AD 2019-16-06
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | SAS | Airworthiness Directives; Airbus SAS Airplanes |
| aircraft | Aviat | Various | Airworthiness Directives; Airbus SAS Airplanes |
Unsafe Condition
Analysis and laboratory testing of the behavior of the flight control laws of the A320neo identified a reduced efficiency of the angle of attack protection when the aeroplane is set in certain flight configurations and in combination with specific manoeuvres commanded by the flight crew, which could lead to excessive pitch attitude, possibly resulting in increased flight crew workload.
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Required Actions
Revising the existing airplane flight manual (AFM) to incorporate operational limitations and updated procedures related to center of gravity, as specified in EASA AD 2019-0189.
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Compliance Time
Before further flight
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Affected Aircraft
All Airbus SAS Model A320-251N and A320-271N airplanes.
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Source: Official FAA Source ↗
Retrieved: Apr 4, 2026
Rights: U.S. Government Public Domain
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