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Published 2008-08-11 · Federal Register document E8-18227

Airworthiness Directives; Eclipse Aviation Corporation Model EA500 Airplanes

Publication summary

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.

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Source: Federal Register annual FAA metadata. Acquired 2026-09-03T22:23:26.953736+00:00. The title, summary and date are source facts.

Source revision
federal_register_ad_metadata_2008-e9cf118935fdae82
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results[325]
Raw source SHA-256
e9cf118935fdae82a000e2c01764c770bd79679c1dd4c2b00fdcd3b030f92fe5

Correction notice · separate source edition

Recorded publication clauses

AD identifier printed in this edition
2008-02-04
Effective date printed in this edition
Unknown

This correction is a separate source edition; it is not counted as a new adopted rule.

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Find all recorded historical references to AD 2008-02-04 · 0 printed reference observations in this pinned collection.

These are observations from one dated publication. Current legal status is unknown; aircraft applicability, installed configuration, compliance and burden require separate evidence. Missing or unparsed conditions remain unknown.

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They were extracted offline from the same immutable official HTML source as the complete recorded text. The dated source wording, original text coordinates and exact quote digests are retained. PDF/text agreement and current regulatory effect have not been qualified.

Observation revision: whole-ad-publication-clause-observations-1.0.1. Text SHA-256: 4b15b85760af7463c95bf696827130d7d1f2c74b171db969ef9851701b75bc75. Source manifest: be7b89c4aeb3fa4b2c2646b8882489b39119f412f17ca020b6aebd0570b8ef46.

Official source · 2008-08-11

Publication text

This is the complete recorded text of this dated publication.

Current legal effect is unknown. Aircraft applicability, installed configuration and compliance require separate evidence. PDF/text agreement has not been evaluated.

Read the complete official publication text
[Federal Register Volume 73, Number 155 (Monday, August 11, 2008)]
[Rules and Regulations]
[Page 46542]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: E8-18227]


-----------------------------------------------------------------------

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2007-29316; Directorate Identifier 2007-CE-078-AD; 
Amendment 39-15334; AD 2008-02-04]
RIN 2120-AA64


Airworthiness Directives; Eclipse Aviation Corporation Model 
EA500 Airplanes

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Final rule; correction.

-----------------------------------------------------------------------

SUMMARY: 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.

DATES: The effective date of this AD remains February 26, 2008, since 
the incorrect reference of the issue date of AD 2008-02-04 does not 
affect compliance.

FOR FURTHER INFORMATION CONTACT: Al Wilson, Flight Test Pilot, Airplane 
Certification Office, FAA, 2601 Meacham Blvd., Fort Worth, Texas 76137-
4298; telephone: (817) 222-5146; fax: (817) 222-5960.

SUPPLEMENTARY INFORMATION:

Discussion

    AD 2008-02-04, Amendment 39-15334 (73 FR 3618, January 22, 2008), 
affects Eclipse Model EA500 airplanes and currently:
    <bullet> Requires incorporating a modification of the angle of 
attack (AOA) probe;
    <bullet> Limits the applicability to airplanes under S/N 000065; 
and
    <bullet> Retains the operating limitations from AD 2007-13-11 until 
the modification is incorporated.

The FAA incorrectly referenced the issue date as ``January 9, 2007'' 
instead of ``January 9, 2008.'' This document corrects the issue date.

Need for the Correction

    This correction is needed to reflect the correct issue date on the 
AD.

Correction of Publication

    Accordingly, the publication of January 22, 2008 (73 FR 3618), 
which was the subject of FR Doc. E8-751, is corrected as follows:

Section 39.13 [Corrected]

    On page 3619, in the third column, in the sixth and seventh lines 
from the bottom, under the heading Sec.  39.13 [Amended], replace 
``January 9, 2007'' with ``January 9, 2008.''
    Action is taken herein to correct this reference in the AD.
    The effective date of this AD remains February 26, 2008, since the 
incorrect reference of the issue date of AD 2008-02-04 does not affect 
compliance.

    Issued in Kansas City, Missouri, on August 1, 2008.
James E. Jackson,
Acting Manager, Small Airplane Directorate, Aircraft Certification 
Service.
 [FR Doc. E8-18227 Filed 8-8-08; 8:45 am]
BILLING CODE 4910-13-P


Why this text is shown

The complete text was extracted from the official GovInfo HTML edition for this publication. Acquired 2026-10-09T03:28:37.638539+00:00. Text extraction preserves the recorded source wording; it does not determine current requirements.

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Source SHA-256
878b96c3337edaa7afd75ce6c55f2d2d50e6a23f6b4aea8691a402723b68906a
Text SHA-256
4b15b85760af7463c95bf696827130d7d1f2c74b171db969ef9851701b75bc75

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These are dated publication metadata, recorded clauses and literal source observations. Word, model-label, header and reference matches do not establish current legal effect, manufacturer/model identity, aircraft applicability, installed configuration or compliance.

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