AD 2014-15-10

final rule
Data completeness: 80%

Airworthiness Directives; Dassault Aviation Airplanes

AD Number
2014-15-10
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2014-0177
FR Citation
79 FR 43616

Applicability

TypeManufacturerModelDetails
aircraft Dassault Aviation Airworthiness Directives; Dassault Aviation Airplanes
aircraft Aviat Various Airworthiness Directives; Dassault Aviation Airplanes

Unsafe Condition

Inversion of the wiring in the slats control manifold (SCM), which could lead to un-commanded retraction of the median and outboard slats in flight, resulting in reduced control of the airplane.

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

Required Actions

Perform an operational test of the SCM. Replace the affected SCM with a serviceable SCM if necessary.

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

Dassault Aviation Model FALCON 7X airplanes.

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

Source: Official FAA Source ↗

Retrieved: Apr 4, 2026

Rights: U.S. Government Public Domain

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