August 23, 2005 – Federal Register Recent Federal Regulation Documents

Results 151 - 159 of 159
Airworthiness Directives; Airbus Model A321 Series Airplanes
Document Number: 05-16458
Type: Rule
Date: 2005-08-23
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new airworthiness directive (AD) for certain Airbus Model A321 series airplanes. This AD requires repetitive measurements for correct control rod gap of the hold-open mechanism of all emergency doors, and corrective actions if necessary. This AD also requires replacing the control rods with new, improved control rods, which would terminate the repetitive measurements. This AD results from a report that an operator found it impossible to lock emergency doors 2 and 3 in the open position. We are issuing this AD to prevent failure of the emergency doors to lock in the open position, which could interfere with passenger evacuation during an emergency.
Airworthiness Directives; Airbus Model A320-111 Airplanes and Model A320-200 Series Airplanes
Document Number: 05-16457
Type: Rule
Date: 2005-08-23
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new airworthiness directive (AD) for certain Airbus Model A320-111 airplanes and Model A320-200 series airplanes. This AD requires doing a one-time general visual inspection of the axle nut on each main landing gear (MLG) wheel for the presence of locking bolts and associated hardware; doing any related investigative and corrective actions as applicable; and submitting an inspection report to the manufacturer. This AD results from a report that an axle nut had separated from an axle on a main landing gear (MLG) wheel, due to missing locking bolts. We are issuing this AD to detect and correct missing locking bolts on the axle nuts of the MLG wheels. Absence of the locking bolts could result in separation of a wheel(s) from the axle and consequent reduced controllability of the airplane during takeoff and landing, and possible injury to people on the ground.
Airworthiness Directives; Saab Model SAAB 2000 Airplanes
Document Number: 05-16456
Type: Rule
Date: 2005-08-23
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new airworthiness directive (AD) for certain Saab Model SAAB 2000 airplanes. This AD requires an inspection for cracking of the fastener holes in the front and rear spars, a modification of the fastener holes of the front and rear spars and the rear spar web, and related investigative/corrective actions if necessary. This AD is prompted by a report of cracking of certain fastener holes in the lower spar cap of the rear spar and in the lower skin at the front spar. We are issuing this AD to prevent cracking of the front and rear spars, which could result in fuel leakage and consequent reduced structural integrity of the wing structure.
Airworthiness Directives; Boeing Model 747, 757, 767 and 777 Series Airplanes
Document Number: 05-16455
Type: Rule
Date: 2005-08-23
Agency: Federal Aviation Administration, Department of Transportation
The FAA is superseding an existing airworthiness directive (AD), which applies to certain Boeing Model 747, 757, 767, and 777 series airplanes. That AD currently requires modifying certain drip shields located on the flight deck, and follow-on actions. This new AD removes certain airplanes that are included in the applicability statement of the existing AD, and requires modifying additional drip shields on the flight deck of certain other airplanes. This AD is prompted by a determination that certain airplanes have drip shields that are not adequately resistant to fire. We are issuing this AD to prevent potential ignition of the moisture barrier cover of the drip shield, which could propagate a small fire that results from an electrical arc, leading to a larger fire.
Airworthiness Directives; General Electric Company (GE) CF6-80C2 and CF6-80E1 Turbofan Engines
Document Number: 05-16454
Type: Rule
Date: 2005-08-23
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new airworthiness directive (AD) for certain GE CF6-80C2 and CF6-80E1 turbofan engines. This AD requires you to inspect the high pressure compressor rotor (HPCR) stage 11-14 spool shaft for circumferential repair cuts, and to repair or replace the spool shaft if you find certain circumferential cuts. This AD results from an updated stress analysis. We are issuing this AD to prevent failure of the HPCR stage 11-14 spool shaft due to low-cycle fatigue that could result in an uncontained engine failure.
Airworthiness Directives; Turbomeca Artouste III Series Turboshaft Engines
Document Number: 05-16453
Type: Rule
Date: 2005-08-23
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new airworthiness directive (AD) for Turbomeca Artouste III series turboshaft engines. This AD requires modification of the engine air intake assembly. This AD results from a report of an in-flight shutdown and subsequent loss of control of the helicopter due to ice ingestion into the engine. We are issuing this AD to prevent ice ingestion into the engine, which could lead to an in- flight shutdown and subsequent loss of control of the helicopter.
Airworthiness Directives; GROB-WERKE Model G120A Airplanes
Document Number: 05-16440
Type: Rule
Date: 2005-08-23
Agency: Federal Aviation Administration, Department of Transportation
This document incorporates corrections to add service information to Airworthiness Directive (AD) 2005-13-09, which was published in the Federal Register on June 22, 2005 (70 FR 35993). AD 2005-13-09 applies to certain GROB-WERKE Model G120A airplanes. This action adds GROB-WERKE Service Bulletin No. MSB1121-052/2, dated February 14, 2005, to paragraphs (e)(1), (e)(2), and (h) of AD 2005-13- 09. This service information was included in the notice of proposed rulemaking (NPRM) for this AD, but we inadvertently omitted it in the final rule request for comments. We are re-issuing the AD in its entirety to help eliminate any confusion that this AD may have created.
DoD Grant and Agreement Regulations
Document Number: 05-16417
Type: Rule
Date: 2005-08-23
Agency: Office of the Secretary, Department of Defense
The Department of Defense (DoD) is revising the DoD Grant and Agreement Regulations (DoDGARs) to implement four Office of Management and Budget (OMB) policy directives, to conform the DoDGARs with several statutory and regulatory revisions, and to make other administrative changes. The four OMB directives that are being implemented: require Federal agencies to use a new standard format for announcements of funding opportunities; require Federal agencies to electronically post synopses of those announcements at a Governmentwide Internet site; require Governmentwide use of the Data Universal Numbering System (DUNS) number as the universal identifier for recipient organizations; and amend OMB Circular A-B3 to raise the threshold of Federal funding at which recipients must obtain single audits. The statutory and regulatory changes with which the DoDGARs are being conformed concern matters such as nonprocurement debarment and suspension, drug-free workplace requirements for grants, and campus access for military recruiters and Reserve Officer Training Corps.
Endangered and Threatened Wildlife and Plants; Designation of Critical Habitat for the California Tiger Salamander, Central Population
Document Number: 05-16234
Type: Rule
Date: 2005-08-23
Agency: Fish and Wildlife Service, Department of the Interior
We, the U.S. Fish and Wildlife Service (Service), are designating critical habitat for the Central population of the California tiger salamander (Ambystoma californiense) pursuant to the Endangered Species Act of 1973, as amended (Act). In total, approximately 199,109 acres (ac) (80,576 hectares (ha)) fall within the boundaries of the critical habitat designation. The critical habitat is located within 19 counties in California.
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