AD 92-26-05
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | BAE Systems (Operations) Limited | ATP | Airworthiness Directives; British Aerospace Model ATP Series Airplanes |
Unsafe Condition
Tightness or seizure of the nose wheel steering quadrant pivot and the upper steering control toggle link assembly could reduce controllability of the airplane.
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Required Actions
Perform a one-time functional inspection of the nose wheel steering quadrant pivot and upper steering control toggle link assembly within 30 days after the AD's effective date. If components are tight or seized, replace the bolt prior to further flight. If the upper toggle link is seized, repair the assembly, inspect support channels/structure for deformation or cracks, and repair or replace any damaged structure as per Service Bulletin ATP-32-37.
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Compliance Time
Within 30 days after the effective date of this AD
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Affected Aircraft
British Aerospace Model ATP series airplanes, serial numbers 2001 through 2044, inclusive; 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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