AD 92-15-04
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Textron Aviation Inc. | BAe.125 Series 800A | BRITISH AEROSPACE Model 125-800A Series Airplanes |
| aircraft | Textron Aviation Inc. | BAe.125 Series 800A (C-29A) | BRITISH AEROSPACE Model 125-800A Series Airplanes |
| aircraft | Textron Aviation Inc. | BAe.125 Series 800A (U-125) | BRITISH AEROSPACE Model 125-800A Series Airplanes |
Unsafe Condition
Excessive wear and premature structural failure of the main landing gear.
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Required Actions
Install steel torque links on the right and left main landing gear, reduce torque link and knuckle axial clearances by installing British Aerospace Modification Number 253257A in accordance with SB.32-226-3257A dated May 3, 1991.
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Compliance Time
Within 180 days after the effective date of this AD
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Affected Aircraft
Model 125-800A series airplanes, certificated in any category.
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Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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