AD 2007-06-13
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); and Model A310 Airplanes; Equipped With General Electric CF6-80A3 or CF6-80C2 Engines |
| engine | General Electric | CF6-80A3 or CF6-80C2 | 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); and Model A310 Airplanes; Equipped With General Electric CF6-80A3 or CF6-80C2 Engines |
Unsafe Condition
Thrust reverser could inadvertently deploy in flight under certain conditions, which could result in reduced controllability of the airplane.
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Required Actions
Install electro-pneumatic locking bar devices (TRAS lock systems) in the engine nacelles, install a dedicated and shielded electrical circuit segregated from the existing thrust reverser control system, and perform related investigative/corrective actions if necessary.
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Compliance Time
Before further flight
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Affected Aircraft
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); and Model A310 Airplanes, equipped with General Electric CF6-80A3 or CF6-80C2 engines.
AI-generated summary from the source AD text. Verify against the official source before acting.
Source: Official FAA Source ↗
Retrieved: Apr 4, 2026
Rights: U.S. Government Public Domain
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