AD 2012-11-06
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Gulfstream | Aerospace Corporation | Airworthiness Directives; Gulfstream Aerospace Corporation Airplanes |
Unsafe Condition
Excessive gaps in the wing-to-fuselage attachment fittings, resulting from an improper structural modification, which could lead to reduced structural integrity and potential wing separation.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Measure the clearance (gap) of the exposed rounded portion of the doubler and clothespin fitting at the wing-to-fuselage attachment. Repair if necessary. Determine if a certain aircraft service change has been incorporated. For affected airplanes, measure the clearance (gap) of the exposed rounded portion of the doubler and clothespin fitting at the wing-to-fuselage attachment and repair if necessary. Send measurement results to Gulfstream.
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 G-1159, G-1159A, and G-1159B 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
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