Airworthiness Directives; The Boeing Company Airplanes, 86069-86072 [2023-27100]

Download as PDF Federal Register / Vol. 88, No. 237 / Tuesday, December 12, 2023 / Proposed Rules AMS has not identified any relevant Federal rules that duplicate, overlap, or conflict with this proposed rule. A small business guide on complying with fruit, vegetable, and specialty crop marketing agreements and orders may be viewed at: https:// www.ams.usda.gov/rules-regulations/ moa/small-businesses. Any questions about the compliance guide should be sent to Richard Lower at the previously mentioned address in the FOR FURTHER INFORMATION CONTACT section. After consideration of all relevant material presented, including the information and recommendations submitted by the Committee and other available information, USDA has determined that this proposed rule is consistent with and will effectuate the purposes of the Act. A 30-day comment period is provided to allow interested persons to respond to this proposed rule. All written comments timely received will be considered before a final determination is made on this rule. List of Subjects in 7 CFR Part 958 Marketing agreements, Onions, Reporting and recordkeeping requirements. For the reasons set forth in the preamble, the Agricultural Marketing Service proposes to amend 7 CFR part 958 as follows: PART 958—ONIONS GROWN IN CERTAIN DESIGNATED COUNTIES IN IDAHO, AND MALHEUR COUNTY, OREGON 1. The authority citation for 7 CFR part 958 continues to read as follows: ■ Authority: 7 U.S.C. 601–674. ■ Assessment rate. ddrumheller on DSK120RN23PROD with PROPOSALS1 On and after July 1, 2023, an assessment rate of $0.07 per hundredweight is established for IdahoEastern Oregon onions. Erin Morris, Associate Administrator, Agricultural Marketing Service. [FR Doc. 2023–27213 Filed 12–11–23; 8:45 am] BILLING CODE P VerDate Sep<11>2014 16:23 Dec 11, 2023 Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA–2023–2234; Project Identifier AD–2023–00963–T] RIN 2120–AA64 Airworthiness Directives; The Boeing Company Airplanes Federal Aviation Administration (FAA), DOT. ACTION: Notice of proposed rulemaking (NPRM). AGENCY: 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 two engine fan blade-out (FBO) events that resulted in the separation of engine inlet cowl and fan cowl parts from the airplane. In one event, fan cowl parts damaged the fuselage, which caused loss of pressurization and subsequent emergency descent. This proposed AD would require replacing the fasteners on the fan cowl support beam hinge fittings for certain airplanes and, for all airplanes, would require modifying the radial restraint assembly and installing an external doubler at the starter vent, or as an option, installing a serviceable fan cowl. This proposed AD would also require revising the existing maintenance or inspection program, as applicable, to incorporate new airworthiness limitations. 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 January 26, 2024. SUMMARY: 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–2023–2234; or in person at Docket Operations between 9 a.m. and ADDRESSES: 2. Revise § 958.240 to read as follows: § 958.240 DEPARTMENT OF TRANSPORTATION Jkt 262001 PO 00000 Frm 00004 Fmt 4702 Sfmt 4702 86069 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 service information identified in this NPRM, 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 by searching for and locating Docket No. FAA–2023–2234. FOR FURTHER INFORMATION CONTACT: Luis Cortez-Muniz, Aviation Safety Engineer, FAA, 2200 South 216th St., Des Moines, WA 98198; telephone: 206–231–3958; email: luis.a.cortez-muniz@faa.gov. SUPPLEMENTARY INFORMATION: Comments Invited The FAA invites you to send any written relevant data, views, or arguments about this proposal. Send your comments to an address listed under ADDRESSES. Include ‘‘Docket No. FAA–2023–2234; Project Identifier AD– 2023–00963–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 E:\FR\FM\12DEP1.SGM 12DEP1 86070 Federal Register / Vol. 88, No. 237 / Tuesday, December 12, 2023 / Proposed Rules ddrumheller on DSK120RN23PROD with PROPOSALS1 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 Luis Cortez-Muniz, Aviation Safety Engineer, FAA, 2200 South 216th St., Des Moines, WA 98198; telephone: 206–231–3958; email: luis.a.cortez-muniz@faa.gov. 