AD 2001-22-13
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Boeing | 737-100 | Airworthiness Directives; Boeing Model 737-100, -200, -300, -400, and -500 Series Airplanes; and Model 747, 757, 767, and 777 Series Airplanes |
Unsafe Condition
Improperly torqued fasteners that connect the rudder pedal pushrod to the rudder pedal assembly could result in loss of rudder control and loss of controllability of the airplane.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Replace the rudder pedal pushrod fasteners for both the captain's and first officer's pedal assemblies with new, improved fasteners that use self-locking, castellated nuts and cotter pins through the bolts for nut retention.
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Compliance Time
Within 18 months of the effective date (December 6, 2001).
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Affected Aircraft
Boeing Model 737-100, -200, -300, -400, and -500 series airplanes; and Boeing Model 747, 757, 767, and 777 series airplanes.
AI-generated summary from the source AD text. Verify against the official source before acting.
Source: Official FAA Source ↗
Retrieved: Apr 6, 2026
Rights: U.S. Government Public Domain
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