AD 2001-16-03
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Boeing | 767-200 | Airworthiness Directives; Boeing Model 767-200, -300, -300F, and -400ER Series Airplanes Equipped with General Electric Model CF6-80C2 Series Engines |
| engine | General Electric | CF6-80C2 Series | Airworthiness Directives; Boeing Model 767-200, -300, -300F, and -400ER Series Airplanes Equipped with General Electric Model CF6-80C2 Series Engines |
Unsafe Condition
Failure of the flexshaft of the thrust reverser actuation system (TRAS) lock between the upper actuator and the TRAS lock, which could result in the loss of the fail-safe level of protection against in-flight thrust reverser deployment.
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Required Actions
Perform repetitive general visual inspections of the bullnose seal, repetitive tests of the electrical connector P3/P4 of the position switch modules, repetitive 'hot short' protection tests on the TRAS lock and directional pilot valve (DPV), and functional tests on both thrust reversers for the electro-mechanical brakes and CDU cone brakes. Replace components as necessary and ensure proper torque.
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Compliance Time
Before further flight following accomplishment of the applicable corrective action(s).
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Affected Aircraft
Boeing Model 767-200, -300, -300F, and -400ER series airplanes equipped with General Electric Model CF6-80C2 series engines.
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Source: Official FAA Source ↗
Retrieved: Apr 6, 2026
Rights: U.S. Government Public Domain
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