Airworthiness Directives; Pacific Aerospace Corporation, Ltd. Model 750XL Airplanes, 53102 [E7-18136]

Download as PDF 53102 Federal Register / Vol. 72, No. 180 / Tuesday, September 18, 2007 / Rules and Regulations period, it is unlikely that this interim rule will have any substantial effects on trade, or on large or small businesses. Under these circumstances, the Administrator of the Animal and Plant Health Inspection Service has determined that this action will not have a significant economic impact on a substantial number of small entities. DEPARTMENT OF TRANSPORTATION Executive Order 12988 Airworthiness Directives; Pacific Aerospace Corporation, Ltd. Model 750XL Airplanes This rule has been reviewed under Executive Order 12988, Civil Justice Reform. This rule: (1) Preempts all State and local laws and regulations that are inconsistent with this rule; (2) has retroactive effect to June 5, 2007; and (3) does not require administrative proceedings before parties may file suit in court challenging this rule. Paperwork Reduction Act This interim rule contains no information collection or recordkeeping requirements under the Paperwork Reduction Act of 1995 (44 U.S.C. 3501 et seq.). List of Subjects in 9 CFR Part 94 Animal diseases, Imports, Livestock, Meat and meat products, Milk, Poultry and poultry products, Reporting and recordkeeping requirements. Accordingly, we are amending 9 CFR part 94 as follows: I PART 94—RINDERPEST, FOOT-ANDMOUTH DISEASE, FOWL PEST (FOWL PLAGUE), EXOTIC NEWCASTLE DISEASE, AFRICAN SWINE FEVER, CLASSICAL SWINE FEVER, AND BOVINE SPONGIFORM ENCEPHALOPATHY: PROHIBITED AND RESTRICTED IMPORTATIONS 1. The authority citation for part 94 continues to read as follows: I Authority: 7 U.S.C. 450, 7701–7772, 7781– 7786, and 8301–8317; 21 U.S.C. 136 and 136a; 31 U.S.C. 9701; 7 CFR 2.22, 2.80, and 371.4. § 94.8 [Amended]. 2. In § 94.8, the introductory text is amended by adding the word ‘‘Georgia,’’ after the word ‘‘Cuba.’’ mstockstill on PROD1PC66 with RULES I Done in Washington, DC, this 12th day of September 2007. Kevin Shea, Acting Administrator, Animal and Plant Health Inspection Service. [FR Doc. E7–18315 Filed 9–17–07; 8:45 am] BILLING CODE 3410–34–P VerDate Aug<31>2005 18:27 Sep 17, 2007 Jkt 211001 Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA–2007–27864; Directorate Identifier 2007–CE–038–AD; Amendment 39–15161; AD 2007–17–03] RIN 2120–AA64 Federal Aviation Administration (FAA), DOT. ACTION: Final rule; correction. AGENCY: Discussion On August 8, 2007, the FAA issued AD 2007–17–03, Amendment 39–15161 (72 FR 46541, August 21, 2007), which applies to certain Pacific Aerospace Corporation Ltd Model 750XL airplanes. AD 2007–17–03 requires you to inspect the inboard end of the rear spar for security of the blind rivets, inspecting the radii of the rear spar upper and lower flanges for cracking, inspecting the aft flange of the inboard rib for cracking, replacing the rear spar if cracks are found in any of the inspections, and replacing rear spar blind rivets with bolts or rivets. The paragraph following the section heading Frm 00002 Fmt 4700 Sfmt 4700 Need for the Correction This correction is needed to specify the paragraph designator for the paragraph that follows the Materials Incorporated by Reference section heading. Correction of Publication Accordingly, the publication of August 21, 2007 (72 FR 46541), of Amendment 39–15161; AD 2007–17–03 which was the subject of FR Doc. E7– 15978, is corrected as follows: I SUMMARY: This document makes a correction to Airworthiness Directive (AD) 2007–17–03, which was published in the Federal Register on August 21, 2007 (72 FR 46541), and applies to certain Pacific Aerospace Corporation Ltd Model 750XL airplanes. AD 2007– 17–03 requires inspecting the inboard end of the rear spar for security of the blind rivets, inspecting the radii of the rear spar upper and lower flanges for cracking, inspecting the aft flange of the inboard rib for cracking, replacing the rear spar if cracks are found in any of the inspections, and replacing rear spar blind rivets with bolts or rivets. The paragraph following the section heading Materials Incorporated by Reference does not have a paragraph designator. This document corrects that paragraph by inserting the paragraph designator ‘‘(i)’’ preceding the paragraph text. DATES: The effective date of this AD (2007–17–03) remains September 25, 2007. FOR FURTHER INFORMATION CONTACT: Karl Schletzbaum, Aerospace Engineer, FAA, Small Airplane Directorate, 901 Locust, Room 301, Kansas City, Missouri 64106; telephone: (816) 329–4146; fax: (816) 329–4090. SUPPLEMENTARY INFORMATION: PO 00000 Materials Incorporated by Reference does not have a paragraph designator. This document corrects that paragraph by inserting the paragraph designator ‘‘(i)’’ preceding the paragraph text. § 39.13 [Corrected] On page 46542, in the second column, at the beginning of the paragraph following the Materials Incorporated by Reference section heading, the paragraph designator (i), indented two spaces, precedes the paragraph. Action is taken herein to correct this reference in AD 2007–17–03 and to add this AD correction to § 39.13 of the Federal Aviation Regulations (14 CFR 39.13). The effective date remains September 25, 2007. I Issued in Kansas City, Missouri, on September 10, 2007. Kim Smith, Manager, Small Airplane Directorate, Aircraft Certification Service. [FR Doc. E7–18136 Filed 9–17–07; 8:45 am] BILLING CODE 4910–13–P DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA–2007–28372; Directorate Identifier 2007–NM–080–AD; Amendment 39–15194; AD 2007–19–04] RIN 2120–AA64 Airworthiness Directives; Airbus Model A300F4–605R and A300F4–622R Airplanes Federal Aviation Administration (FAA), Department of Transportation (DOT). ACTION: Final rule. AGENCY: SUMMARY: We are adopting a new airworthiness directive (AD) for the products listed above. This AD results from mandatory continuing airworthiness information (MCAI) originated by an aviation authority of E:\FR\FM\18SER1.SGM 18SER1

