing Alert Service
Bulletin 737-53A1217, Revision 1, dated September 8, 2022.
(h) Exceptions to Service Information Specifications
(1) Where Boeing Alert Service Bulletin 737-53A1217, Revision 1,
dated September 8, 2022, specifies contacting Boeing for repair
instructions or for alternative inspections: This AD requires doing
the repair, or doing the alternative inspections and applicable on-
condition actions, using a method approved in accordance with the
procedures specified in paragraph (i) of this AD.
(2) Where Boeing Alert Service Bulletin 737-53A1217, Revision 1,
dated September 8, 2022, specifies using corrosion inhibiting
compound (CIC) compound BMS 3-23, this AD also allows use of CIC
compound BMS 3-35.
(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, AIR-520 Continued Operational
Safety Branch, FAA, send it to the attention of the person
identified in paragraph (j) 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) Except as specified by paragraph (h) of this AD: For service
information that
[[Page 6416]]
contains steps that are labeled as Required for Compliance (RC), the
provisions of paragraphs (i)(4)(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.
(j) Related Information
For more information about this AD, contact Bill Ashforth,
Aviation Safety Engineer, FAA, 2200 South 216th St., Des Moines, WA
98198; telephone 206-231-3520; email [email protected].
(k) 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 Service Bulletin 737-53A1217, Revision 1, dated
September 8, 2022.
(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 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 January 6, 2024.
Caitlin Locke,
Director, Compliance & Airworthiness Division, Aircraft Certification
Service.
[FR Doc. 2024-01968 Filed 1-31-24; 8:45 am]
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