June 27, 2005 – Federal Register Recent Federal Regulation Documents

Results 101 - 104 of 104
Airworthiness Directives; Airbus Model A300 B2 and B4 Series Airplanes
Document Number: 05-12505
Type: Rule
Date: 2005-06-27
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new airworthiness directive (AD) for certain Airbus Model A300 B2 and B4 series airplanes. This AD requires modifying the wiring of the autopilot pitch torque limiter switch. This AD is prompted by several reports of pitch trim disconnect caused by insufficient length in the wiring to the pitch torque limiter lever. We are issuing this AD to prevent possible trim loss when the flightcrew tries to override the autopilot pitch control, which could result in uncontrolled flight of the airplane.
Airworthiness Directives; Fokker Model F.28 Mark 1000, 2000, 3000, and 4000 Airplanes
Document Number: 05-12504
Type: Rule
Date: 2005-06-27
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new airworthiness directive (AD) for all Fokker Model F.28 Mark 1000, 2000, 3000, and 4000 airplanes. This AD requires a detailed inspection to determine the presence of incorrectly installed bushings in the attachment holes of the reinforcing strap of the left- and right-hand wings' lower skin, and corrective actions if necessary. This AD is prompted by a report that bushings were installed in accordance with improper procedures in the structural repair manual. We are issuing this AD to detect and correct improperly installed bushings, which could result in reduced tensile strength of the reinforcing strap of the wing's lower skin, and consequently a reduction of the structural capability of the wing and possible wing failure.
Airworthiness Directives; Boeing Model 737-100, -200, and -200C Series Airplanes
Document Number: 05-12503
Type: Rule
Date: 2005-06-27
Agency: Federal Aviation Administration, Department of Transportation
This amendment adopts a new airworthiness directive (AD), applicable to all Boeing Model 737-100, -200, and -200C series airplanes, that requires repetitive inspections to detect discrepancies of certain fuselage skin panels located just aft of the wheel well, and repair if necessary. The actions specified by this AD are intended to detect and correct fatigue cracking of the skin panels, which could cause rapid decompression of the airplane. This action is intended to address the identified unsafe condition.
Formations of, Acquisitions by, and Mergers of Bank Holding Companies
Document Number: 05-12496
Type: Notice
Date: 2005-06-27
Agency: Federal Reserve System, Agencies and Commissions
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