AD 2014-16-08
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Bombardier | Various | Airworthiness Directives; Bombardier, Inc. Airplanes |
Unsafe Condition
Shorter nacelle strut bushings (P/N 85410265-105) were inadvertently installed instead of the correct bushings (P/N 85410265-103), providing insufficient engagement in the strut fork end (P/N 215T16534-12/-13), which may deform under bearing load and lead to joint failure.
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Required Actions
Inspect the left and right nacelle upper strut bushings; install bolts and preload indicating (PLI) washers if necessary; replace the bushing or repair the bushing installation if necessary.
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 CL-215-6B11 (CL-215T Variant) and CL-215-6B11 (CL-415 Variant) airplanes.
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Source: Official FAA Source ↗
Retrieved: Apr 4, 2026
Rights: U.S. Government Public Domain
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