AD 2012-26-51

final rule
Data completeness: 70%

Airworthiness Directives; Airbus Airplanes

AD Number
2012-26-51
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2012-1314
FR Citation
78 FR 1723

Applicability

TypeManufacturerModelDetails
aircraft Airbus A318 Airworthiness Directives; Airbus Airplanes

Unsafe Condition

Blockage of Angle of Attack (AoA) sensors installed with conic plates during climb, leading to autopilot disconnection and activation of alpha protection (Alpha Prot) when Mach number is increased, which could result in reduced control of the airplane.

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Required Actions

Revise the Emergency Procedures section of the AFM to incorporate Airbus Temporary Revision TR286, Issue 1.0, dated December 17, 2012, to advise flight crews of emergency procedures for addressing AoA sensor blockage. Optional terminating action involves replacing AoA sensor conic plates with flat plates.

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Compliance Time

Within 50 flight hours after the effective date of this AD.

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Affected Aircraft

All 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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