AD 2011-01-13
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A300 B4-600 | Airworthiness Directives; Airbus Model A300 B4-600, B4-600R, and F4-600R Series Airplanes, and Model C4-605R Variant F Airplanes (Collectively Called A300-600 Series Airplanes) |
| aircraft | Aviat | Various | Airworthiness Directives; Airbus Model A300 B4-600, B4-600R, and F4-600R Series Airplanes, and Model C4-605R Variant F Airplanes (Collectively Called A300-600 Series Airplanes) |
Unsafe Condition
Pitch uncoupling unit installed at an incorrect location, inverted with the rod assembly.
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Required Actions
Perform a one-time visual inspection to detect incorrect installation of the pitch uncoupling unit. If found, remove and re-install the unit and rod assembly at the correct location, followed by a functional test to verify correct operation.
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Compliance Time
Before further flight
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Affected Aircraft
Airbus Model A300 B4-601, B4-603, B4-620, B4-622, B4-605R, B4-622R, F4-605R, F4-622R, and C4-605R Variant F airplanes, all serial numbers, except those where the pitch uncoupling functional test has already been performed in service since new.
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Source: Official FAA Source ↗
Retrieved: Apr 6, 2026
Rights: U.S. Government Public Domain
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