AD 2006-18-13

final rule
Data completeness: 70%

Airworthiness Directives; Gulfstream Model GV and GV-SP Series Airplanes

AD Number
2006-18-13
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2006-24951
FR Citation
71 FR 52990

Applicability

TypeManufacturerModelDetails
aircraft Gulfstream GV and GV-SP Airworthiness Directives; Gulfstream Model GV and GV-SP Series Airplanes

Unsafe Condition

The wiring harness outer shield and insulation on the primary conductors may have been inadvertently cut due to an improper method used to remove the wiring outer jacket, potentially leading to a short circuit in the wiring harness and loss of the hardover prevention system (HOPS) in the roll axis.

AI-generated summary from the source AD text. Verify against the official source before acting.

Required Actions

Repair the force link assembly wire harness within 12 months after the effective date by following the Accomplishment Instructions in the applicable service information. Inspect the environmental seal around the installed wires; if any nick or damage is found, repair it before further flight using an approved method.

AI-generated summary from the source AD text. Verify against the official source before acting.

Compliance Time

Within 12 months of the effective date

AI-generated summary from the source AD text. Verify against the official source before acting.

Affected Aircraft

Gulfstream Model GV series airplanes with serial numbers 674 through 693 inclusive, and GV-SP series airplanes with serial numbers 5001 through 5072 inclusive.

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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