FAA Proposes AD for Pilatus PC-12/47E Stall Warning System
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The FAA has proposed an airworthiness directive for the Pilatus PC-12/47E to fix a stall protection system flaw previously identified by EASA.
Key Takeaways
- •Proposes a mandatory software update for the Pilatus PC-12/47E Stall Warning Protection System.
- •Addresses a flaw causing premature stick pusher activation during low-g maneuvers near landing.
- •Follows an original airworthiness directive issued by EASA on December 2, 2025.
- •Sets a public comment deadline for May 4, 2026, before finalizing the safety rule.
The Federal Aviation Administration (FAA) has issued a Notice of Proposed Rulemaking (NPRM) for an Airworthiness Directive (AD) targeting certain Pilatus Aircraft Ltd. Model PC-12/47E airplanes. The proposed rule addresses an unsafe condition within the aircraft's Stall Warning Protection System (SWPS), which could lead to an unintended activation of the stick pusher during critical phases of flight. This action follows a prior mandate from the European Union Aviation Safety Agency (EASA).
The core safety issue involves the potential for the SWPS to activate at a higher-than-expected airspeed. According to the FAA's docket, this anomaly was observed during maneuvers close to 0 g, specifically during a landing approach with flaps set to 40 degrees. In such a scenario, an uncommanded stick pusher activation could result in a sudden pitch-down moment at low altitude, potentially leading to loss of control. The directive aims to mitigate this risk by mandating a software update and a revision to the aircraft's flight manual.
Regulatory Background and Required Actions
The FAA's proposed directive, published in the Federal Register under Docket No. FAA-2026-2715 on March 19, 2026, was prompted by what the agency terms Mandatory Continuing Airworthiness Information (MCAI) from a foreign authority. The originating directive, EASA AD 2025-0271, was issued on December 2, 2025, after the unsafe condition was first identified.
To correct the issue, the FAA proposes requiring two specific actions for operators of the affected aircraft:
- Software Update: An update to the Honeywell Primus Apex Operational Software to Build 12.7.2. This new build contains revised logic to prevent the erroneous SWPS activation under the identified flight conditions.
- Manual Revision: The incorporation of Temporary Revision No. 32 into the Pilot's Operating Handbook (POH), which provides flight crews with updated information and procedures related to the SWPS.
The impact on operators primarily involves minor maintenance downtime to perform the software installation. For Pilatus Aircraft Ltd., the manufacturer, and Honeywell Aerospace, the avionics provider, the impact includes the administrative and support costs associated with distributing the fix across the affected fleet.
Technical Analysis and Industry Context
This proposed AD for the Pilatus PC-12/47E aligns with a broader industry trend of increased regulatory focus on automated flight control systems. In recent years, aviation authorities have issued multiple directives to address anomalies in stall protection systems across various aircraft types, reflecting the growing complexity of modern avionics and their interaction with aerodynamic envelopes.
Historical precedents illustrate a pattern of addressing similar system vulnerabilities. In April 2019, an emergency AD was issued for the Cirrus SF50 after its SWPS engaged inappropriately, mandating an Angle of Attack (AOA) sensor replacement. Similarly, an AD for the ATR 42/72 in September 2024 addressed false stick pusher activations caused by faulty AOA data. These events highlight the critical role of sensor inputs and software logic in ensuring automated safety systems behave predictably.
The reliance on a software update as the primary solution for the PC-12/47E is also indicative of modern aircraft design. As aircraft become more dependent on integrated avionics suites like the Honeywell Primus Apex, software revisions are increasingly the standard method for resolving safety-critical issues, offering a more efficient path to remediation than extensive hardware modifications.
What Comes Next
The FAA has established a public comment period for the proposed rule, which is set to close on May 4, 2026. During this time, owners, operators, and other stakeholders can submit feedback on the directive's content and its estimated economic impact. Following the comment period, the agency will review the input before publishing a final rule.
Based on standard regulatory timelines, the final Airworthiness Directive is expected to be issued in the third quarter of 2026. Once finalized, compliance will become mandatory for all U.S.-registered Pilatus PC-12/47E aircraft specified in the directive.
Why This Matters
This action underscores the importance of international regulatory cooperation, with the FAA leveraging safety data from EASA to ensure a harmonized approach to a known risk. For the business and general aviation sectors, it reinforces the critical need for vigilance over automated systems, whose failure modes can present unique challenges. Ultimately, the directive reflects the proactive stance regulators are taking to ensure that software-driven safety nets in modern aircraft function as intended throughout all flight regimes.
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Written by Hardik Vishwakarma
Co-Founder & Aviation News Editor leading initiatives that improve trust and visibility across the global aviation industry. Covers airlines, airports, safety, and emerging technology.
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