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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.

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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

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Find all recorded historical references to AD 2003-14-06 · 0 printed reference observations in this pinned collection.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.

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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]


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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


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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.

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Source SHA-256
3b93948bef72777ac1ab768daf99b4cb29297508d2a0c50504075c308873101c
Text SHA-256
1baa056ac6ceb45e0d93af71112cac537c37c658c0907d8b78be4c6f01f96986

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