March 14, 2005 – Federal Register Recent Federal Regulation Documents

Loss Limitation Rules
Document Number: C5-3951
Type: Rule
Date: 2005-03-14
Agency: Internal Revenue Service, Department of Treasury, Department of the Treasury
Termination of Designation of the State of North Dakota With Respect to the Inspection of Poultry Products
Document Number: 05-4993
Type: Proposed Rule
Date: 2005-03-14
Agency: Department of Agriculture, Food Safety and Inspection Service
The Food Safety and Inspection Service (FSIS) is proposing to amend the poultry products inspection regulations by terminating the designation of the State of North Dakota under sections 1 through 4, 6 through 10, 11(b), 11(c), and 12 through 22 of the Poultry Products Inspection Act (PPIA). The Commissioner of Agriculture of the State of North Dakota has advised this Department that effective November 8, 2004, the State will be in a position to administer a State poultry inspection program that includes requirements that are at least equal to those imposed under the Federal poultry products inspection program for poultry and poultry products distributed in interstate commerce.
Establishment of Class E Airspace; Mifflintown, PA
Document Number: 05-4981
Type: Rule
Date: 2005-03-14
Agency: Federal Aviation Administration, Department of Transportation
This action establishes Class E airspace at Mifflintown, PA. Controlled airspace extending upward from 700 feet Above Ground Level (AGL) is needed to contain aircraft operating into Mifflintown Airport, Mifflintown, PA, under Instrument Flight Rules (IFR).
Amendment to Class E Airspace; Presque Isles, ME
Document Number: 05-4980
Type: Rule
Date: 2005-03-14
Agency: Federal Aviation Administration, Department of Transportation
This action revises the Class E airspace area at Presque Isle, ME (PQI) to increase the controlled airspace in the vicinity of the Northern Main Regional Airport (PQI), the Caribou Municipal Airport (CAR), and the Loring International Airport (ME16). This action is necessary to accommodate aircraft arriving at Loring International Airport using the new Instrument Landing System (ILS) approach to that airport.
Modification of Class E Airspace; Rolla/Vichy, MO
Document Number: 05-4979
Type: Rule
Date: 2005-03-14
Agency: Federal Aviation Administration, Department of Transportation
This document confirms the effective date of the direct final rule which revises Class E airspace at Rolla/Vichy, MO.
Security Zone; Protection of Military Cargo, Captain of the Port Zone Puget Sound, WA
Document Number: 05-4965
Type: Rule
Date: 2005-03-14
Agency: Coast Guard, Department of Homeland Security
The Captain of the Port Puget Sound will begin enforcing the Budd Inlet security zone in West Bay, Olympia, WA, on Friday, March 11, 2005 at 8 a.m. Pacific Standard Time. The security zone provides for the security of Department of Defense assets and military cargo in the navigable waters of Puget Sound and adjacent waters. The security zone will be enforced until Tuesday, March 15, 2005 at 11:59 p.m. Pacific Standard Time.
Uniform Compliance Date for Food Labeling Regulations
Document Number: 05-4956
Type: Rule
Date: 2005-03-14
Agency: Food and Drug Administration, Department of Health and Human Services
The Food and Drug Administration (FDA) is establishing January 1, 2008, as the uniform compliance date for food labeling regulations that are issued between March 14, 2005, and December 31, 2006. FDA periodically announces uniform compliance dates for new food labeling requirements to minimize the economic impact of label changes. On December 31, 2002, FDA established January 1, 2006, as the uniform compliance date for food labeling regulations that issued between January 1, 2003, and December 31, 2004.
