AD 2011-19-01
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A318 | Airworthiness Directives; Airbus Model A318, A319, A320, and A321 Series Airplanes |
| aircraft | Aviat | Various | Airworthiness Directives; Airbus Model A318, A319, A320, and A321 Series Airplanes |
Unsafe Condition
Pin to socket arcing at the Integrated Drive Generator (IDG) feeder cable pylon/nacelle interface connector, caused by fretting corrosion and a non-optimized electrical harness installation, leading to electrical arcs and possible flickering of display units.
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Required Actions
Amend the applicable Airplane Flight Manual (AFM) to include a new 'DISPLAY UNIT FAILURE' procedure, allowing flight crew to determine the affected generator, select it OFF, and reset the rudder trim.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Before further flight
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Affected Aircraft
Airbus Model A318, A319, A320, and A321 series airplanes.
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Source: Official FAA Source ↗
Retrieved: Apr 6, 2026
Rights: U.S. Government Public Domain
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