September 22, 2009 – Federal Register Recent Federal Regulation Documents

Results 151 - 159 of 159
Senior Executive Service; Financial Management Service Performance Review Board (PRB)
Document Number: E9-22649
Type: Notice
Date: 2009-09-22
Agency: Fiscal Service, Public Debt Bureau, Department of Treasury, Department of the Treasury
This notice announces the appointment of members to the Financial Management Service (EMS) Performance Review Board (PRB).
Office of Inspector General; Senior Executive Services (SES) Performance Review Board: Update
Document Number: E9-22637
Type: Notice
Date: 2009-09-22
Agency: Agency for International Development, Agencies and Commissions
This notice is hereby given of the appointment of members of the updated USAID OIG SES Performance Review Board.
Center for Scientific Review; Notice of Closed Meetings
Document Number: E9-22592
Type: Notice
Date: 2009-09-22
Agency: Department of Health and Human Services, National Institutes of Health
Endangered and Threatened Wildlife and Plants; Proposed Rule To List the Shovelnose Sturgeon as Threatened Due to Similarity of Appearance
Document Number: E9-22541
Type: Proposed Rule
Date: 2009-09-22
Agency: Fish and Wildlife Service, Department of the Interior
We, the U.S. Fish and Wildlife Service (Service or USFWS), propose to treat the shovelnose sturgeon (Scaphirhynchus platorynchus) as threatened under the ``Similarity of Appearance'' provisions of the Endangered Species Act of 1973, as amended (Act). The shovelnose sturgeon (Scaphirhynchus platorynchus) and the endangered pallid sturgeon (Scaphirhynchus albus) are difficult to differentiate in the wild and inhabit overlapping portions of the Missouri and Mississippi River basins. Four States where the two species commonly coexist allow for commercial fishing of shovelnose sturgeon which is in demand for its roe (eggs sold as caviar). The close resemblance in appearance between the two species creates substantial difficulty for fishermen, State regulators, and law enforcement personnel in differentiating between shovelnose and pallid sturgeon, both whole specimens and parts (including flesh and roe). This similarity of appearance has resulted in the documented take of pallid sturgeon and is a threat to the species. The determination that the shovelnose sturgeon should be treated as threatened due to similarity of appearance will substantially facilitate law enforcement actions to protect and conserve pallid sturgeon. We also propose a special rule to define activities that would and would not constitute take of shovelnose sturgeon under section 9 of the Act.
Airworthiness Directives; Teledyne Continental Motors O-470, IO-470, TSIO-470, IO-520, TSIO-520, IO-550, and IOF-550 Series Reciprocating Engines
Document Number: E9-22287
Type: Rule
Date: 2009-09-22
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new airworthiness directive (AD) for Teledyne Continental Motors (TCM) O-470, IO-470, TSIO-470, IO-520, TSIO-520, IO-550, and IOF-550 series reciprocating engines with TCM EQ3 cylinders installed. This AD requires initial and repetitive visual inspections of TCM EQ3 cylinders for cracks. This AD also requires removal of all EQ3 cylinders as terminating action to the repetitive visual inspections. This AD results from reports of 35 EQ3 cylinders found cracked. We are issuing this AD to prevent loss of engine power due to cracks in the cylinder head, possible engine failure, and fire in the engine compartment.
Airworthiness Directives; Boeing Model 747 Airplanes
Document Number: E9-21922
Type: Rule
Date: 2009-09-22
Agency: Federal Aviation Administration, Department of Transportation
We are adopting a new airworthiness directive (AD) for certain Boeing Model 747 airplanes. This AD requires repetitive inspections for cracking of the fuselage frames in section 41, and corrective actions if necessary. This AD results from reports of cracking in fuselage frames made of 2024 aluminum alloy that were installed during previous modification of the frames in section 41 and during production. We are issuing this AD to detect and correct frame cracks, which could result in cracking of the adjacent fuselage skin and consequent rapid decompression of the airplane.
Airworthiness Directives; McCauley Propeller Systems Propeller Models B5JFR36C1101/114GCA-0, C5JFR36C1102/L114GCA-0, B5JFR36C1103/114HCA-0, and C5JFR36C1104/L114HCA-0
Document Number: E9-21919
Type: Rule
Date: 2009-09-22
Agency: Federal Aviation Administration, Department of Transportation
The FAA is superseding an existing airworthiness directive (AD) for McCauley Propeller Systems propeller models B5JFR36C1101/ 114GCA-0, C5JFR36C1102/L114GCA-0, B5JFR36C1103/114HCA-0, and C5JFR36C1104/L114HCA-0. That AD currently requires initial and repetitive fluorescent penetrant inspections (FPI) and eddy current inspections (ECI) of propeller blades for cracks, and if any crack indications are found, removing the blade from service. That AD also mandates a life limit for the blades. This AD requires the same inspections, adds a visual inspection, and mandates a new propeller blade life limit. This AD also requires removing propeller blades with more than 10,000 operating hours time-since-new (TSN), before further flight. This AD also requires removal from service of all the propeller blades and the propeller hub if one or more propeller blades have been found cracked on a propeller assembly. This AD also requires removing from service all C-5963 split retainers. This AD results from eight reports of propeller blades found cracked since May of 2006. We are issuing this AD to detect cracks in the propeller blade that could cause failure and separation of the propeller blade and loss of control of the airplane.
Airworthiness Directives; Airbus Model A300, A310, and A300-600 Series Airplanes
Document Number: E9-21033
Type: Rule
Date: 2009-09-22
Agency: Federal Aviation Administration, Department of Transportation
The FAA is superseding an existing airworthiness directive (AD), which applies to certain Airbus Model A300 and A310 series airplanes. That AD currently requires replacement of the nose landing gear drag strut upper attachment pin. This new AD requires revising the Airworthiness Limitations section (ALS) of the Instructions for Continued Airworthiness (ICA) to require additional life limits and/or replacements for certain main landing gear and nose landing gear components, and also expands the applicability. This AD results from revisions to the ALS of the ICA to include new or more restrictive life limits and/or replacements. We are issuing this AD to ensure the continued structural integrity of these airplanes.
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