AD 2003-14-10
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Boeing | 767-200 and -300 | Airworthiness Directives; Boeing Model 767-200 and -300 Series Airplanes |
Unsafe Condition
Chafing of the wire bundles of the video control center (VCC) against the rudder and/or elevator control cables, which could result in arcing of the wires in the wire bundles and severing of the cables. Severed cables, if combined with an engine-out during takeoff, or a high crosswind during takeoff or landing, could result in reduced controllability of the airplane.
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Required Actions
Modify the wire bundles of the VCC of the passenger address and entertainment system by installing a wiring shroud and associated hardware, re-routing the VCC wire bundles above the flight control pulley box, and replacing existing clamps with new clamps, as applicable. An operational test may be required after the modification.
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Compliance Time
Within 6 months of the effective date
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Affected Aircraft
Boeing Model 767-200 and -300 series airplanes, as specified in the service bulletins 767-23A0147, 767-23A0154, 767-23A0155, 767-23A0156, and 767-23A0157.
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Source: Official FAA Source ↗
Retrieved: Apr 6, 2026
Rights: U.S. Government Public Domain
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