Airworthiness Directives; Raytheon Aircraft Company 65, 90, 99, 100, 200, and 1900 Series Airplanes, and Models 70 and 300 Airplanes

[Federal Register Volume 72, Number 32 (Friday, February 16, 2007)]
[Rules and Regulations]
[Page 7581]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: E7-2754]



[[Page 7581]]

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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. 2003-CE-51-AD; Amendment 39-13857; AD 2004-23-02]
RIN 2120-AA64


Airworthiness Directives; Raytheon Aircraft Company 65, 90, 99, 
100, 200, and 1900 Series Airplanes, and Models 70 and 300 Airplanes

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Final rule; correction.

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SUMMARY: This document makes a correction to Airworthiness Directive 
(AD) 2004-23-02, which was published in the Federal Register on 
November 9, 2004 (69 FR 64842), and applies to all Raytheon Aircraft 
Company (Raytheon) 65, 90, 99, 100, 200, and 1900 series airplanes and 
Models 70 and 300 airplanes. AD 2004-23-2 requires repetitive 
inspections of the nose landing gear (NLG) fork for cracks with 
replacement if cracks are found (replacement terminates repetitive 
inspections). Current language in paragraph (e)(3) of AD 2004-23-02 
references Part III of the Accomplishment Instructions of the service 
bulletin instead of Part II. This document corrects that paragraph by 
changing the reference from Part III to Part II.

DATES: The effective date of this AD (2004-23-02) remains December 23, 
2004.

FOR FURTHER INFORMATION CONTACT: Steven E. Potter, Aerospace Engineer, 
Wichita Aircraft Certification Office (ACO), FAA, 1801 Airport Road, 
Wichita, Kansas 67209; telephone: (316) 946-4124; facsimile: (316) 946-
4407.

SUPPLEMENTARY INFORMATION:

Discussion

    On November 1, 2004, the FAA issued AD 2004-23-02, Amendment 39-
13857 (69 FR 64842, November 9, 2004), which applies to all 65, 90, 99, 
100, 200, and 1900 series airplanes and Models 70 and 300 airplanes. AD 
2004-23-2 requires repetitive inspections of the NLG fork for cracks 
with replacement if cracks are found (replacement terminates repetitive 
inspections). Current language in paragraph (e)(3) of AD 2004-23-02 
references Part III of the Accomplishment Instructions of Raytheon 
Mandatory Service Bulletin SB 32-2102, Revision 7, Revised: July, 2003, 
instead of Part II.

Need for the Correction

    This correction is needed to specify the correct section of the 
service bulletin necessary to do the actions of AD 2004-23-02.

Correction of Publication

0
Accordingly, the publication of November 9, 2004 (69 FR 64842), of 
Amendment 39-13857, AD 2004-23-02, which was the subject of FR Doc. 04-
24718, is corrected as follows:

PART 39--AIRWORTHINESS DIRECTIVES

0
1. The authority citation for part 39 continues to read as follows:

    Authority: 49 U.S.C. 106(g), 40113, 44701.


Sec.  39.13  [Corrected]

0
2. On page 64845, in Sec.  39.13 [Amended], in paragraph (e)(3), in the 
Procedures column, remove the phrase ``Part III'' and add ``Part II'' 
in its place.
    Action is taken herein to correct this reference in AD 2004-23-02 
and to add this AD correction to Sec.  39.13 of the Federal Aviation 
Regulations (14 CFR 39.13).
    The effective date remains December 23, 2004.

    Issued in Kansas City, Missouri, on February 9, 2007.
David R. Showers,
Acting Manager, Small Airplane Directorate, Aircraft Certification 
Service.
 [FR Doc. E7-2754 Filed 2-15-07; 8:45 am]
BILLING CODE 4910-13-P

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