AD 2024-03-04
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Boeing | Company | Airworthiness Directives; The Boeing Company Airplanes |
Unsafe Condition
A disconnect between the aft rudder quadrant and the output rod would result in loss of rudder control via the rudder pedals and insufficient rudder control to counter an engine-out scenario during takeoff/climb out or to counter a high crosswind during landing, which could result in the loss of continued safe flight and landing.
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Required Actions
Perform a one-time detailed visual inspection or remote video inspection of the aft rudder quadrant for any missing bolt, nut, or washer; any gap between the bolt/nut/washer and quadrant; and insufficient thread protrusion. If necessary, inspect the bolt and nut for damage and replacement as needed; torque application; and a rudder travel test.
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Compliance Time
Within 30 days
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Affected Aircraft
The Boeing Company Model 737-8, 737-8200, and 737-9 airplanes.
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Source: Official FAA Source ↗
Retrieved: Apr 4, 2026
Rights: U.S. Government Public Domain
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