AD 2017-13-02
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Dassault | Aviation | Airworthiness Directives; Dassault Aviation Airplanes |
| aircraft | Aviat | Various | Airworthiness Directives; Dassault Aviation Airplanes |
Unsafe Condition
Reports indicate that during the assembly of structural elements on some airplanes, lack of established procedures and tools caused boring and torqueing defects to be present at some locations on the foot of frame (FR) 36 and FR39.
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Required Actions
Remove sheer bolts at FR36 and FR39, left hand and right hand, and perform a detailed visual inspection of the bore holes for defects. Replace bolts and repair affected areas if defects are found, in accordance with Dassault Service Bulletin 7X-379.
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Compliance Time
Before exceeding 4,100 flight cycles after the specified date or within 3 months from the effective date of this AD, whichever occurs later.
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Affected Aircraft
Dassault Aviation Model FALCON 7X airplanes, certificated in any category, serial numbers 2, 5, and 8 through 182 inclusive, excluding S/Ns 141, 148, 149, 157, 159, 166, 170, 171, 174, 175, and 177 through 180 inclusive.
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Source: Official FAA Source ↗
Retrieved: Apr 4, 2026
Rights: U.S. Government Public Domain
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