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 received two reports of engine events that resulted in the separation of engine inlet cowl and fan cowl parts from the airplane. One event occurred in August 2016 on a Boeing Model 737–700 series airplane powered by a CFM56–7B engine. The left engine failed due to the FBO but the airplane landed successfully. The second event occurred on April 17, 2018, on a Boeing Model 737–700 series airplane powered by a CFM56–7B engine. In that event, an FBO occurrence resulted in the release of fan cowl parts and the engine cowling departing the airplane. The fan cowl parts damaged the fuselage, which caused loss of pressurization and subsequent emergency descent. Although the airplane landed safely, there was one passenger fatality. In that event, the suspected cause of the FBO occurrence was a low-cycle fatigue crack in the dovetail of fan blade number 13 of engine number 1. The broken fan blade hit the engine fan case at a critical location causing a significant impulse, displacement, and imbalance of the fan rotor effecting the structural integrity of the engine cowling. In response to these events, the FAA issued two AD actions for the CFM International S.A. (CFM) Model CFM56–7B engines. The FAA issued emergency AD 2018–09–51, Amendment 39–19287 (83 FR 23794, May 23, 2018) (AD 2018–09–51), which requires a one-time ultrasonic inspection of the concave and convex sides of the fan blade dovetail. The FAA also issued AD 2018–26–01, Amendment 39–19531 (83 FR 66090, December 26, 2018) (AD 2018–26–01), which requires initial and repetitive inspections of the concave and convex sides of the fan blade dovetail to detect VerDate Sep<11>2014 16:23 Dec 11, 2023 Jkt 262001 cracking and replacement of any blades found. The FAA issued AD 2018–09–51 to address fan blade failure due to cracking, which could result in an engine in-flight shutdown (IFSD), uncontained release of debris, damage to the engine, damage to the airplane, and possible airplane decompression. The FAA issued AD 2018–26–01 to address failure of the fan blade, which could result in the engine inlet cowl disintegrating and debris penetrating the fuselage, causing a loss of pressurization, and prompting an emergency descent. Since AD 2018–09–51 and AD 2018– 26–01 were issued, the FAA has determined further rulemaking is necessary to reduce the probability of unsecured nacelle components, should an engine fan blade failure occur. As evidenced by Exemption No. 19212, dated July 13, 2022 (Docket No. FAA– 2023–2234), Boeing developed modifications to the inlet cowl, fan cowl, and exhaust nozzle that must be accomplished prior to July 31, 2028. Boeing petitioned and the FAA later agreed to amend Exemption No. 19212 to 19212A, which added a requirement that solutions to address potential maintenance errors must be incorporated prior to December 31, 2029. However, to implement these design changes, the FAA must issue rulemaking to address the unsafe condition. This proposed AD would address fan cowls that are not strengthened, which could, in the event of an FBO occurrence, depart the nacelle potentially damaging a stabilizer, or the fan cowl could strike the fuselage and window. The unsafe condition, if not addressed, could result in loss of control of the airplane, or in a rapid decompression and hazard to windowseated passengers aft of the wing. 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 Special Attention Requirements Bulletin 737– 71–1937 RB, dated July 27, 2023. This service information specifies procedures for replacing, for certain airplanes, the fasteners on the fan cowl support beam hinge fittings on the left and right engine strut, and, for engine 1 and engine 2 for all airplanes, modifying the radial restraint assembly and installing an external doubler at the starter vent, PO 00000 Frm 00005 Fmt 4702 Sfmt 4702 or as an option, installing a serviceable fan cowl. The service information also requires revision of the operator’s maintenance or inspection program, as applicable, by incorporating certain airworthiness limitations (AWLs). 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 as discussed under ‘‘Differences Between this Proposed AD and the Service Information’’ and 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 regulations.gov under Docket No. FAA– 2023–2234. This proposed AD would require revisions to certain operator maintenance documents to include new airworthiness limitations. Compliance with these limitations is required by 14 CFR 91.403(c). For airplanes that have been previously modified, altered, or repaired in the areas addressed by this proposed AD, the operator may not be able to accomplish the actions described in the revisions. In this situation, to comply with 14 CFR 91.403(c), the operator must request approval for