Tennessee: Final Authorization of State Hazardous Waste Management Program Revisions
Document Number: 05-4953
Type: Proposed Rule
Date: 2005-03-14
Agency: Environmental Protection Agency
Tennessee has applied to EPA for Final authorization of the changes to its hazardous waste program under the Resource Conservation and Recovery Act (RCRA). EPA proposes to grant final authorization to Tennessee for RCRA Cluster XIII. In the ``Rules and Regulations'' section of this Federal Register, EPA is authorizing the changes by an immediate final rule. EPA did not make a proposal prior to the immediate final rule because we believe this action is not controversial and do not expect comments that oppose it. We have explained the reasons for this authorization in the preamble to the immediate final rule. Unless we get written comments which oppose this authorization during the comment period, the immediate final rule will become effective on the date it establishes, and we will not take further action on this proposal. If we get comments that oppose this action, we will withdraw the immediate final rule and it will not take effect. We will then respond to public comments in a later final rule based on this proposal. You may not have another opportunity for comment. If you want to comment on this action, you must do so at this time.
Tennessee: Final Authorization of State Hazardous Waste Management Program Revision
Document Number: 05-4952
Type: Rule
Date: 2005-03-14
Agency: Environmental Protection Agency
Tennessee has applied to EPA for Final authorization of the changes to its hazardous waste program under the Resource Conservation and Recovery Act (RCRA). EPA has determined that these changes satisfy all requirements needed to qualify for Final authorization, and is authorizing the State's changes through this immediate final action. EPA is publishing this rule to authorize the changes without a prior proposal because we believe this action is not controversial and do not expect comments that oppose it. Unless we get written comments which oppose this authorization during the comment period, the decision to authorize Tennessee's changes to its hazardous waste program will take effect. If we get comments that oppose this action, we will publish a document in the Federal Register withdrawing this rule before it takes effect and a separate document in the proposed rules section of this Federal Register will serve as a proposal to authorize the changes.
Scholar Accountability Policy
Document Number: 05-4951
Type: Proposed Rule
Date: 2005-03-14
Agency: Harry S. Truman Scholarship Foundation, Agencies and Commissions
The Truman Scholarship Foundation (Foundation) proposes to amend its regulations with respect to Scholar accountability to the Foundation for scholarship funds received. This rule is to clarify existing Foundation policy. This is the second notice for public comment: the first was published in the Federal Register (January 21, 2005 70 FR 3178-3179), and no comments were received.
Valuation of Benefits; Mortality Assumptions
Document Number: 05-4950
Type: Proposed Rule
Date: 2005-03-14
Agency: Pension Benefit Guaranty Corporation, Agencies and Commissions
The Pension Benefit Guaranty Corporation proposes to amend its benefit valuation regulation by adopting more current mortality assumptions (moving from a version of GAM-83 to a version of GAM-94). The updated mortality assumptions will better conform to those used by private- sector insurers in pricing group annuities.
Modification of Class E Airspace; Coffeyville, KS
Document Number: 05-4911
Type: Rule
Date: 2005-03-14
Agency: Federal Aviation Administration, Department of Transportation
This document confirms the effective date of the direct final rule which revises Class E airspace at Coffeyville, KS.
Proposed Revision of VOR Federal Airway 363; CA
Document Number: 05-4909
Type: Proposed Rule
Date: 2005-03-14
Agency: Federal Aviation Administration, Department of Transportation
This action proposes to revise VOR Federal Airway 363 (V-363) between the Mission Bay, CA, Very High Frequency Omnidirectional Range/ Tactical Air Navigation (VORTAC) and the Pomona, CA, VORTAC. Specifically, the FAA is proposing this realignment to provide a southwestern route structure to circumnavigate the Camp Pendleton, CA, range complex.
Proposed Establishment of Area Navigation Routes (RNAV), Alaska
Document Number: 05-4908
Type: Proposed Rule
Date: 2005-03-14
Agency: Federal Aviation Administration, Department of Transportation
This action proposes to establish 39 low altitude area navigation (RNAV) routes in Alaska to support the Alaskan Capstone Program. The FAA is proposing this action to enhance safety and improve the efficient use of the navigable airspace in Alaska.
