AD 2003-18-11
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Gulfstream | G-V | Airworthiness Directives; Gulfstream Model G-V Series Airplanes |
Unsafe Condition
Separation of the balance weights of the aileron, which could result in jamming of the pilot's aileron control system, subsequent loss of aileron control, and consequent reduced controllability of the airplane.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Within the next 50 landings or 90 days after the effective date of this AD, whichever is first, perform a one-time general visual inspection of the balance weight installation of the left and right ailerons for correctly installed attachment components. If necessary, take corrective actions including ensuring proper engagement of the self-locking nut, replacing any missing fasteners, and re-torqueing any loose fasteners. Any applicable corrective actions must be completed before further flight.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 50 landings or 90 days after the effective date of this AD, whichever is first.
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Affected Aircraft
Gulfstream Model G-V series airplanes, serial numbers 501 through 667 inclusive, and serial number 699; certificated in any category.
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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