an alternative method of compliance according to paragraph (j) of this proposed AD. Differences Between This Proposed AD and the Service Information Boeing Special Attention Requirements Bulletin 737–71–1937 RB, dated July 27, 2023, identifies ‘‘System Airworthiness Limitation NO. 2—Fan Blade Out Conditions,’’ and ‘‘System Airworthiness Limitation NO. 3—Fan Blade Out Conditions’’ as the airworthiness limitations that must be incorporated. In addition to those system limitations, the FAA has determined that ‘‘System Airworthiness Limitation NO. 4—Engine Nacelle Maintenance Errors’’ must also be incorporated as specified in paragraph (h) of this proposed AD. System Airworthiness Limitation NO. 4 specifically provides the limitation that mandates solutions to maintenance errors that must be accomplished prior to December 31, 2029, as required by Exemption No. 19212A. E:\FR\FM\12DEP1.SGM 12DEP1 86071 Federal Register / Vol. 88, No. 237 / Tuesday, December 12, 2023 / Proposed Rules Costs of Compliance The FAA estimates that this AD, if adopted as proposed, would affect 1,979 airplanes of U.S. registry. The FAA estimates the following costs to comply with this proposed AD: ESTIMATED COSTS Action * Labor cost Parts cost Cost per product Modification and Installation ........ 140 work-hours × $85 per hour = $11,900. Up to 8 work-hour × $85 per hour = $680. $1,400 ........................ $13,300 ...................... $26,320,700. Up to $2,300 .............. Up to $2,980 .............. Up to $5,897,420. Fastener replacement .................. Cost on U.S. operators * The option to install a serviceable fan cowl would cost up to $16,280 per product. The FAA has determined that revising the existing maintenance or inspection program takes an average of 90 workhours per operator, although the agency recognizes that this number may vary from operator to operator. Since operators incorporate maintenance or inspection program changes for their affected fleet(s), the FAA has determined that a per-operator estimate is more accurate than a per-airplane estimate. Therefore, the agency estimates the average total cost per operator to be $7,650 (90 work-hours × $85 per work-hour). 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. ddrumheller on DSK120RN23PROD with PROPOSALS1 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. VerDate Sep<11>2014 16:23 Dec 11, 2023 Jkt 262001 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 1. The authority citation for part 39 continues to read as follows: ■ Authority: 49 U.S.C. 106(g), 40113, 44701. § 39.13 [Amended] 2. The FAA amends § 39.13 by adding the following new airworthiness directive: ■ The Boeing Company: Docket No. FAA– 2023–2234; Project Identifier AD–2023– 00963–T. (a) Comments Due Date The FAA must receive comments on this airworthiness directive (AD) by January 26, 2024. (b) Affected ADs None. (c) Applicability This AD applies to all The Boeing Company Model 737–600, –700, –700C, –800, –900, and –900ER series airplanes, certificated in any category. (d) Subject Air Transport Association (ATA) of America Code 71, Powerplant. PO 00000 Frm 00006 Fmt 4702 Sfmt 4702 (e) Unsafe Condition This AD was prompted by two engine fan blade-out (FBO) events that resulted in the separation of engine inlet cowl and fan cowl parts from the airplane. In one event, fan cowl parts damaged the fuselage, which caused loss of pressurization and subsequential emergency descent. The FAA is issuing this AD to address fan cowls that are not strengthened, which, in the event of an FBO occurrence, could depart the nacelle potentially damaging a stabilizer, or the fan cowl striking the fuselage and window. The unsafe condition, if not addressed, could result in loss of control of the airplane, or in a rapid decompression and hazard to window-seated passengers aft of the wing. (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 Special Attention Requirements Bulletin 737–71– 1937 RB, dated July 27, 2023, do all applicable actions identified in, and in accordance with, the Accomplishment Instructions of Boeing Special Attention Requirements Bulletin 737–71–1937 RB, dated July 27, 2023. Note 1 to paragraph (g): Guidance for accomplishing the actions required by this AD can be found in Boeing Special Attention Service Bulletin 737–71–1937, dated July 27, 2023, which is referred to in Boeing Special Attention Requirements Bulletin 737–71– 1937 RB, dated July 27, 2023. (h) Exceptions to Service Information Specifications (1) Where the service information referenced in paragraph (g) of this AD specifies contacting