AD Amdt-39-10321
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 of the lower caps of the wing front spar and rear spar could result in reduced structural integrity of the airplane.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Perform repetitive ultrasonic inspections to detect cracking of the lower caps of the wing front spar and rear spar. Take corrective action 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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