Definitions of Terms, 73589 [07-55526]

Download as PDF Federal Register / Vol. 72, No. 248 / Friday, December 28, 2007 / Rules and Regulations the Administrator finds necessary for safety in air commerce. This regulation is within the scope of that authority because it addresses an unsafe condition that is likely to exist or develop on products identified in this rulemaking action. Regulatory Findings We have determined that this AD will not have federalism implications under Executive Order 13132. This AD will not have a substantial direct effect on the States, on the relationship between the national government and the States, or on the distribution of power and responsibilities among the various levels of government. For the reasons discussed above, I certify that this AD: (1) Is not a ‘‘significant regulatory action’’ under Executive Order 12866; (2) Is not a ‘‘significant rule’’ under DOT Regulatory Policies and Procedures (44 FR 11034, February 26, 1979); and (3) Will not have a significant economic impact, positive or negative, on a substantial number of small entities under the criteria of the Regulatory Flexibility Act. We prepared a regulatory evaluation of the estimated costs to comply with this AD and placed it in the AD docket. See the ADDRESSES section for a location to examine the regulatory evaluation. List of Subjects in 14 CFR Part 39 Air transportation, Aircraft, Aviation safety, Incorporation by reference, Safety. Adoption of the Amendment Accordingly, under the authority delegated to me by the Administrator, the FAA amends 14 CFR part 39 as follows: I PART 39—AIRWORTHINESS DIRECTIVES 1. The authority citation for part 39 continues to read as follows: I Authority: 49 U.S.C. 106(g), 40113, 44701. § 39.13 [Amended] 2. The Federal Aviation Administration (FAA) amends § 39.13 by adding the following new airworthiness directive (AD): I pwalker on PROD1PC71 with RULES 2007–26–07 Boeing: Amendment 39–15309. Docket No. FAA–2007–28352; Directorate Identifier 2007–NM–037–AD. Effective Date (a) This AD becomes effective February 1, 2008. Affected ADs (b) None. VerDate Aug<31>2005 23:53 Dec 27, 2007 Jkt 214001 Applicability (c) This AD applies to Boeing Model 747– 200B, 747–300, 747–400, 747–400D, and 747–400F series airplanes, certificated in any category, equipped with General Electric CF6–80C2 engines. Unsafe Condition (d) This AD results from two reports of missing flipper doors for the engine core cowl. We are issuing this AD to detect and correct migrated hinge pins and damaged flipper doors, which could allow the flipper door to fall off, resulting in the potential for an engine fire to propagate into the flammable leakage zone of the strut and for the amount of fire extinguishing agent reaching the fire to be diluted, and subsequent uncontained fire in the engine strut. Compliance (e) You are responsible for having the actions required by this AD performed within the compliance times specified, unless the actions have already been done. Inspection of the Flipper Door Assemblies (f) Within 24 months after the effective date of this AD: Do a general visual inspection for migrated hinge pins and damaged flipper doors of the left- and righthand flipper door assemblies of the engine core cowls, and do all applicable corrective actions, by accomplishing all the actions specified in the Accomplishment Instructions of Boeing Special Attention Service Bulletin 747–71–2310, dated October 13, 2005. Do all applicable corrective actions before further flight. Repeat the inspection thereafter at intervals not to exceed 18 months for that flipper door assembly, until doing the actions specified in paragraph (g) of this AD. Note 1: Boeing Special Attention Service Bulletin 747–71–2310, dated October 13, 2005, refers to Rohr Service Bulletin TBC/ 80C2–NAC–71–035, dated October 10, 2005, as an additional source of service information for accomplishing the actions specified in paragraph (f) of this AD. Terminating Action for Repetitive Inspections (g) Accomplishing the inspection and applicable modification of a hinge assembly of a flipper door assembly of the engine core cowl in accordance with the Accomplishment Instructions of Boeing Special Attention Service Bulletin 747–71– 2310, dated October 13, 2005; or Rohr Service Bulletin TBC/80C2–NAC–71–035, dated October 10, 2005; terminates the repetitive inspection requirements of this AD for that hinge assembly. Parts Installation (h) As of the effective date of this AD, no person may install, on any airplane, a hinge assembly, part number 224–2335–69, for the flipper door of the engine core cowl unless it has been modified in accordance with the requirements of paragraph (g) of this AD. Material Incorporated by Reference (i) You must use Boeing Special Attention Service Bulletin 747–71–2310, dated October PO 00000 Frm 00017 Fmt 4700 Sfmt 4700 73589 13, 2005, to perform the actions that are required by this AD, unless the AD specifies otherwise. The Director of the Federal Register approved the incorporation by reference of this document in accordance with 5 U.S.C. 552(a) and 1 CFR part 51. Contact Boeing Commercial Airplanes, P.O. Box 3707, Seattle, Washington 98124–2207, for a copy of this service information. You may review copies at the FAA, Transport Airplane Directorate, 1601 Lind Avenue SW., Renton, Washington; or at the National Archives and Records Administration (NARA). For information on the availability of this material at NARA, call 202–741–6030, or go to: http://www.archives.gov/federalregister/cfr/ibr-locations.html. Issued in Renton, Washington, on December 11, 2007. Michael J. Kaszycki, Acting Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. E7–24520 Filed 12–27–07; 8:45 am] BILLING CODE 4910–13–P DEPARTMENT OF COMMERCE Bureau of Industry and Security 15 CFR Part 772 Definitions of Terms CFR Correction In Title 15 of the Code of Federal Regulations, Parts 300 to 799, revised as of January 1, 2007, on page 577, in § 772.1, in the second column, the second definition of Production is removed. [FR Doc. 07–55526 Filed 12–27–07; 8:45 am] BILLING CODE 1505–01–D DEPARTMENT OF HEALTH AND HUMAN SERVICES Food and Drug Administration 21 CFR Parts 201, 312, 314, 601, 610, 801, 807, 809, 812, and 814 [Docket No. 2006N–0466] Exceptions or Alternatives to Labeling Requirements for Products Held by the Strategic National Stockpile AGENCY: Food and Drug Administration, HHS. Interim final rule; request for comments. ACTION: SUMMARY: The Food and Drug Administration (FDA) is issuing regulations to permit FDA Center Directors to grant exceptions or alternatives to certain regulatory labeling requirements applicable to human drugs, biological products, or E:\FR\FM\28DER1.SGM 28DER1

Agencies

[Federal Register Volume 72, Number 248 (Friday, December 28, 2007)]
[Rules and Regulations]
[Page 73589]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: 07-55526]


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DEPARTMENT OF COMMERCE

Bureau of Industry and Security

15 CFR Part 772


Definitions of Terms

CFR Correction

    In Title 15 of the Code of Federal Regulations, Parts 300 to 799, 
revised as of January 1, 2007, on page 577, in Sec.  772.1, in the 
second column, the second definition of Production is removed.

[FR Doc. 07-55526 Filed 12-27-07; 8:45 am]
BILLING CODE 1505-01-D