AD 95-10-12
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus SAS | A320-111 | Airworthiness Directives; Airbus Model A320-111, -211, and -212 Series Airplanes |
| aircraft | Airbus SAS | A320-211 | Airworthiness Directives; Airbus Model A320-111, -211, and -212 Series Airplanes |
| aircraft | Airbus SAS | A320-212 | Airworthiness Directives; Airbus Model A320-111, -211, and -212 Series Airplanes |
Unsafe Condition
Traces of fungus and corrosion on the electrical harness junction box and connector backshells of the thrust reverser could result in multiple faults in the thrust reverser position indication and subsequent uncontrolled reduction of engine power.
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Required Actions
Modify the junction box, connector backshells, and electrical harness assembly of the thrust reverser in accordance with Airbus Service Bulletin A320-71-1011 or Revision 1. Alternative methods of compliance may be approved by the FAA.
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Compliance Time
Within 3,000 flight hours after the effective date of this AD (June 21, 1995).
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Affected Aircraft
Airbus Model A320-111, -211, and -212 series airplanes powered by CFM 56-5A engines with electrical harness assembly part number 238W0908-513 and without Airbus Modification 23693 installed.
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Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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