Published 2003-09-17 · Federal Register document 03-23669
Airworthiness Directives; Bombardier Model CL-600-2B19 (Regional Jet Series 100 & 440) Airplanes
Publication summary
This document corrects typographical errors that appeared in airworthiness directive (AD) 2003-14-02 that was published as a final rule; correction in the Federal Register on August 15, 2003 (68 FR 48783). The typographical errors resulted in an incorrect AD number and effective date. This AD is applicable to certain Bombardier Model CL- 600-2B19 (Regional Jet series 100 & 440) airplanes. This AD requires a one-time inspection of the aft edge of the left and right main windshields to determine whether a certain placard is installed, and corrective actions if necessary.
Why this record is shown
Source: Federal Register annual FAA metadata. Acquired 2026-09-03T22:23:10.496508+00:00. The title, summary and date are source facts.
- Source revision
- federal_register_ad_metadata_2003-b6c0b146601d56c4
- Source row
- results[337]
- Raw source SHA-256
- b6c0b146601d56c4829685d26300140986ff1ab0185264ed2f7f002dc27cf9e7
Correction notice · separate source edition
Recorded publication clauses
- AD identifier printed in this edition
- 2003-14-02
- Effective date printed in this edition
- Unknown
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Find all recorded historical references to AD 2003-14-02 · 0 printed reference observations in this pinned collection.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: 953a425e3a8af9a5964dec7dbc011834a996689940c227edcaa36bd92c85a02d. Source manifest: bfacf2bdfca311e5d7a09c0d5dac6589c7988ba78fa121c3096db0ad2e0714c5.
Official source · 2003-09-17
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 68, Number 180 (Wednesday, September 17, 2003)]
[Rules and Regulations]
[Page 54327]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 03-23669]
========================================================================
Rules and Regulations
Federal Register
________________________________________________________________________
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having general applicability and legal effect, most of which are keyed
to and codified in the Code of Federal Regulations, which is published
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Federal Register / Vol. 68, No. 180 / Wednesday, September 17, 2003 /
Rules and Regulations
[[Page 54327]]
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. 2001-NM-322-AD; Amendment 39-13221; AD 2003-14-02]
RIN 2120-AA64
Airworthiness Directives; Bombardier Model CL-600-2B19 (Regional
Jet Series 100 & 440) Airplanes
AGENCY: Federal Aviation Administration, DOT.
ACTION: Final rule; correction.
-----------------------------------------------------------------------
SUMMARY: This document corrects typographical errors that appeared in
airworthiness directive (AD) 2003-14-02 that was published as a final
rule; correction in the Federal Register on August 15, 2003 (68 FR
48783). The typographical errors resulted in an incorrect AD number and
effective date. This AD is applicable to certain Bombardier Model CL-
600-2B19 (Regional Jet series 100 & 440) airplanes. This AD requires a
one-time inspection of the aft edge of the left and right main
windshields to determine whether a certain placard is installed, and
corrective actions if necessary.
DATES: Effective August 14, 2003.
FOR FURTHER INFORMATION CONTACT: Serge Napoleon, Aerospace Engineer,
Airframe and Propulsion Branch, ANE-171, FAA, New York Aircraft
Certification Office, 10 Fifth Street, Third Floor, Valley Stream, New
York 11581; telephone (516) 256-7512; fax (516) 568-2716.
SUPPLEMENTARY INFORMATION: Airworthiness Directive (AD) 2003-14-02,
amendment 39-13221, applicable to certain Bombardier Model CL-600-2B19
(Regional Jet series 100 & 440) airplanes, was published as a final
rule; correction in the Federal Register on August 15, 2003 (68 FR
48783). That AD requires a one-time inspection of the aft edge of the
left and right main windshields to determine whether a certain placard
is installed, and corrective actions if necessary.
As published, that final rule; correction incorrectly specified the
AD number as ``2003-14-02 R1'' instead of ``2003-14-02'' and the
effective date as ``August 11, 2003'' instead of ``August 14, 2003.''
Since no other part of the regulatory information has been changed,
the final rule is not being republished in the Federal Register.
The effective date of this AD remains August 14, 2003.
Sec. 39.13 [Corrected]
0
On page 48783, in the third column, paragraph 2 of Part 39--
Airworthiness Directives is corrected to read as follows:
* * * * *
2. Section 39.13 is amended by correctly adding the following
airworthiness directive (AD):
AD 2003-14-02 Bombardier, Inc. (Formerly Canadair): Amendment 39-
13221. Docket 2001-NM-322-AD.
* * * * *
0
On page 48784, in the second column, paragraph (e) of AD 2003-14-02 is
corrected to read as follows:
* * * * *
(e) The effective date of this amendment remains August 14,
2003.
* * * * *
Issued in Renton, Washington, on September 11, 2003.
Vi L. Lipski,
Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 03-23669 Filed 9-16-03; 8:45 am]
BILLING CODE 4910-13-U
Why this text is shown
The complete text was extracted from the official GovInfo HTML edition for this publication. Acquired 2026-10-09T04:10:44.741156+00:00. Text extraction preserves the recorded source wording; it does not determine current requirements.
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- 67784a6848fbb9484676fe9a4b132978f0341031a9081b50c434b2e0c6f9fcfa
- Text SHA-256
- 953a425e3a8af9a5964dec7dbc011834a996689940c227edcaa36bd92c85a02d
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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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