Boeing or Collins Aerospace for repair instructions: This AD requires doing the repair before further flight using a method approved in accordance with the procedures specified in paragraph (j) of this AD. (2) Where Tables 1 through 4 of Boeing Special Attention Requirements Bulletin 737–71–1937 RB, dated July 27, 2023, specify incorporating 737–600/700/700C/800/900/ 900ER Airworthiness Limitations (AWLs) document D626A001–9–01 ‘‘System Airworthiness Limitation NO. 2—Fan Blade E:\FR\FM\12DEP1.SGM 12DEP1 86072 Federal Register / Vol. 88, No. 237 / Tuesday, December 12, 2023 / Proposed Rules Out Conditions’’ and ‘‘System Airworthiness Limitation NO. 3—Fan Blade Out Conditions’’ into the operators’ maintenance program, this AD requires revising the existing maintenance or inspection program, as applicable, by incorporating the information specified in Figure 1 to the introductory text of paragraph (h) of this AD into the airworthiness limitations within 90 days after the effective date of this AD, or before further flight after accomplishing the (Option 1) or (Option 2) actions in Boeing Special Attention Requirements Bulletin 737–71–1937 RB, dated July 27, 2023, whichever occurs first. Figure 1 to the Introductory Text of Paragraph (h)—System Airworthiness Limitations SYSTEM .AIR.WORTHINESS LIMITATION No. 2 Fk~ BLADE OUT CONDmONS All airaaihnustinstall the following modifications: (l)engine inlets \\iith new spacer design and .increased fastener capability (2) fan cowls l\ith new radial testraiut fitting hooks. new radial restraint clips. and an external doubler at the starter \'ent (3)f.m cowl support beam fastener changes (except for 7'57:-900ER. aircraft, bee.use the fan cowl support beam fastener changes are already incmporated). All . aircraftthatha\.re not inootporated these modifkationscannotoperatepast July 31, 2028 unless upgraded to new hardware that is fully compliant to §§25.901(e) and AppendixK25.1.1 to Part 25. Boeing u,ill •release all sen.ice data to allow retrofit of hardware updates to the CFM56-1B nacelle prior to that date~ SYSTEM AIRWORTHINESS LIMITATION No. 3 FAN BLADE OUT CONDmONS All aircraft delivered without the Penonnance Improvement Package (PIP) must install engine exhaust nozzle stmctura1 stiffening: elements. All aircraft that have not incorporated these modifications cannot operate past July 31~ 2028 unless upgraded to new hardware that is fully compliant to §§25.901{c) and .Appendix K.25:1.1 to Part 25. Boeing "'ill release all sen'ice data to allow retrofit of hardware updates to the CFM56-1Bnacelle prior to that date. SYSTEMAIR.WORTHINESSLIMITATION No. 4 ENG~"E NACELLE :MAINTENANCE ERR.ORS ..\.11 aircraft must incmporate solutions to address potential maintenance errors. e.g., the failure to .. completely latch the f.m cowl or the fan cowl integrated drive generator (IDG) door. All aircraft that have not incotpOrated dlanges to become fully compliant 'INith §§25.901(c) and AppendixK.2S;Lt to Part 25 cannot be operated past December 31~ 20.29. After the existing maintenance or inspection program has been revised as required by paragraph (h)(2) of this AD, no alternative actions may be used unless the actions are approved as an alternative method of compliance (AMOC) in accordance with the procedures specified in paragraph (j) of this AD. ddrumheller on DSK120RN23PROD with PROPOSALS1 (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 the certification office, send it to the attention of the person identified in paragraph (k) of this AD. Information may be emailed to: 9-ANMSeattle-ACO-AMOC-Requests@faa.gov. (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 VerDate Sep<11>2014 16:23 Dec 11, 2023 Jkt 262001 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. (k) Related Information For more information about this AD, contact Luis Cortez-Muniz, Aviation Safety Engineer, FAA, 2200 South 216th St., Des Moines, WA 98198; telephone: 206–231– 3958; email: luis.a.cortez-muniz@faa.gov. (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 Special Attention Requirements Bulletin 737–71–1937 RB, dated July 27, 2023. (ii) [Reserved] (3) For service information identified in this AD, contact Boeing Commercial PO 00000 Frm 00007 Fmt 4702 Sfmt 9990 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 fr.inspection@nara.gov. Issued on December 1, 2023. Victor Wicklund, Deputy Director, Compliance & Airworthiness Division, Aircraft Certification Service. [FR Doc. 2023–27100 Filed 12–11–23; 8:45 am] BILLING CODE 4910–13–P E:\FR\FM\12DEP1.SGM 12DEP1 EP12DE23.002</GPH> (i) No Alternative Actions

