AD Amdt-39-10458
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 repetitively to detect cracking on certain wing to fuselage frame-angles and repair if necessary.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Before further flight
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 6, 2026
Rights: U.S. Government Public Domain
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