AD 2024-10-15
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Gulfstream | Aerospace Corporation | Airworthiness Directives; Gulfstream Aerospace Corporation Airplanes |
Unsafe Condition
A partially disengaged rear engine mount was discovered on an in-service Model GVII-G600 airplane due to the upper, aft engine mount fastener migrating out of position in the pylon area. The cause of the upper rear engine mount failure was determined to be the secondary locking device (cotter pin) not being installed, and the separation of the retaining nut from the single strut attachment bolt, resulting in the bolt migrating out of position.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspecting the left and right engine mount points within the pylons and engine nacelles for non-conforming hardware installation, repairing the engine mount points if necessary, and revising the existing aircraft maintenance manual (AMM) to include revised procedures for engine removal and installation.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Before further flight
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Gulfstream Aerospace Corporation Model GVII-G500 and GVII-G600 airplanes.
AI-generated summary from the source AD text. Verify against the official source before acting.
Source: Official FAA Source ↗
Retrieved: Apr 6, 2026
Rights: U.S. Government Public Domain
This site is not affiliated with or endorsed by the FAA. Always verify with official sources.