Agencies

[Federal Register Volume 88, Number 237 (Tuesday, December 12, 2023)]
[Proposed Rules]
[Pages 86069-86072]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2023-27100]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2023-2234; Project Identifier AD-2023-00963-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 two engine 
fan blade-out (FBO) events that resulted in the separation of engine 
inlet cowl and fan cowl parts from the airplane. In one event, fan cowl 
parts damaged the fuselage, which caused loss of pressurization and 
subsequent emergency descent. This proposed AD would require replacing 
the fasteners on the fan cowl support beam hinge fittings for certain 
airplanes and, for all airplanes, would require modifying the radial 
restraint assembly and installing an external doubler at the starter 
vent, or as an option, installing a serviceable fan cowl. This proposed 
AD would also require revising the existing maintenance or inspection 
program, as applicable, to incorporate new airworthiness limitations. 
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 January 26, 
2024.

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-2023-2234; 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 service information identified in this NPRM, 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 by searching for and locating Docket No. FAA-2023-2234.

FOR FURTHER INFORMATION CONTACT: Luis Cortez-Muniz, Aviation Safety 
Engineer, FAA, 2200 South 216th St., Des Moines, WA 98198; telephone: 
206-231-3958; 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 to an address listed 
under ADDRESSES. Include ``Docket No. FAA-2023-2234; Project Identifier 
AD-2023-00963-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

[[Page 86070]]

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 Luis Cortez-Muniz, 
Aviation Safety Engineer, FAA, 2200 South 216th St., Des Moines, WA 
98198; telephone: 206-231-3958; 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 received two reports of engine events that resulted in the 
separation of engine inlet cowl and fan cowl parts from the airplane. 
One event occurred in August 2016 on a Boeing Model 737-700 series 
airplane powered by a CFM56-7B engine. The left engine failed due to 
the FBO but the airplane landed successfully. The second event occurred 
on April 17, 2018, on a Boeing Model 737-700 series airplane powered by 
a CFM56-7B engine. In that event, an FBO occurrence resulted in the 
release of fan cowl parts and the engine cowling departing the 
airplane. The fan cowl parts damaged the fuselage, which caused loss of 
pressurization and subsequent emergency descent. Although the airplane 
landed safely, there was one passenger fatality. In that event, the 
suspected cause of the FBO occurrence was a low-cycle fatigue crack in 
the dovetail of fan blade number 13 of engine number 1. The broken fan 
blade hit the engine fan case at a critical location causing a 
significant impulse, displacement, and imbalance of the fan rotor 
effecting the structural integrity of the engine cowling.
    In response to these events, the FAA issued two AD actions for the 
CFM International S.A. (CFM) Model CFM56-7B engines. The FAA issued 
emergency AD 2018-09-51, Amendment 39-19287 (83 FR 23794, May 23, 2018) 
(AD 2018-09-51), which requires a one-time ultrasonic inspection of the 
concave and convex sides of the fan blade dovetail. The FAA also issued 
AD 2018-26-01, Amendment 39-19531 (83 FR 66090, December 26, 2018) (AD 
2018-26-01), which requires initial and repetitive inspections of the 
concave and convex sides of the fan blade dovetail to detect cracking 
and replacement of any blades found. The FAA issued AD 2018-09-51 to 
address fan blade failure due to cracking, which could result in an 
engine in-flight shutdown (IFSD), uncontained release of debris, damage 
to the engine, damage to the airplane, and possible airplane 
decompression. The FAA issued AD 2018-26-01 to address failure of the 
fan blade, which could result in the engine inlet cowl disintegrating 
and debris penetrating the fuselage, causing a loss of pressurization, 
and prompting an emergency descent.
    Since AD 2018-09-51 and AD 2018-26-01 were issued, the FAA has 
determined further rulemaking is necessary to reduce the probability of 
unsecured nacelle components, should an engine fan blade failure occur. 
As evidenced by Exemption No. 19212, dated July 13, 2022 (Docket No. 
FAA-2023-2234), Boeing developed modifications to the inlet cowl, fan 
cowl, and exhaust nozzle that must be accomplished prior to July 31, 
2028. Boeing petitioned and the FAA later agreed to amend Exemption No. 
19212 to 19212A, which added a requirement that solutions to address 
potential maintenance errors must be incorporated prior to December 31, 
2029. However, to implement these design changes, the FAA must issue 
rulemaking to address the unsafe condition.
    This proposed AD would address fan cowls that are not strengthened, 
which could, in the event of an FBO occurrence, depart the nacelle 
potentially damaging a stabilizer, or the fan cowl could strike the 
fuselage and window. The unsafe condition, if not addressed, could 
result in loss of control of the airplane, or in a rapid decompression 
and hazard to window-seated passengers aft of the wing.

