AD 2008-24-14
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Bombardier | Various | Airworthiness Directives; Bombardier Model CL-600-2B19 (Regional Jet Series 100 & 440) Airplanes |
| aircraft | Aviat | Various | Airworthiness Directives; Bombardier Model CL-600-2B19 (Regional Jet Series 100 & 440) Airplanes |
Unsafe Condition
Cracks on the main landing gear trunnion fitting web have been discovered during fatigue testing. Failure of the main landing gear trunnion fitting web could compromise the structural integrity of the trunnion fitting and result in a main landing gear collapse.
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Required Actions
Revise the Airworthiness Limitations Section of the Instructions for Continued Airworthiness to incorporate new structural inspection requirements. Compliance with these inspections is required by 14 CFR 91.403(c).
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Compliance Time
Within 50 flight hours after the effective date of this AD.
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Affected Aircraft
All Bombardier Model CL-600-2B19 (Regional Jet Series 100 & 440) airplanes, certificated in any category.
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Source: Official FAA Source ↗
Retrieved: Apr 4, 2026
Rights: U.S. Government Public Domain
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