2026-13129: Airworthiness Directives; The Boeing Company Airplanes
Public comment closed · opened June 30, 2026.
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The FAA proposes to adopt a new airworthiness directive (AD) for certain The Boeing Company Model 747-400 series airplanes. This proposed AD was prompted by reports of potable water leaking into the electrical equipment bay cooling air inlet. This proposed AD would require performing repetitive inspections of potential water sources from the upper deck and the main deck, including potable water and waste water lines, for any water leaks and clogs, and applicable on- condition actions. The FAA is proposing this AD to address the unsafe condition on these products.
The agency’s own summary, as published.
The rule, in full
2,682 words as published, June 30, 2026. View the original →
Federal Register, Volume 91 Issue 124 (Tuesday, June 30, 2026) [Federal Register Volume 91, Number 124 (Tuesday, June 30, 2026)] [Proposed Rules] [Pages 39573-39575] From the Federal Register Online via the Government Publishing Office [www.gpo.gov] [FR Doc No: 2026-13129] ----------------------------------------------------------------------- DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2026-4668; Project Identifier AD-2025-01680-T] RIN 2120-AA64 Airworthiness Directives; The Boeing Company Airplanes
Agency
Federal Aviation Administration (FAA), DOT.
Action
Notice of proposed rulemaking (NPRM). -----------------------------------------------------------------------
Summary
The FAA proposes to adopt a new airworthiness directive (AD) for certain The Boeing Company Model 747-400 series airplanes. This proposed AD was prompted by reports of potable water leaking into the electrical equipment bay cooling air inlet. This proposed AD would require performing repetitive inspections of potential water sources from the upper deck and the main deck, including potable water and waste water lines, for any water leaks and clogs, and applicable on- condition actions. 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 14, 2026.
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-2026-4668; 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 Boeing material identified in this proposed 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. You may view this material at the FAA, Airworthiness Products Section, Operational Safety Branch, 2200 South 216th St., Des Moines, WA. For information on the availability of this material at the FAA, call 206-231-3195. It is also available at regulations.gov under Docket No. FAA-2026-4668.
For Further Information Contact
Nicole S. Tsang, Aviation Safety Engineer, FAA, 2200 South 216th St., Des Moines, WA 98198; phone: 206- 231-3959; email: [email protected].
Supplementary Information
Comments Invited The FAA invites you to send any written relevant data, views, or arguments about this proposal. Send your comments using a method listed under the ADDRESSES section. Include ``Docket No. FAA-2026-4668; Project Identifier AD-2025-01680-T'' at the beginning of your comments. The most helpful comments reference a specific portion of the proposal, explain the reason for any recommended change, and include supporting data. The FAA will consider all comments received by the closing date and may amend this proposal because of those comments. Except for Confidential Business Information (CBI) as described in the following paragraph, and other information as described in 14 CFR 11.35, the FAA will post all comments received, without change, to regulations.gov, including any personal information you provide. The agency will also post a report summarizing each substantive verbal contact received about this NPRM. Confidential Business Information CBI is commercial or financial information that is both customarily and actually treated as private by its owner. Under the Freedom of Information Act (FOIA) (5 U.S.C. 552), CBI is exempt from public disclosure. If your comments responsive to this NPRM contain commercial or financial information that is customarily treated as private, that you actually treat as private, and that is relevant or responsive to this NPRM, it is important that you clearly designate the submitted comments as CBI. Please mark each page of your submission containing CBI as ``PROPIN.'' The FAA will treat such marked submissions as confidential under the FOIA, and they will not be placed in the public docket of this NPRM. Submissions containing CBI should be sent to Nicole S. Tsang, Aviation Safety Engineer, FAA, 2200 South 216th St., Des Moines, WA 98198; phone: 206-231-3959; 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 reports of potable water leaking into the electrical equipment bay cooling air inlet on the Boeing Model 777F series airplanes. There are no reported events of water leaking into the electrical equipment bay cooling air inlet on the large cargo freighter variant of the Model 747-400 series airplanes. However, there are reported events of leakages on the upper deck in areas that could pool and drip onto the air inlet. The FAA has determined that the large cargo freighter variant has unique design features that introduce several potential potable and waste water sources from the upper deck and the main deck that could leak into the air inlet and enter the electrical equipment bay. This condition, if not addressed, could impact the function of multiple electronics and line replaceable units in the equipment bay racks that are essential for safe flight, which could result in loss of continued safe flight and landing. 