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 Special Attention Requirements Bulletin 
737-71-1937 RB, dated July 27, 2023. This service information specifies 
procedures for replacing, for certain airplanes, the fasteners on the 
fan cowl support beam hinge fittings on the left and right engine 
strut, and, for engine 1 and engine 2 for all airplanes, modifying the 
radial restraint assembly and installing an external doubler at the 
starter vent, or as an option, installing a serviceable fan cowl.
    The service information also requires revision of the operator's 
maintenance or inspection program, as applicable, by incorporating 
certain airworthiness limitations (AWLs).
    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 as discussed under 
``Differences Between this Proposed AD and the Service Information'' 
and 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 regulations.gov 
under Docket No. FAA-2023-2234.
    This proposed AD would require revisions to certain operator 
maintenance documents to include new airworthiness limitations. 
Compliance with these limitations is required by 14 CFR 91.403(c). For 
airplanes that have been previously modified, altered, or repaired in 
the areas addressed by this proposed AD, the operator may not be able 
to accomplish the actions described in the revisions. In this 
situation, to comply with 14 CFR 91.403(c), the operator must request 
approval for an alternative method of compliance according to paragraph 
(j) of this proposed AD.

Differences Between This Proposed AD and the Service Information

    Boeing Special Attention Requirements Bulletin 737-71-1937 RB, 
dated July 27, 2023, identifies ``System Airworthiness Limitation NO. 
2--Fan Blade Out Conditions,'' and ``System Airworthiness Limitation 
NO. 3--Fan Blade Out Conditions'' as the airworthiness limitations that 
must be incorporated. In addition to those system limitations, the FAA 
has determined that ``System Airworthiness Limitation NO. 4--Engine 
Nacelle Maintenance Errors'' must also be incorporated as specified in 
paragraph (h) of this proposed AD. System Airworthiness Limitation NO. 
4 specifically provides the limitation that mandates solutions to 
maintenance errors that must be accomplished prior to December 31, 
2029, as required by Exemption No. 19212A.

[[Page 86071]]

Costs of Compliance

    The FAA estimates that this AD, if adopted as proposed, would 
affect 1,979 airplanes of U.S. registry. The FAA estimates the 
following costs to comply with this proposed AD:

                                                 Estimated Costs
----------------------------------------------------------------------------------------------------------------
                                                                                                 Cost on U.S.
            Action *                  Labor cost          Parts cost       Cost per product        operators
----------------------------------------------------------------------------------------------------------------
Modification and Installation...  140 work-hours x    $1,400............  $13,300...........  $26,320,700.
                                   $85 per hour =
                                   $11,900.
Fastener replacement............  Up to 8 work-hour   Up to $2,300......  Up to $2,980......  Up to $5,897,420.
                                   x $85 per hour =
                                   $680.
----------------------------------------------------------------------------------------------------------------
* The option to install a serviceable fan cowl would cost up to $16,280 per product.

    The FAA has determined that revising the existing maintenance or 
inspection program takes an average of 90 work-hours per operator, 
although the agency recognizes that this number may vary from operator 
to operator. Since operators incorporate maintenance or inspection 
program changes for their affected fleet(s), the FAA has determined 
that a per-operator estimate is more accurate than a per-airplane 
estimate. Therefore, the agency estimates the average total cost per 
operator to be $7,650 (90 work-hours x $85 per work-hour).

