EASA AD 2019-0144: Aircraft Flight Manual — Amendment ; Ice and Rain Protection — Total Air Temperature Probe Heater / Electrical Circuit — Modification | RegNotify

OtherEASA AD 2019-0144

Aircraft Flight Manual — Amendment ; Ice and Rain Protection — Total Air Temperature Probe Heater / Electrical Circuit — Modification

Published: Jun 19, 2019
Effective: Jul 3, 2019

Piaggio P180

AI-generated summary of the official EASA document. Verify against the PDF before acting.

What to do

Affected operators and maintenance organizations should update their Aircraft Flight Manuals to incorporate the amendment. They must also ensure that maintenance practices and operational procedures reflect the modified total air temperature probe heater electrical circuit. Compliance deadlines are not specified in the document.

Summary

The document titled 'Aircraft Flight Manual — Amendment ; Ice and Rain Protection — Total Air Temperature Probe Heater / Electrical Circuit — Modification' applies specifically to the Piaggio P180 aircraft. It details an amendment to the Aircraft Flight Manual concerning modifications to the ice and rain protection system, focusing on the total air temperature probe heater and its electrical circuit.

What changed

This amendment introduces modifications to the electrical circuit of the total air temperature probe heater on the Piaggio P180. It updates the Aircraft Flight Manual to reflect these changes, ensuring that the procedures and system descriptions align with the new configuration.

Why it matters

These changes are important for aviation professionals because they affect the operation and maintenance of the ice and rain protection system on the Piaggio P180. Operators and maintenance teams must understand the updated procedures to ensure continued safe and compliant aircraft operation, particularly in icing conditions.

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