AD 2003-14-06
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | The Boeing Company | 737-200 Series | Airworthiness Directives; Boeing Model 737-200, -200C, -300, - 400, and -500 Series Airplanes |
| aircraft | The Boeing Company | 737-200C Series | Airworthiness Directives; Boeing Model 737-200, -200C, -300, - 400, and -500 Series Airplanes |
| aircraft | The Boeing Company | 737-300 Series | Airworthiness Directives; Boeing Model 737-200, -200C, -300, - 400, and -500 Series Airplanes |
| aircraft | The Boeing Company | 737-400 Series | Airworthiness Directives; Boeing Model 737-200, -200C, -300, - 400, and -500 Series Airplanes |
| aircraft | The Boeing Company | 737-500 Series | Airworthiness Directives; Boeing Model 737-200, -200C, -300, - 400, and -500 Series Airplanes |
Unsafe Condition
Cracking of certain lap splices.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Conduct repetitive inspections for cracking of certain lap splices. Take corrective action if necessary.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Before further flight.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Boeing Model 737-200, -200C, -300, -400, and -500 series airplanes.
AI-generated summary from the source AD text. Verify against the official source before acting.
Federal Register Abstract
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.
Document Text
Show stored source text (verify against official source)
[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 [<a href="http://www.gpo.gov">www.gpo.gov</a>]
[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
Source: Official FAA Source ↗
Retrieved: Apr 6, 2026
Rights: U.S. Government Public Domain
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