Approval and Promulgation of Air Quality Implementation Plans; Ohio; Withdrawal of Direct Final Rule
Document Number: 05-4899
Type: Rule
Date: 2005-03-14
Agency: Environmental Protection Agency
Due to the receipt of adverse comments the EPA is withdrawing the January 19, 2005 (70 FR 2954), direct final rule approving a revision to Ohio's Oxides of Nitrogen (NOX) State Implementation Plan (SIP). The State of Ohio submitted this revision as a change to the SIP for NOX on June 28, 2004. In the direct final rule, EPA stated that if adverse comments were submitted by February 19, 2005, the rule would be withdrawn and not take effect. On February 18, 2005, EPA received a comment from a citizen and from the State of Ohio. EPA believes the comments are adverse and, therefore, EPA is withdrawing the direct final rule. EPA will address the comments in a subsequent final action based upon the proposed action also published on January 19, 2005 (70 FR 2992). EPA will not institute a second comment period on this action.
Airworthiness Directives; Boeing Model 737-600, -700, -700C, -800, and -900 Series Airplanes
Document Number: 05-4829
Type: Rule
Date: 2005-03-14
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new airworthiness directive (AD) for certain Boeing Model 737-600, -700, -700C, -800, and -900 series airplanes. This AD requires repetitive detailed, low frequency eddy current, and high frequency eddy current inspections of the webs of the aft pressure bulkhead at body station 1016 for cracks, and corrective action if necessary. This AD is prompted by a report of cracks found, during fatigue testing, at several of the fastener rows in the web lap splices at the dome apex of the aft pressure bulkhead. We are issuing this AD to detect and correct fatigue cracks in the webs of the aft pressure bulkhead, which could result in rapid decompression of the airplane.
Airworthiness Directives; Airbus Model A300 B4-622R and A300 F4-622R Airplanes
Document Number: 05-4828
Type: Rule
Date: 2005-03-14
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new airworthiness directive (AD) for certain Airbus Model A300 B4-622R and A300 F4-622R airplanes. This AD requires doing a one-time inspection to determine if lower guide fittings for the forward doors are installed in the correct positions, and corrective action if necessary. This AD is prompted by reports that lower guide fittings for the forward doors were found installed in the wrong positions at frames 14 and 16A. We are issuing this AD to prevent difficulty opening the forward doors, which could impede an emergency evacuation and result in injury to passengers or crewmembers.
Airworthiness Directives; Boeing Model 737-300, -400, and -500 Series Airplanes Modified In Accordance With Supplemental Type Certificate (STC) ST00127BO
Document Number: 05-4827
Type: Rule
Date: 2005-03-14
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new airworthiness directive (AD) for Boeing Model 737-300, -400, and -500 series airplanes modified in accordance with STC ST00127BO. This AD requires installation of bonding straps to the safe side harnesses of the digital transient suppression device of the fuel quantity indicating system. This AD is prompted by the results of fuel system reviews conducted by the STC holder. We are issuing this AD to prevent unsafe levels of current or energy from entering the fuel tank, due to hot short faults or threat conditions associated with the safe side harness assembly, which could result in a fire or explosion of the fuel tank.
Airworthiness Directives; Eurocopter France Model EC 155B and EC 155B1 Helicopters
Document Number: 05-4807
Type: Rule
Date: 2005-03-14
Agency: Federal Aviation Administration, Department of Transportation
This amendment adopts a new airworthiness directive (AD) for Eurocopter France (Eurocopter) Model EC 155B and EC 155B1 helicopters that requires inspecting the chamfer of the stop on the cabin sliding doors (doors) and installing an airworthy stop if the chamfer exceeds a certain length; and prior to each flight, visually checking the door to determine if it is correctly locked in the open position before flying with the doors open, and checking the locking indicator light and the position of the door handles before flying with the doors closed. This amendment also requires revising the Limitations Section of the Rotorcraft Flight Manual (RFM) to prohibit the opening or closing of a cabin sliding door at airspeeds of 40 or greater knots indicated airspeed (KIAS). This amendment is prompted by a report of a door separating from a helicopter during flight. The actions specified by this AD are intended to prevent separation of a door during flight and damage to the helicopter, resulting in a forced landing or loss of control of the helicopter.
