AD 2009-24-19
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A320 | Airworthiness Directives; Airbus Model A320 Series Airplanes |
| aircraft | Aviat | Various | Airworthiness Directives; Airbus Model A320 Series Airplanes |
Unsafe Condition
Excessive wear of the uplock segments against the inner cylinder of the Ejection Jack, due to an incorrect blend radius of the inner cylinder, which may prevent the effective deployment and use of the RAT in emergency conditions.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Replace the Ejection Jack that has been previously reworked in accordance with the incomplete Component Maintenance Manual (CMM) requirements. Identify the serial number of the installed ejection jack.
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Compliance Time
Within 12 months after the effective date of this AD.
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Affected Aircraft
Airbus Model A320-111, -211, -212, -214, -231, -232, and -233 series airplanes, certificated in any category, all certified models, all serial numbers, equipped with Hamilton Sundstrand (formerly Dowty) Ram Air Turbine (RAT) Ejection Jack, Model ERPS13EJ, part number (P/N) 114160004A or 114160005, except those airplanes on which Airbus modification 27189 was done in production or Airbus Service Bulletin A320-29-1100 was done in service, and on which Airbus modification 28413 was not done in production.
AI-generated summary from the source AD text. Verify against the official source before acting.
Source: Official FAA Source ↗
Retrieved: Apr 6, 2026
Rights: U.S. Government Public Domain
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