AD 2006-03-10
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A318-100 and A319-100 | Airworthiness Directives; Airbus Model A318-100 and A319-100 Series Airplanes; A320-111 Airplanes; A320-200 Series Airplanes; and A321-100 and A321-200 Series Airplanes |
Unsafe Condition
Electrical wire damage was found in the 103VU electrical panel due to contact between the hinge pin and the adjacent electrical wire harness.
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Required Actions
Within 600 flight hours after the effective date, perform a general visual inspection of the horizontal hinge pin of the 103VU electrical panel in the avionics compartment to determine if the pin can move out of the hinge. Perform any applicable investigative and corrective actions, including repairing damaged electrical wires, before further flight.
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Compliance Time
Within 600 flight hours after the effective date of this AD.
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Affected Aircraft
Airbus Model A318-111 and -112; A319-111, -112, -113, -114, -115, -131, -132, and -133; A320-111, -211, -212, -214, -231, -232, and -233; and A321-111, -112, -131, -211, and -231 airplanes, certificated in any category, with serial numbers 1 through 2396 inclusive, except S/Ns 2104, 2143, 2248, 2270, 2347, 2366, 2372, 2376, 2384, 2386, 2388, 2390, 2391, 2393, and 2395.
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Source: Official FAA Source ↗
Retrieved: Apr 4, 2026
Rights: U.S. Government Public Domain
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