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Published 2006-01-04 · Federal Register document 06-16

Airworthiness Directives; Empresa Brasileira de Aeronautica S.A. (EMBRAER) Model EMB-135 Airplanes and Model EMB-145, -145ER, -145MR, -145LR, -145XR, -145MP, and -145EP Airplanes

Publication summary

The FAA is correcting a typographical error in an existing airworthiness directive (AD) that was published in the Federal Register on December 5, 2005 (70 FR 72363). The error resulted in an incorrect reference to the effective date of Brazilian airworthiness directive 2003-01-03R1. This AD applies to certain EMBRAER Model EMB-135 and Model EMB-145 series airplanes. This AD is superseding an existing AD that currently requires repetitive inspections of the spring cartridges of the elevator gust lock system to determine if the lock washer projection correctly fits the slots in the cartridge flange, and corrective action if necessary, for certain airplanes. This AD retains the requirements of the existing AD and adds a requirement for final terminating action for all affected airplanes.

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Source: Federal Register annual FAA metadata. Acquired 2026-09-03T22:23:20.745856+00:00. The title, summary and date are source facts.

Source revision
federal_register_ad_metadata_2006-8d787f8b35bc8016
Source row
results[0]
Raw source SHA-256
8d787f8b35bc80165a417cea66de09cd32a1700face13759db364c607e405963

Correction notice · separate source edition

Recorded publication clauses

AD identifier printed in this edition
2005-24-11
Effective date printed in this edition
Unknown

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Find all recorded historical references to AD 2005-24-11 · 0 printed reference observations in this pinned collection.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: f6bc42a12edd782844e979367ad9109bca39f276b16309e9e27caf8e3c1435aa. Source manifest: 613a5172aa4dbf538e0cbddf4a89b264125ef7c032b3e6a6c2136c3b222b230b.

Official source · 2006-01-04

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 71, Number 2 (Wednesday, January 4, 2006)]
[Rules and Regulations]
[Page 231]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 06-16]



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Rules and Regulations
                                                Federal Register
________________________________________________________________________

This section of the FEDERAL REGISTER contains regulatory documents 
having general applicability and legal effect, most of which are keyed 
to and codified in the Code of Federal Regulations, which is published 
under 50 titles pursuant to 44 U.S.C. 1510.

The Code of Federal Regulations is sold by the Superintendent of Documents. 
Prices of new books are listed in the first FEDERAL REGISTER issue of each 
week.

========================================================================


Federal Register / Vol. 71, No. 2 / Wednesday, January 4, 2006 / 
Rules and Regulations

[[Page 231]]



DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2005-22033; Directorate Identifier 2004-NM-218-AD; 
Amendment 39-14391; AD 2005-24-11]
RIN 2120-AA64


Airworthiness Directives; Empresa Brasileira de Aeronautica S.A. 
(EMBRAER) Model EMB-135 Airplanes and Model EMB-145, -145ER, -145MR, -
145LR, -145XR, -145MP, and -145EP Airplanes

AGENCY: Federal Aviation Administration (FAA), Department of 
Transportation (DOT).

ACTION: Final rule; correction.

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

SUMMARY: The FAA is correcting a typographical error in an existing 
airworthiness directive (AD) that was published in the Federal Register 
on December 5, 2005 (70 FR 72363). The error resulted in an incorrect 
reference to the effective date of Brazilian airworthiness directive 
2003-01-03R1. This AD applies to certain EMBRAER Model EMB-135 and 
Model EMB-145 series airplanes. This AD is superseding an existing AD 
that currently requires repetitive inspections of the spring cartridges 
of the elevator gust lock system to determine if the lock washer 
projection correctly fits the slots in the cartridge flange, and 
corrective action if necessary, for certain airplanes. This AD retains 
the requirements of the existing AD and adds a requirement for final 
terminating action for all affected airplanes.

DATES: Effective January 9, 2006.

ADDRESSES: The AD docket contains the proposed AD, comments, and any 
final disposition. You may examine the AD docket on the Internet at 
http://dms.dot.gov, or in person at the Docket Management Facility 
office between 9 a.m. and 5 p.m., Monday through Friday, except Federal 
holidays. The Docket Management Facility office (telephone (800) 647-
5227) is located on the plaza level of the Nassif Building at the U.S. 
Department of Transportation, 400 Seventh Street SW., room PL-401, 
Washington, DC. This docket number is FAA-2005-22033; the directorate 
identifier for this docket is 2004-NM-218-AD.

FOR FURTHER INFORMATION CONTACT: Todd Thompson, Aerospace Engineer, 
International Branch, ANM-116, FAA, Transport Airplane Directorate, 
1601 Lind Avenue, SW., Renton, Washington 98055-4056; telephone (425) 
227-1175; fax (425) 227-1149.

SUPPLEMENTARY INFORMATION: On November 18, 2005, the FAA issued AD 
2005-24-11, amendment 39-14391 (70 FR 72363, December 5, 2005), for 
certain EMBRAER Model EMB-135BJ, -135ER, -135KE, -135KL, -135LR, and 
Model EMB-145, -145ER, -145MR, -145LR, -145XR, -145MP, and -145EP 
airplanes. That AD requires repetitive inspections of the spring 
cartridges of the elevator gust lock system to determine if the lock 
washer projection correctly fits the slots in the cartridge flange, and 
corrective action if necessary. That AD also adds a requirement for 
final terminating action for all affected airplanes.
    As published, AD 2005-24-11 cited Brazilian airworthiness directive 
2003-01-03R1, which was issued showing an incorrect effective date of 
July 26, 2004. The Departmento de Aviacao Civil (DAC), which is the 
airworthiness authority for Brazil, has corrected the effective date of 
Brazilian airworthiness directive 2003-01-03R1 to read August 26, 2004.
    No other part of the regulatory information has been changed; 
therefore, the final rule is not republished in the Federal Register.
    The effective date of this AD remains January 9, 2006.


Sec.  39.13  [Corrected]

0
In the Federal Register of December 5, 2005, on page 72363, in the 
right-hand column, paragraph (1) of AD 2005-24-11 is corrected to read 
as follows:
* * * * *
    (1) Brazilian airworthiness directive 2003-01-03R1, dated August 
26, 2004, also addresses the subject of this AD.
* * * * *

    Issued in Renton, Washington, on December 23, 2005.
Ali Bahrami,
Manager, Transport Airplane Directorate, Aircraft Certification 
Service.
[FR Doc. 06-16 Filed 1-3-06; 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 2026-10-09T03:49:24.721881+00:00. Text extraction preserves the recorded source wording; it does not determine current requirements.

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1bda75bffb6a52cf4b78dbdab58410601f0d1234abf213e9aa9f8178253af453
Text SHA-256
f6bc42a12edd782844e979367ad9109bca39f276b16309e9e27caf8e3c1435aa

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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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