Airworthiness directives › 2026-01-02
AD 2026-01-02 Airworthiness Directives; Gulfstream Aerospace Corporation Airplanes
Models named: GVI. Read the applicability below — it usually turns on serial or part numbers too.
Applicability*9
This AD applies to all Gulfstream Aerospace Corporation Model GVI airplanes, certificated in any category.
Compliance
Comply with this AD within the compliance times specified, unless already done.
Required actions
Within 30 days after the effective date of this AD, revise the existing maintenance or inspection program, as applicable, to incorporate the information specified in Section 05-10-10, “Airworthiness Limitations,” Chapter 05, “Time Limits/Maintenance Checks,” Gulfstream G650 Aircraft Maintenance Manual, Revision 24, dated October 30, 2024; and Section 05-10-10, “Airworthiness Limitations,” Chapter 05, “Time Limits/Maintenance Checks,” Gulfstream G650ER Aircraft Maintenance Manual, Revision 19, dated October 30, 2024; as applicable. The initial compliance time for doing the tasks is at the time specified in Section 05-10-10, “Airworthiness Limitations,” Chapter 05, “Time Limits/Maintenance Checks,” Gulfstream G650 Aircraft Maintenance Manual, Revision 24, dated October 30, 2024; and Section 05-10-10, “Airworthiness Limitations,” Chapter 05, “Time Limits/Maintenance Checks,” Gulfstream G650ER Aircraft Maintenance Manual, Revision 19, dated October 30, 2024; as applicable, or within 30 days after the effective date of this AD, whichever occurs later. Using a later revision of Section 05-10-10 of the applicable AMM with information identical to that contained in Section 05-10-10, “Airworthiness Limitations,” Chapter 05, “Time Limits/Maintenance Checks,” Gulfstream G650 Aircraft Maintenance Manual, Revision 24, dated October 30, 2024; and Section 05-10-10, “Airworthiness Limitations,” Chapter 05, “Time Limits/Maintenance Checks,” Gulfstream G650ER Aircraft Maintenance Manual, Revision 19, dated October 30, 2024; as applicable, is acceptable for compliance with the requirements of this paragraph.
Unsafe condition
This AD was prompted by a determination that new and more restrictive airworthiness limitations are necessary. The FAA is issuing this AD to prevent failure of principal structural elements throughout the service life of each part. This condition, if not addressed, could compromise the structural integrity of the airplane.
Affected ADs
None.
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The directive text above is reproduced from the Federal Register, a work of the United States government and in the public domain. The separation into applicability, compliance and required actions is TrackAD's.*1