AD 2013-11-03
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Bombardier | Various | Airworthiness Directives; Bombardier, Inc. Airplanes |
Unsafe Condition
Cracking of the left-hand (LH) and right-hand (RH) wing lower skin, front and rear spar caps, front and rear spar webs, and reinforcing straps, which could lead to wing failure.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Conduct repetitive detailed inspections for cracking of the LH and RH wing lower skin, front and rear spar caps, front and rear spar webs, and reinforcing straps. Repair any cracking found during inspections. Terminate inspections with either a detailed inspection or an optional eddy-current inspection of the LH and RH wing lower front and rear spar caps, followed by repair if necessary.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 50 flight hours after the effective date of this AD.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Bombardier, Inc. Model CL-215-1A10 and CL-215-6B11 (CL-215T Variant) 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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