AD 2015-07-02
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Bombardier | Various | Airworthiness Directives; Bombardier, Inc. Airplanes |
Unsafe Condition
The forward lugs of the flap hinge box may not conform to engineering drawings, which could result in premature fatigue cracking.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Revise the maintenance or inspection program to include new airworthiness limitations tasks. Measure the forward lug edge distance of each flap hinge box, inspect for cracking and damage (i.e., deformation or bearing failure) of the forward lug edge, and repair any cracking or damage if necessary.
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Compliance Time
Before further flight
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Affected Aircraft
Bombardier, Inc. Model CL-600-1A11 (CL-600), CL-600-2A12 (CL-601), and CL-600-2B16 (CL-601-3A, CL-601-3R, and CL-604 Variants) airplanes.
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Source: Official FAA Source ↗
Retrieved: Apr 6, 2026
Rights: U.S. Government Public Domain
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