AD 2016-13-15
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Dassault | Aviation | Airworthiness Directives; Dassault Aviation Airplanes |
| aircraft | Aviat | Various | Airworthiness Directives; Dassault Aviation Airplanes |
Unsafe Condition
Improperly drilled bores located on upper and lower stiffener joints to the web at a certain frame, with defects such as ovalization, excessive depth, and irregular surface qualities, which can adversely affect the structural integrity of the airplane.
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Required Actions
Inspect the bores for surface defects greater than or equal to 0.5 mm or chamfer dimensions/edge distances not within specified limits. Repair affected stiffener bores if necessary.
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Compliance Time
Within 4,000 flight cycles or 98 months, whichever occurs first, since the date of issuance of the original airworthiness certificate or date of issuance of the original export certificate of airworthiness.
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Affected Aircraft
Dassault Aviation Model FALCON 7X airplanes, manufacturer serial numbers 1 through 221 inclusive, except serial numbers 182 and 220.
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Source: Official FAA Source ↗
Retrieved: Apr 6, 2026
Rights: U.S. Government Public Domain
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