Airworthiness Directives; Honeywell International Inc. TFE731-2 and -3 Series Turbofan Engines
Document Number: 05-4686
Type: Rule
Date: 2005-03-14
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new airworthiness directive (AD) for Honeywell International Inc. (formerly AlliedSignal Inc. and Garrett Turbine Engine Co.) TFE731-2 and -3 series turbofan engines with certain part number (P/N) low pressure turbine (LPT) stage 1 disks installed. This AD requires for TFE731-2 and -2C series engines, initial and repetitive measurements and calculations to determine acceptance, and adjustment or replacement if necessary, of the LPT stage 1 nozzle assembly. This AD also requires for TFE731-3, -3A, -3AR, -3B, -3BR, and -3R series engines, replacement of LPT stage 1 disks with serviceable disks. This AD also allows replacement of the LPT stage 1 disk with a disk having a part number not listed in the AD as optional terminating action to the repetitive actions. This AD results from a report of an uncontained failure of the LPT stage 1 disk installed in a TFE731-3-1H turbofan engine. We are issuing this AD to prevent additional uncontained failure of the LPT stage 1 disk, and possible damage to the airplane.
Airworthiness Directives; Dornier Model 328-300 Series Airplanes
Document Number: 05-4413
Type: Rule
Date: 2005-03-14
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new airworthiness directive (AD) for certain Dornier Model 328-300 series airplanes. This AD requires performing repetitive inspections for discrepancies of the heat pack rotor assembly and rotor drive clips of the brake unit of the main landing gear (MLG), and replacing the assembly if any discrepancy is found. This AD is prompted by reports of cracking and breakage of the heat pack rotor assemblies. We are issuing this AD to find and fix discrepancies of the heat pack rotor assembly of the brake unit of the MLG and consequent loss of braking capability, which could result in the airplane overrunning the runway during take-off or landing.
Airworthiness Directives; Honeywell International Inc., (Formerly AlliedSignal, Inc., Formerly Textron Lycoming) T5309, T5311, T5313B, T5317A, T5317A-1, and T5317B Series, and T53-L-9, T53-L-11, T53-L-13B, T53-L-13BA, T53-L-13B S/SA, T53-L-13B S/SB, T53-L-13B/D, and T53-L-703 Series Turboshaft Engines
Document Number: 05-4404
Type: Proposed Rule
Date: 2005-03-14
Agency: Federal Aviation Administration, Department of Transportation
The FAA is reopening the comment period of a proposed airworthiness directive (AD) for Honeywell International Inc., (formerly AlliedSignal, Inc., formerly Textron Lycoming) T5309, T5311, T5313B, T5317A, T5317A-1, and T5317B series turboshaft engines, installed on, but not limited to, Bell 205 and Kaman K-1200 series helicopters, and T53-L-9, T53-L-11, T53-L-13B, T53-L-13BA, T53-L-13B S/ SA, T53-L-13B S/SB, T53-L-13B/D, and T53-L-703 series turboshaft engines, installed on, but not limited to, Bell AH-1 and UH-1 helicopters, certified under Sec. 21.25 or 21.27 of the Code of Federal Regulations (14 CFR 21.25 or 14 CFR 21.27). The proposed AD would require operators to remove from service affected compressor, gas producer, and power turbine rotating components at reduced life limits, and would require use of replacement drawdown schedules for components on certain engine models that exceed the new limits. Since issuing the NPRM, we have determined that the comment period for NPRM, Docket No. FAA-2004-18038 (69 FR 33599, June 16, 2004) should be reopened and the public should have additional time to comment.
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