AD 83-24-06
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Bombardier Inc. | CL-44D4 | Airworthiness Directives; CANADAIR Model CL-44D4 and CL-44J Airplanes |
| aircraft | Bombardier Inc. | CL-44J | Airworthiness Directives; CANADAIR Model CL-44D4 and CL-44J Airplanes |
Unsafe Condition
Cracks in the upper main landing gear actuator eye attachment pins, part number 44-87815, could result in structural failure.
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Required Actions
Inspect both left and right upper main landing gear actuator eye attachment pins for cracks per Canadair SIC No. 441-CL44. Replace cracked parts with new or serviceable parts of the same part number before further flight. Alternate compliance may be approved by the FAA Manager, Seattle Aircraft Certification Office.
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Compliance Time
Within the next 100 hours time in service or 25 landings, whichever occurs first, after the effective date of this AD, unless accomplished within the last 1100 hours time in service or 275 landings, and thereafter at intervals not to exceed 1200 hours time in service or 300 landings, whichever occurs first.
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Affected Aircraft
Bombardier Inc. Model CL-44D4 and CL-44J airplanes certificated in all categories.
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Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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