Published 2003-07-21 · Federal Register document 03-18421
Airworthiness Directives; Boeing Model 737-200, -200C, -300, -400, and -500 Series Airplanes
Publication summary
This document corrects a typographical error that appeared in airworthiness directive (AD) 2003-14-06 that was published in the Federal Register on July 9, 2003 (68 FR 40759). The typographical error resulted in an incorrect AD number in one location of the document. This AD is applicable to certain Boeing Model 737-200, -200C, -300, - 400, and -500 series airplanes. This AD requires repetitive inspections for cracking of certain lap splices, and corrective action 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[269]
- Raw source SHA-256
- b6c0b146601d56c4829685d26300140986ff1ab0185264ed2f7f002dc27cf9e7
Correction notice · separate source edition
Recorded publication clauses
- AD identifier printed in this edition
- 2003-14-06
- Effective date printed in this edition
- Unknown
This correction is a separate source edition; it is not counted as a new adopted rule.
No adopted-clause structure was recorded for this source edition. Read the complete text; no applicability conclusion has been inferred.
No replacement link has been established from this edition. The complete historical rule chain and current legal effect remain unknown.
Find all recorded historical references to AD 2003-14-06 · 0 printed reference observations in this pinned collection.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.
Why these observations are shown
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: 1baa056ac6ceb45e0d93af71112cac537c37c658c0907d8b78be4c6f01f96986. Source manifest: 525408076cca61bef5197b93685b8949f213bfe1b3acee7ad3d19e487773d3c1.
Official source · 2003-07-21
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 139 (Monday, July 21, 2003)]
[Rules and Regulations]
[Pages 42956-42957]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 03-18421]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. 2003-NM-165-AD; Amendment 39-13225; AD 2003-14-06]
RIN 2120-AA64
Airworthiness Directives; Boeing Model 737-200, -200C, -300, -
400, and -500 Series Airplanes
AGENCY: Federal Aviation Administration, DOT.
ACTION: Final rule; correction.
-----------------------------------------------------------------------
SUMMARY: This document corrects a typographical error that appeared in
airworthiness directive (AD) 2003-14-06 that was published in the
Federal Register on July 9, 2003 (68 FR 40759). The typographical error
resulted in an incorrect AD number in one location of the document.
This AD is applicable to certain Boeing Model 737-200, -200C, -300, -
400, and -500 series airplanes. This AD requires repetitive inspections
for cracking of certain lap splices, and corrective action if
necessary.
DATES: Effective July 14, 2003.
FOR FURTHER INFORMATION CONTACT: Duong Tran, Aerospace Engineer,
Airframe Branch, ANM-120S, FAA, Seattle Aircraft Certification Office,
1601 Lind Avenue, SW., Renton, Washington 98055-4056; telephone (425)
917-6452; fax (425) 917-6590.
SUPPLEMENTARY INFORMATION: Airworthiness Directive (AD) 2003-14-06,
amendment 39-13225, applicable to certain Boeing Model 737-200, -200C,
-300, -400, and -500 series airplanes, was published in the Federal
Register on July 9, 2003 (68 FR 40759). That AD requires repetitive
inspections for cracking of certain lap splices, and corrective action
if necessary.
As published, the AD number appears as ``2003-14-60'' in the
Product Identification line in the regulatory text of the AD. The
correct AD number is 2003-14-06. The number is referenced correctly
throughout the remainder of the document.
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 July 14, 2003.
Sec. 39.13 [Corrected]
0
On page 40761, in the first column, the Product Identification line of
AD 2003-14-06 is corrected to read as follows:
* * * * *
[[Page 42957]]
2003-14-06 Boeing: Amendment 39-13225. Docket 2003-NM-165-AD.
* * * * *
Issued in Renton, Washington, on July 15, 2003.
Ali Bahrami,
Acting Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 03-18421 Filed 7-18-03; 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 2026-10-09T04:11:51.265823+00:00. Text extraction preserves the recorded source wording; it does not determine current requirements.
Open the captured official edition
- Source SHA-256
- 3b93948bef72777ac1ab768daf99b4cb29297508d2a0c50504075c308873101c
- Text SHA-256
- 1baa056ac6ceb45e0d93af71112cac537c37c658c0907d8b78be4c6f01f96986
Return to the full metadata catalog · Search complete publication text · Explore retained publication text and evidence
Coverage and limits
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.
The collection uses 33 explicit annual source snapshots. Source captures and operative-text qualifications have separate states. Missing information remains unknown.