AD 2005-13-33
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A300 B2 and B4 | Airworthiness Directives; Airbus Model A300 B2 and B4 Series Airplanes |
Unsafe Condition
Reports of pitch trim disconnect caused by insufficient length in the wiring to the pitch torque limiter lever.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Modify the wiring of the autopilot pitch torque limiter switch by performing all applicable actions specified in Airbus Service Bulletin A300-22-0117.
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Compliance Time
Within 20 months after the effective date of this AD.
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Affected Aircraft
Airbus Model A300 B2-1A, B2-1C, B2K-3C, B2-203, B4-2C, B4-103, and B4-203 airplanes, certificated in any category, as identified in Airbus Service Bulletin A300-22-0117.
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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