
[Federal Register: April 11, 2008 (Volume 73, Number 71)]
[Rules and Regulations]               
[Page 19746]
From the Federal Register Online via GPO Access [wais.access.gpo.gov]
[DOCID:fr11ap08-2]                         

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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 23

 
Damage Tolerance and Fatigue Evaluation of Structure

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Final rule; technical amendment.

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SUMMARY: This action corrects a paragraph reference that appeared in 
the final rule, Airworthiness Standards; Airframe Rules Based on 
European Joint Aviation Requirements, which the FAA published in the 
Federal Register on February 9, 1996. In that final rule, the FAA 
inadvertently changed a paragraph reference. The intent of this action 
is to correct the error in the regulation to ensure the requirement is 
clear and accurate.

DATES: Effective Date: April 11, 2008.

FOR FURTHER INFORMATION CONTACT: Pat Mullen, Regulations and Policy, 
ACE-111, Federal Aviation Administration, 901 Locust Street, Kansas 
City, MO 64106; telephone (816) 329-4111; e-mail pat.mullen@faa.gov.

SUPPLEMENTARY INFORMATION: On February 9, 1996, the FAA published in 
the Federal Register (61 FR 5147) a final rule that amended Sec.  
23.573(b) by removing the reference ``Sec.  23.571(c)'' and adding the 
reference ``Sec.  23.571(a)(3)'' in its place. Paragraph (a)(3) of 
Sec.  23.571 does not exist, and the reference to Sec.  23.571(c) 
should have remained. This document corrects Sec.  23.573(b) to reflect 
the correct paragraph reference, Sec.  23.571(c). This correction will 
not impose any additional requirements.

Technical Amendment

    This technical amendment will correct Sec.  23.573(b) to properly 
reference Sec.  23.571(c).

Justification for Immediate Adoption

    Because this action corrects an incorrect paragraph reference, the 
FAA finds that notice and public comment under 5 U.S.C. 553(b) is 
unnecessary. For the same reason, the FAA finds that good cause exists 
under 5 U.S.C. 553(d) for making this rule effective upon publication.

List of Subjects in 14 CFR Part 23

    Aircraft, Aviation safety, Signs and symbols.

The Amendment

0
Accordingly, Title 14 of the Code of Federal Regulations (CFR) part 23 
is amended as follows:

PART 23--AIRWORTHINESS STANDARDS: NORMAL, UTILITY, ACROBATIC, AND 
COMMUTER CATEGORY AIRPLANES

0
1. The authority citation for part 23 continues to read as follows:

    Authority: 49 U.S.C. 106(g), 40013, 44701, 44702, 44704.


0
2. Amend Sec.  23.573 by revising the first sentence in paragraph (b) 
introductory text to read as follows:


Sec.  23.573  Damage tolerance and fatigue evaluation of structure.

* * * * *
    (b) Metallic airframe structure. If the applicant elects to use 
Sec.  23.571(c) or Sec.  23.572(a)(3), then the damage tolerance 
evaluation must include a determination of the probable locations and 
modes of damage due to fatigue, corrosion, or accidental damage. * * *
* * * * *

    Issued in Washington, DC, on April 7, 2008.
Pamela Hamilton-Powell,
Director, Office of Rulemaking.
[FR Doc. E8-7649 Filed 4-10-08; 8:45 am]

BILLING CODE 4910-13-P
