AD 2002-12-12
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Bombardier | CL-215-1A10 and CL-215-6B11 | Airworthiness Directives; Bombardier Model CL-215-1A10 and CL-215-6B11 Series Airplanes |
Unsafe Condition
Cracking on certain wing-to-fuselage frame angles could result in reduced structural integrity of the airframe.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect for cracking on certain wing-to-fuselage frame angles. Repair, if necessary. Decrease the compliance time for the initial inspection and the interval between repetitive inspections.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within the revised compliance times specified in the AD.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Bombardier Model CL-215-1A10 and CL-215-6B11 series 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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