AD 2001-22-02
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A300 B2 and B4 | Airworthiness Directives; Airbus Model A300 B2 and B4 Series Airplanes |
Unsafe Condition
Failure of both spring boxes of the variable lever arm (VLA) due to corrosion damage, which could result in loss of rudder control and consequent reduced controllability of the airplane.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Determine the part and amendment numbers of the VLA of the rudder control system to verify the parts were installed using the correct standard. If necessary, perform a detailed visual inspection of the VLA tie rod for damage (bent or ruptured rod) and replace any damaged tie rod with a new one.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 50 flight hours after the effective date of the AD.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Airbus Model A300 B2 and B4 series airplanes, certificated in any category.
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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