- Effective
- October 7, 2024
- Published
- September 20, 2024 · 89 FR 77013–77015
- Issued
- September 13, 2024
- Models
- LEAP-1A32, A321-251NX
- Data sheets
- TCDSA28NMTCDSE00089EN
- Product
- Engine · Large airplane
- ATA chapter
- 73 · Engine fuel and control
- Amendment
- 39-22849
- Docket
- FAA-2024-2146
- Project
- AD-2024-00464-E
- Issued as
- Final rule; request for comments
Unofficial copy from the Federal Register XML, document 2024-21408. Only the govinfo PDF is the legal edition. DRS record last changed November 21, 2025.
Copies of the files this page was built from, with their SHA-256. Retrieved October 18, 2026.
| File | Size | SHA-256 | Original |
|---|---|---|---|
| Official PDF | 245 KB | dffef1b5…38160d6 | 2024-21408.pdf on govinfo.gov |
| Federal Register XML | 19 KB | 67107c72…a37081b | 2024-21408.xml on federalregister.gov |
| FAA DRS HTML | 37 KB | c6d4003a…222fcc0 | FAA DRS (API key needed) |
On this page
Summary
The FAA is adopting a new airworthiness directive (AD) for certain CFM International, S.A. (CFM) Model LEAP-1A32 engines. This AD was prompted by a report of multiple events of loss of thrust control during go-around. This AD requires replacement of the full set of fuel nozzles. The FAA is issuing this AD to address the unsafe condition on these products.
The airworthiness directive
2024-19-07 CFM International, S.A.: Amendment 39-22849; Docket No. FAA-2024-2146; Project Identifier AD-2024-00464-E.
(a) Effective Date
PDF page 2This airworthiness directive (AD) is effective October 7, 2024.
(b) Affected ADs
PDF page 2None.
(c) Applicability
PDF page 2This AD applies to CFM International, S.A. (CFM) Model LEAP-1A32 engines installed on Airbus SAS Model A321-251NX airplanes having any of the following airplane serial numbers: 11200, 11420, 11473, 11609, 11698, 11791, 11815, 12136, 12314, and 12370.
(d) Subject
PDF page 2Joint Aircraft System Component (JASC) Code 7300, Engine Fuel and Control.
(e) Unsafe Condition
PDF page 2This AD was prompted by a report of multiple events of loss of thrust control during go-around. The FAA is issuing this AD to prevent the loss of engine thrust control. The unsafe condition, if not addressed, could result in reduced control of the airplane.
(f) Compliance
PDF page 2Comply with this AD within the compliance times specified, unless already done.
(g) Required Actions
PDF page 2(1) At the applicable times specified in paragraphs (g)(1)(i) and (ii) of this AD, replace the full set of fuel nozzles, on each engine, with parts eligible for installation.
(i) On either affected engine installed on the airplane: Before accumulating 600 flight cycles (FCs) since new or since last replacement of the full set of fuel nozzles, or within 10 FCs after the effective date of this AD, whichever occurs later.
(ii) On the other affected engine installed on the same airplane: Before accumulating 800 FCs since new or since last replacement of the full set of fuel nozzles, or within 10 FCs after the effective date of this AD, whichever occurs later.
(2) Thereafter, on each affected engine installed on the airplane, at intervals not to exceed 600 FCs since last replacement of the full set of fuel nozzles, replace the full set of fuel nozzles with parts eligible for installation.
(h) Definition
PDF page 2For the purpose of this AD, “parts eligible for installation” are new fuel nozzles or fuel nozzles made serviceable using CFM Component Maintenance Manual (CMM) 73-11-30 (CFM-TP.CM.056.), any revision.
(i) Alternative Methods of Compliance (AMOCs)
PDF page 2(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 local Flight Standards District Office, as appropriate. If sending information directly to the manager of AIR-520 Continued Operational Safety Branch, send it to the attention of the person identified in paragraph (j)(1) of this AD and email to: AMOC@faa.gov.
(2) Before using any approved AMOC, notify your appropriate principal inspector, or lacking a principal inspector, the manager of the local flight standards district office/certificate holding district office.
(j) Additional Information
PDF page 3(1) For more information about this AD, contact Mehdi Lamnyi, Aviation Safety Engineer, FAA, 2200 South 216th Street, Des Moines, WA 98198; phone: (781) 238-7743; email: mehdi.lamnyi@faa.gov.
(2) Material identified in this AD that is not incorporated by reference is available at CFM International, S.A., GE Aviation Fleet Support, 1 Neumann Way, M/D Room 285, Cincinnati, OH 45215; phone: (877) 432-3272; email: aviation.fleetsupport@ge.com.