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. Material Incorporated by Reference Under 1 CFR Part 51 The FAA reviewed Boeing Message TBC-TBC-25-6694-01B, dated [[Page 39574]] November 7, 2025 (pages 4 through 15 of this document are dated October 29, 2025). This material specifies procedures for the following repetitive inspections of potential water sources from the upper deck and the main deck, including potable water and waste water lines, for any water leaks and clogs, and applicable on-condition actions. The inspections include the following actions: Perform general visual inspection (GVI) of the potable water lines for any water leaks; Run the coffee maker through a brew cycle; Perform GVI of the galley compartments for any water leaks; Check for any indication of clog from the drainage system in the lavatory and galley sinks and the lavatory and galley sink drains; Perform GVI of the floor of the lavatory, the lavatory sink, the area behind the galley on its outboard left side including the potable water and waste water lines, and the upper deck hallway floor for signs of leakage; and Inspect the potable water and drain lines running along the main deck ceiling for sign of leaks. On-condition actions include using normal operator procedures and repeating the work step(s) as required to resolve the leakage or clog or rendering the water/waste systems or individual components inoperable; and checking the engine indication crew alert system (EICAS) display for any new messages. This material is reasonably available because the interested parties have access to it through their normal course of business or by the means identified in the ADDRESSES section. Proposed AD Requirements in This NPRM This proposed AD would require accomplishing the actions identified as ``RC'' (required for compliance) in the Water Leak Check Work Instructions of Boeing Message TBC-TBC-25-6694-01B, dated November 7, 2025, 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 material at regulations.gov under Docket No. FAA-2026-4668. Clarification of Compliance Time for On-Condition Actions Although Boeing Message TBC-TBC-25-6694-01B, dated November 7, 2025, specifies the compliance time to perform RC actions is within 1,000 flight hours (FH) of the date of Boeing Message TBC-TBC-25-6694- 01B and at recurring intervals not to exceed 1,000 FH, step 27 of the Water Leak Check Work Instructions specifies the compliance times for the applicable on-condition actions are before further flight. Therefore, paragraph (h)(2) of this proposed AD would require the applicable on-condition actions to be done before further flight. Interim Action The FAA considers that this proposed AD would be an interim action. The manufacturer is currently developing a modification that will address the unsafe condition identified in this AD. Once this modification is developed, approved, and available, the FAA might consider additional rulemaking. Costs of Compliance The FAA estimates that this AD, if adopted as proposed, would affect 4 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 ---------------------------------------------------------------------------------------------------------------- Inspection....................... 5 work-hours x $85 $0 $425 per inspection $1,700 per per hour = $425 cycle. inspection cycle. per inspection cycle. ---------------------------------------------------------------------------------------------------------------- The FAA estimates the following costs to do any necessary on- condition actions that would be required based on the results of the proposed inspection. The agency has no way of determining the number of aircraft that might need these on-condition actions: On-Condition Costs ---------------------------------------------------------------------------------------------------------------- Action Labor cost Parts cost Cost per product ---------------------------------------------------------------------------------------------------------------- On-condition actions.................... Up to 6 work-hours x $85 $0 Up to $510. per hour = $510. ---------------------------------------------------------------------------------------------------------------- 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. [[Page 39575]] 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-2026-4668; Project Identifier AD- 2025-01680-T. (a) Comments Due Date The FAA must receive comments on this airworthiness directive (AD) by