DEPARTMENT OF TRANSPORTATION
<SUBAGY>Federal Aviation Administration</SUBAGY>
<CFR>14 CFR Part 39</CFR>
<DEPDOC>[Docket No. FAA-2025-2260; Project Identifier MCAI-2025-00043-T]</DEPDOC>
<RIN>RIN 2120-AA64</RIN>
<SUBJECT>Airworthiness Directives; Gulfstream Aerospace LP (Type Certificate Previously Held by Israel Aircraft Industries, Ltd.) Airplanes</SUBJECT>
<HD SOURCE="HED">AGENCY:</HD>
Federal Aviation Administration (FAA), DOT.
<HD SOURCE="HED">ACTION:</HD>
Notice of proposed rulemaking (NPRM).
<SUM>
<HD SOURCE="HED">SUMMARY:</HD>
The FAA proposes to adopt a new airworthiness directive (AD) for all Gulfstream Aerospace LP Model Gulfstream 100, Astra SPX, and 1125 Westwind Astra airplanes. This proposed AD was prompted by a determination that new airworthiness limitations are necessary. This proposed AD would 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.
</SUM>
<EFFDATE>
<HD SOURCE="HED">DATES:</HD>
The FAA must receive comments on this proposed AD by October 6, 2025.
</EFFDATE>
<HD SOURCE="HED">ADDRESSES:</HD>
You may send comments, using the procedures found in 14 CFR 11.43 and 11.45, by any of the following methods:
•
<E T="03">Federal eRulemaking Portal:</E>
Go to
<E T="03">regulations.gov</E>
. Follow the instructions for submitting comments.
•
<E T="03">Fax:</E>
202-493-2251.
•
<E T="03">Mail:</E>
U.S. Department of Transportation, Docket Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New Jersey Avenue SE, Washington, DC 20590.
•
<E T="03">Hand Delivery:</E>
Deliver to Mail address above between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays.
<E T="03">AD Docket:</E>
You may examine the AD docket at
<E T="03">regulations.gov</E>
under Docket No. FAA-2025-2260; 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, the mandatory continuing airworthiness information (MCAI), any comments received, and other information. The street address for Docket Operations is listed above.
<E T="03">Material Incorporated by Reference:</E>
• For Civil Aviation Authority of Israel (CAAI) material identified in this proposed AD, contact CAAI, P.O. Box 1101, Golan Street, Airport City, 70100, Israel; telephone 972-3-9774665; fax 972-3-9774592; email
<E T="03">aip@mot.gov.il</E>
. You may find this material on the CAAI website at
<E T="03">gov.il/en/pages/israeli-airworthiness-directives</E>
. It is also available at
<E T="03">regulations.gov</E>
under Docket No. FAA-2025-2260.
• 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.
<FURINF>
<HD SOURCE="HED">FOR FURTHER INFORMATION CONTACT:</HD>
Trevor Carlton, Aviation Safety Engineer, FAA, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; phone: 404-474-5597; email:
<E T="03">trevor.p.carlton@faa.gov</E>
.
</FURINF>
<SUPLINF>
<HD SOURCE="HED">SUPPLEMENTARY INFORMATION:</HD>
<HD SOURCE="HD1">Comments Invited</HD>
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
<E T="02">ADDRESSES</E>
section. Include “Docket No. FAA-2025-2260; Project Identifier MCAI-2025-00043-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
<E T="03">regulations.gov,</E>
including any personal information you provide. The agency will also post a report summarizing each substantive verbal contact received about this NPRM.
<HD SOURCE="HD1">Confidential Business Information</HD>
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 Trevor Carlton, Aviation Safety Engineer, FAA, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; phone: 404-474-5597; email:
<E T="03">trevor.p.carlton@faa.gov</E>
. Any commentary that the FAA receives which is not specifically designated as CBI will be placed in the public docket for this rulemaking.
<HD SOURCE="HD1">Background</HD>
The CAAI, which is the aviation authority for Israel, has issued CAAI AD ISR I-32-25-01-7, dated January 13, 2025 (CAAI AD ISR I-32-25-01-7) (also referred to as the MCAI), to correct an unsafe condition for all Gulfstream Aerospace LP Model Gulfstream 100, Astra SPX, and 1125 Westwind Astra airplanes. The MCAI states an in-service failure of the nose landing gear (NLG) actuator-to-strut attachment pin was reported.
The FAA has determined that new airworthiness limitations are necessary for NLG actuator-to-strut attachment pins, part numbers (P/Ns) 2247.0500.007 and 2247.0500.008. The FAA is proposing this AD to prevent failure of the NLG actuator-to-strut attachment pin. The unsafe condition, if not addressed, could result in failure of the NLG to retract and lock after take-off or extend and lock before landing. You may examine the MCAI in the AD docket at
<E T="03">regulations.gov</E>
under Docket No. FAA-2025-2260.
<HD SOURCE="HD1">Material Incorporated by Reference Under 1 CFR Part 51</HD>
The FAA reviewed CAAI AD ISR I-32-25-01-7, which specifies new airworthiness limitations for safe life limits of the NLG actuator-to-strut attachment pins, P/Ns 2247.0500.007 and 2247.0500.008. 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
<E T="02">ADDRESSES</E>
section.
<HD SOURCE="HD1">FAA's Determination</HD>
These products have been approved by the civil aviation authority of another country and are approved for operation in the United States. Pursuant to the FAA's bilateral agreement with this State of Design Authority, that authority has notified the FAA of the unsafe condition described in the MCAI referenced above. The FAA is issuing this NPRM after determining that the unsafe condition described previously is likely to exist or develop in other products of the same type design.
<HD SOURCE="HD1">Proposed AD Requirements in This NPRM</HD>
This proposed AD would require revising the existing maintenance or inspection program, as applicable, to incorporate new airworthiness limitations, which are specified in CAAI AD ISR I-32-25-01-7 described previously, as incorporated by reference. Any differences with CAAI AD ISR I-32-25-01-7 are identified as exceptions in the regulatory text of this proposed AD.
This proposed AD would require revisions to certain operator maintenance documents to include new actions (
<E T="03">e.g.,</E>
inspections). Compliance with these actions 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 § 91.403(c), the operator must request approval for an alternative method of compliance (AMOC) according to paragraph (j)(1) of this proposed AD.
<HD SOURCE="HD1">Explanation of Required Compliance Information</HD>
In the FAA's ongoing efforts to improve the efficiency of the AD process, the FAA developed a process to use some civil aviation authority (CAA) ADs as the primary source of information for compliance with requirements for corresponding FAA ADs. The FAA has been coordinating this process with manufacturers and CAAs. As a result, the FAA proposes to incorporate CAAI AD ISR I-32-25-01-7 by reference in the FAA final rule. This proposed AD would, therefore, require compliance with CAAI AD ISR I-32-25-01-7 through that incorporation, except for any differences identified as exceptions in the regulatory text of this proposed AD. Material required by CAAI AD ISR I-32-25-01-7 for compliance will be available at
<E T="03">regulations.gov</E>
by searching for and locating Docket No. FAA-2025-2260 after the FAA final rule is published.
<HD SOURCE="HD1">Airworthiness Limitation ADs Using the New Process</HD>
The FAA's process of incorporating by reference MCAI ADs as the primary source of information for compliance with corresponding FAA ADs has been limited to certain MCAI ADs (primarily those with service bulletins as the primary source of information for accomplishing the actions required by the FAA AD). However, the FAA is now expanding the process to include MCAI ADs that require a change to airworthiness limitation documents, such as airworthiness limitation sections.
For these ADs that incorporate by reference an MCAI AD that changes airworth
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