(k) Material Incorporated by Reference
PDF page 3None.
Rule preamble
The FAA’s background, reasoning and cost estimate, published with the AD.
DatesPage 1
This AD is effective October 7, 2024.
The FAA must receive comments on this AD by November 4, 2024.
AddressesPage 1
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-2024-2146; 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 street address for Docket Operations is listed above.
For further information contactPage 1
Mehdi Lamnyi, Aviation Safety Engineer, FAA, 2200 South 216th Street, Des Moines, WA 98198; phone: (781) 238-7743; email: mehdi.lamnyi@faa.gov.
Comments invitedPage 1
The FAA invites you to send any written data, views, or arguments about this final rule. Send your comments to an address listed under the ADDRESSES section. Include “Docket No. FAA-2024-2146; Project Identifier AD-2024-00464-E” at the beginning of your comments. The most helpful comments reference a specific portion of the final rule, 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 final rule 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 final rule.
Confidential business informationPage 1
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 AD 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 AD, 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 AD. Submissions containing CBI should be sent to Mehdi Lamnyi, Aviation Safety Engineer, FAA, 2200 South 216th Street, Des Moines, WA 98198. Any commentary that the FAA receives which is not specifically designated as CBI will be placed in the public docket for this rulemaking.
BackgroundPage 1
On January 11, 2024, an Airbus Model A321neo airplane powered by CFM Model LEAP-1A engines experienced a loss of thrust control on engine 1 during a go-around. On February 4, 2024, the same Airbus Model A321neo airplane experienced N1 fluctuation/reduction on engine 2 during a go-around. A manufacturer investigation determined that significantly higher than expected fuel nozzle coking was creating back pressure in the fuel system that then triggered the fuel pump relief valve to open, reducing fuel flow to the engine and resulting in a reduction in thrust. This condition, if not addressed, could result in loss of engine thrust control and reduced control of the airplane. The FAA is issuing this AD to address the unsafe condition on these products.
FAA's DeterminationPage 1
The FAA is issuing this AD because the agency determined the unsafe condition described previously is likely to exist or develop in other products of the same type design.
AD RequirementsPage 1
This AD requires replacement of the full set of fuel nozzles.
Interim actionPage 1
The FAA considers this AD to be an interim action. The unsafe condition is still under investigation by the manufacturer and, depending on the results of that investigation, the FAA may consider further rulemaking action.
Justification for Immediate Adoption and Determination of the Effective DatePage 1
Section 553(b) of the Administrative Procedure Act (APA) (5 U.S.C. 551 et seq.) authorizes agencies to dispense with notice and comment procedures for rules when the agency, for “good cause,” finds that those procedures are “impracticable, unnecessary, or contrary to the public interest.” Under this section, an agency, upon finding good cause, may issue a final rule without providing notice and seeking comment prior to issuance. Further, section 553(d) of the APA authorizes agencies to make rules effective in less than thirty days, upon a finding of good cause.
The FAA justifies waiving notice and comment prior to adoption of this rule because no domestic operators use this product. It is unlikely that the FAA will receive any adverse comments or useful information about this AD from any U.S. operator. Accordingly, notice and opportunity for prior public comment are unnecessary, pursuant to 5 U.S.C. 553(b). In addition, for the foregoing reason(s), the FAA finds that good cause exists pursuant to 5 U.S.C. 553(d) for making this amendment effective in less than 30 days.
Regulatory flexibility actPage 2
The requirements of the Regulatory Flexibility Act (RFA) do not apply when an agency finds good cause pursuant to 5 U.S.C. 553 to adopt a rule without prior notice and comment. Because FAA has determined that it has good cause to adopt this rule without prior notice and comment, RFA analysis is not required.
Costs of CompliancePage 2
The FAA estimates that this AD affects 0 engines installed on airplanes of U.S. registry.
The FAA estimates the following costs to comply with this AD:
| Action | Labor cost | Parts cost | Cost per product | Cost on U.S. operators |
|---|---|---|---|---|
| Replace the full set of fuel nozzles | 40 work-hours × $85 per hour = $3,400 | $126,000 | $129,400 | $0 |
Authority for This RulemakingPage 2
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 findingsPage 2
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, and
(2) Will not affect intrastate aviation in Alaska.
The amendmentPage 2
Accordingly, under the authority delegated to me by the Administrator, the FAA amends 14 CFR part 39 as follows:
Adoption of the amendmentPage 2
1. The authority citation for part 39 continues to read as follows:
2. The FAA amends § 39.13 by adding the following new airworthiness directive:
Affected TCDS · 2
The type certificate data sheets for the models this AD names, matched by model and maker.