AD 2003-14-06

Recurring final rule

Airworthiness Directives; Boeing Model 737-200, -200C, -300, -400, and -500 Series Airplanes

AD Number
2003-14-06
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 2003-NM-165-AD
FR Citation
68 FR 42956

Applicability

TypeManufacturerModelDetails
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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