Agencies

[Federal Register Volume 72, Number 180 (Tuesday, September 18, 2007)]
[Rules and Regulations]
[Page 53102]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: E7-18136]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2007-27864; Directorate Identifier 2007-CE-038-AD; 
Amendment 39-15161; AD 2007-17-03]
RIN 2120-AA64


Airworthiness Directives; Pacific Aerospace Corporation, Ltd. 
Model 750XL 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) 2007-17-03, which was published in the Federal Register on August 
21, 2007 (72 FR 46541), and applies to certain Pacific Aerospace 
Corporation Ltd Model 750XL airplanes. AD 2007-17-03 requires 
inspecting the inboard end of the rear spar for security of the blind 
rivets, inspecting the radii of the rear spar upper and lower flanges 
for cracking, inspecting the aft flange of the inboard rib for 
cracking, replacing the rear spar if cracks are found in any of the 
inspections, and replacing rear spar blind rivets with bolts or rivets. 
The paragraph following the section heading Materials Incorporated by 
Reference does not have a paragraph designator. This document corrects 
that paragraph by inserting the paragraph designator ``(i)'' preceding 
the paragraph text.

DATES: The effective date of this AD (2007-17-03) remains September 25, 
2007.

FOR FURTHER INFORMATION CONTACT: Karl Schletzbaum, Aerospace Engineer, 
FAA, Small Airplane Directorate, 901 Locust, Room 301, Kansas City, 
Missouri 64106; telephone: (816) 329-4146; fax: (816) 329-4090.

SUPPLEMENTARY INFORMATION:

Discussion

    On August 8, 2007, the FAA issued AD 2007-17-03, Amendment 39-15161 
(72 FR 46541, August 21, 2007), which applies to certain Pacific 
Aerospace Corporation Ltd Model 750XL airplanes. AD 2007-17-03 requires 
you to inspect the inboard end of the rear spar for security of the 
blind rivets, inspecting the radii of the rear spar upper and lower 
flanges for cracking, inspecting the aft flange of the inboard rib for 
cracking, replacing the rear spar if cracks are found in any of the 
inspections, and replacing rear spar blind rivets with bolts or rivets. 
The paragraph following the section heading Materials Incorporated by 
Reference does not have a paragraph designator. This document corrects 
that paragraph by inserting the paragraph designator ``(i)'' preceding 
the paragraph text.

Need for the Correction

    This correction is needed to specify the paragraph designator for 
the paragraph that follows the Materials Incorporated by Reference 
section heading.

Correction of Publication

0
Accordingly, the publication of August 21, 2007 (72 FR 46541), of 
Amendment 39-15161; AD 2007-17-03 which was the subject of FR Doc. E7-
15978, is corrected as follows:


Sec.  39.13  [Corrected]

0
On page 46542, in the second column, at the beginning of the paragraph 
following the Materials Incorporated by Reference section heading, the 
paragraph designator (i), indented two spaces, precedes the paragraph.
    Action is taken herein to correct this reference in AD 2007-17-03 
and to add this AD correction to Sec.  39.13 of the Federal Aviation 
Regulations (14 CFR 39.13).
    The effective date remains September 25, 2007.

    Issued in Kansas City, Missouri, on September 10, 2007.
Kim Smith,
Manager, Small Airplane Directorate, Aircraft Certification Service.
 [FR Doc. E7-18136 Filed 9-17-07; 8:45 am]
BILLING CODE 4910-13-P