AD 2017-14-16
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Bombardier | Various | Airworthiness Directives; Bombardier, Inc., Airplanes |
Unsafe Condition
Improperly installed fasteners attaching the machined center fitting to the rear spar frame lower flange splice could cause premature failure of the fitting fasteners and cracking within the fitting or frame, resulting in reduced structural integrity of the wing-to-fuselage attachment.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Remove the fasteners attaching the machined center fitting to the rear spar frame lower flange splice, inspect the fasteners and fastener holes for damage, rework and repair the fastener holes as applicable, and replace the fasteners.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Before further flight
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Affected Aircraft
Bombardier, Inc., Model BD-100-1A10 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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