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:

The Boeing Company: Docket No. FAA-2023-2234; Project Identifier AD-
2023-00963-T.

(a) Comments Due Date

    The FAA must receive comments on this airworthiness directive 
(AD) by January 26, 2024.

(b) Affected ADs

    None.

(c) Applicability

    This AD applies to all The Boeing Company Model 737-600, -700, -
700C, -800, -900, and -900ER series airplanes, certificated in any 
category.

(d) Subject

    Air Transport Association (ATA) of America Code 71, Powerplant.

(e) Unsafe Condition

    This AD was prompted by two engine fan blade-out (FBO) events 
that resulted in the separation of engine inlet cowl and fan cowl 
parts from the airplane. In one event, fan cowl parts damaged the 
fuselage, which caused loss of pressurization and subsequential 
emergency descent. The FAA is issuing this AD to address fan cowls 
that are not strengthened, which, in the event of an FBO occurrence, 
could depart the nacelle potentially damaging a stabilizer, or the 
fan cowl striking the fuselage and window. The unsafe condition, if 
not addressed, could result in loss of control of the airplane, or 
in a rapid decompression and hazard to window-seated passengers aft 
of the wing.

(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 
Special Attention Requirements Bulletin 737-71-1937 RB, dated July 
27, 2023, do all applicable actions identified in, and in accordance 
with, the Accomplishment Instructions of Boeing Special Attention 
Requirements Bulletin 737-71-1937 RB, dated July 27, 2023.
    Note 1 to paragraph (g): Guidance for accomplishing the actions 
required by this AD can be found in Boeing Special Attention Service 
Bulletin 737-71-1937, dated July 27, 2023, which is referred to in 
Boeing Special Attention Requirements Bulletin 737-71-1937 RB, dated 
July 27, 2023.

(h) Exceptions to Service Information Specifications

    (1) Where the service information referenced in paragraph (g) of 
this AD specifies contacting Boeing or Collins Aerospace for repair 
instructions: This AD requires doing the repair before further 
flight using a method approved in accordance with the procedures 
specified in paragraph (j) of this AD.
    (2) Where Tables 1 through 4 of Boeing Special Attention 
Requirements Bulletin 737-71-1937 RB, dated July 27, 2023, specify 
incorporating 737-600/700/700C/800/900/900ER Airworthiness 
Limitations (AWLs) document D626A001-9-01 ``System Airworthiness 
Limitation NO. 2--Fan Blade

[[Page 86072]]

Out Conditions'' and ``System Airworthiness Limitation NO. 3--Fan 
Blade Out Conditions'' into the operators' maintenance program, this 
AD requires revising the existing maintenance or inspection program, 
as applicable, by incorporating the information specified in Figure 
1 to the introductory text of paragraph (h) of this AD into the 
airworthiness limitations within 90 days after the effective date of 
this AD, or before further flight after accomplishing the (Option 1) 
or (Option 2) actions in Boeing Special Attention Requirements 
Bulletin 737-71-1937 RB, dated July 27, 2023, whichever occurs 
first.

Figure 1 to the Introductory Text of Paragraph (h)--System 
Airworthiness Limitations
[GRAPHIC] [TIFF OMITTED] TP12DE23.002

(i) No Alternative Actions

    After the existing maintenance or inspection program has been 
revised as required by paragraph (h)(2) of this AD, no alternative 
actions may be used unless the actions are approved as an 
alternative method of compliance (AMOC) in accordance with the 
procedures specified in paragraph (j) of this AD.

(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 the certification office, 
send it to the attention of the person identified in paragraph (k) 
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.

(k) Related Information

    For more information about this AD, contact Luis Cortez-Muniz, 
Aviation Safety Engineer, FAA, 2200 South 216th St., Des Moines, WA 
98198; telephone: 206-231-3958; email: [email protected].

(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 Special Attention Requirements Bulletin 737-71-1937 
RB, dated July 27, 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 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 December 1, 2023.
Victor Wicklund,
Deputy Director, Compliance & Airworthiness Division, Aircraft 
Certification Service.
[FR Doc. 2023-27100 Filed 12-11-23; 8:45 am]
BILLING CODE 4910-13-P

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