Airworthiness Directive E8-18227

one-time
AD E8-18227 · 2008-08-11 · airframe

Airworthiness Directives; Eclipse Aviation Corporation Model EA500 Airplanes

What this AD requires

This document makes a correction to Airworthiness Directive (AD) 2008-02-04, which was published in the Federal Register on January 22, 2008 (73 FR 3618), and applies to all Eclipse Aviation Corporation (Eclipse) Model EA500 airplanes. This AD requires incorporating a modification of the angle of attack (AOA) system, limits the applicability to airplanes under S/N 000065, and retains the operating limitations from AD 2007-13-11 until the modification is incorporated. The FAA incorrectly referenced the issue date of the AD as "January 9, 2007" instead of "January 9, 2008." This document corrects the issue date.

Which aircraft AD E8-18227 applies to

MakesEclipse Aviation Corporation
ModelsEA500

incorporating

Whether AD E8-18227 actually applies to your aircraft (by serial and installed parts) and whether it’s already complied with comes from that aircraft’s records.

How AD compliance is recorded

A valid compliance record (14 CFR 43.9) states:

Method of complianceThe specific action taken (inspected, replaced, modified) and to what revision.
DateWhen the work was done.
Aircraft timeTotal time in service / tach at compliance — how recurring next-due is computed.
Signature & certificateThe A&P/IA who returned it to service, with certificate number.
Is AD E8-18227 complied with on your aircraft?

Tailplate reads a tail number’s logbooks and matches every applicable AD — including this one — to its compliance evidence, with recurring next-due dates computed.

Look up a tail number →Read the full directive (Federal Register)

Applicability is derived from the FAA directive corpus and is advisory, not a legal airworthiness determination. Compliance is established only from an aircraft’s actual records.