Airworthiness Directives; Raytheon Aircraft Company 65, 90, 99, 100, 200, and 1900 Series Airplanes, and Models 70 and 300 Airplanes, 7581 [E7-2754]

Download as PDF Federal Register / Vol. 72, No. 32 / Friday, February 16, 2007 / Rules and Regulations DEPARTMENT OF TRANSPORTATION This correction is needed to specify the correct section of the service bulletin necessary to do the actions of AD 2004–23–02. Federal Aviation Administration 14 CFR Part 39 [Docket No. 2003–CE–51–AD; Amendment 39–13857; AD 2004–23–02] Airworthiness Directives; Raytheon Aircraft Company 65, 90, 99, 100, 200, and 1900 Series Airplanes, and Models 70 and 300 Airplanes Federal Aviation Administration (FAA), DOT. ACTION: Final rule; correction. AGENCY: 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. Jkt 211001 PART 39—AIRWORTHINESS DIRECTIVES 1. The authority citation for part 39 continues to read as follows: FOR FURTHER INFORMATION CONTACT: rmajette on PROD1PC67 with RULES 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: I 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. 14:54 Feb 15, 2007 Correction of Publication I RIN 2120–AA64 VerDate Aug<31>2005 Need for the Correction Authority: 49 U.S.C. 106(g), 40113, 44701. § 39.13 [Corrected] 2. On page 64845, in § 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 § 39.13 of the Federal Aviation Regulations (14 CFR 39.13). The effective date remains December 23, 2004. I 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 DEPARTMENT OF HOMELAND SECURITY Coast Guard 33 CFR Part 117 [CGD08–07–002] RIN 1625–AA09 Drawbridge Operation Regulation; Upper Mississippi River, Rock Island, IL Coast Guard, DHS. Notice of deviation from drawbridge regulation. AGENCY: ACTION: SUMMARY: The Commander, Eighth Coast Guard District has issued a temporary deviation from the regulation governing the operations of the Rock Island Railroad and Highway Drawbridge, Mile 482.9, Rock Island, Illinois across the Upper Mississippi River. This deviation allows the bridge to remain closed-to-navigation from 9 PO 00000 Frm 00035 Fmt 4700 Sfmt 4700 7581 a.m. until 11:30 a.m., May 19, 2007. The deviation is necessary as the drawbridge is part of the annual route for the Quad Cities Heart Walk. DATES: This temporary deviation is effective from 9 a.m. until 11:30 a.m., May 19, 2007. ADDRESSES: Materials referred to in this document are available for inspection or copying at Room 2.107F in the Robert A. Young Federal Building, 1222 Spruce Street, St. Louis, MO 63103–2832, between 8 a.m. and 4 p.m., Monday through Friday, except Federal holidays. The Bridge Administration Branch maintains the public docket for this temporary deviation. FOR FURTHER INFORMATION CONTACT: Roger K. Wiebusch, Bridge Administrator, (314) 269–2378. SUPPLEMENTARY INFORMATION: The U.S. Army Rock Island Arsenal requested a temporary deviation for the Rock Island Railroad and Highway Drawbridge, mile 482.9, at Rock Island, Illinois across the Upper Mississippi River as the drawbridge is along the route of the annual Quad Cities Heart Walk. The Rock Island Railroad and Highway Drawbridge currently operates in accordance with 33 CFR 117.5 which requires the drawbridge to open promptly and fully for passage of vessels when a request to open is given in accordance with 33 CFR 117, Subpart A. In order to facilitate the annual event, the drawbridge must be kept in the closed-to-navigation position. This deviation allows the drawbridge to remain closed-to-navigation for two and one-half hours from 9 a.m. until 11:30 a.m., May 19, 2007. There are no alternate routes for vessels transiting this section of the Upper Mississippi River. The Rock Island Railroad and Highway Drawbridge, in the closed-tonavigation position, provides a vertical clearance of 23.8 feet above normal pool. Navigation on the waterway consists primarily of commercial tows and recreational watercraft. This temporary deviation has been coordinated with waterway users. No objections were received. In accordance with 33 CFR 117.35(e), the drawbridge shall return to its regular operating schedule immediately at the end of the designated time period. This deviation from the operating regulations is authorized under 33 CFR 117.35. Dated: February 1, 2007. Roger K. Wiebusch, Bridge Administrator. [FR Doc. E7–2795 Filed 2–15–07; 8:45 am] BILLING CODE 4910–15–P E:\FR\FM\16FER1.SGM 16FER1

Agencies

[Federal Register Volume 72, Number 32 (Friday, February 16, 2007)]
[Rules and Regulations]
[Page 7581]
From the Federal Register Online via the Government Printing 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.

-----------------------------------------------------------------------

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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