August 14, 2026. (b) Affected ADs None. (c) Applicability This AD applies to The Boeing Company Model 747-400 series airplanes, certificated in any category, as identified in Boeing Message TBC-TBC-25-6694-01B, dated November 7, 2025. (d) Subject Air Transport Association (ATA) of America Code 38, Water/waste. (e) Unsafe Condition This AD was prompted by reports of potable water leaking into the electrical equipment bay cooling air inlet. The FAA is issuing this AD to address water leaking into the air inlet and entering the electrical equipment bay. The unsafe condition, if not addressed, could impact the function of multiple electronics and line replaceable units in the equipment bay racks that are essential for safe flight, which could result in loss of continued safe flight and landing. (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: At the applicable times specified in paragraph ``Recommended Incorporation Timeframe'' of Boeing Message TBC-TBC-25-6694-01B, dated November 7, 2025, do all applicable actions identified as ``RC'' (required for compliance) in, and in accordance with, the Water Leak Check Work Instructions of Boeing Message TBC-TBC-25-6694-01B, dated November 7, 2025. (h) Exceptions to Service Bulletin Specifications (1) Where Boeing Message TBC-TBC-25-6694-01B, dated November 7, 2025, refers to the message date of Boeing Message TBC-TBC-25-6694- 01B, this AD requires using the effective date of this AD. (2) This AD requires performing all applicable on-condition actions as specified in step 27 of the Water Leak Check Work Instructions of Boeing Message TBC-TBC-25-6694-01B before further flight. (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) of this AD. Information may be emailed to: [email protected]. Before using any approved AMOC, notify your appropriate principal inspector, or lacking a principal inspector, the manager of the responsible Flight Standards Office. (2) 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. (3) For material that contains steps that are labeled as Required for Compliance (RC), the provisions of paragraphs (i)(3)(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) Additional Information For more information about this AD, contact Nicole S. Tsang, Aviation Safety Engineer, FAA, 2200 South 216th St., Des Moines, WA 98198; phone: 206-231-3959; email: [email protected]. (k) Material Incorporated by Reference (1) The Director of the Federal Register approved the incorporation by reference of the material listed in this paragraph under 5 U.S.C. 552(a) and 1 CFR part 51. (2) You must use this material as applicable to do the actions required by this AD, unless the AD specifies otherwise. (i) Boeing Message TBC-TBC-25-6694-01B, dated November 7, 2025. Note 1 to paragraph (k)(2)(i): Pages 4 through 15 of this document are dated October 29, 2025. (ii) [Reserved] (3) For Boeing material 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 material at the FAA, Airworthiness Products Section, Operational Safety Branch, 2200 South 216th St., Des Moines, WA. For information on the availability of this material at the FAA, call 206-231-3195. (5) You may view this material at the National Archives and Records Administration (NARA). For information on the availability of this material at NARA, visit www.archives.gov/federal-register/cfr/ibr-locations or email [email protected]. Issued on June 24, 2026. Brian Knaup, Acting Deputy Director, Integrated Certificate Management Division, Aircraft Certification Service. [FR Doc. 2026-13129 Filed 6-29-26; 8:45 am] BILLING CODE 4910-13-P
What this changes
Amends 1 part of the Code of Federal Regulations — the standing rules this notice rewrites.
Rulemaking docket
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Proposed Rule June 30, 2026Airworthiness Directives: The Boeing Company Airplanes
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Supporting & Related Material June 30, 2026U.S. DOT/FAA - Supplemental AD Documents
Public comments
What people are saying
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Air Line Pilots Association, Int'l 2026-08-17
“See attached file(s)”
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The Foundation for Aviation Safety 2026-08-10
“The Foundation for Aviation Safety is wondering when this water leak problem was first reported by operators. Water leaking into electronic equipment is extremely dangerous. Why is it taking the FAA so long to make this straightforward inspection mandatory? This problem is also widespread among other Boeing models. Air India 171 also reported water leakage into its E/E Bay.”
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Boeing Commercial Airplanes 2026-08-05
“Concur, no additional comments will be forthcoming”
Read all comments on Regulations.gov →
Comment volume from Regulations.gov; the comment-submission API was retired in 2025, so comments are filed on Regulations.gov directly.
Documents
- Full text (Federal Register) · June 30, 2026
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