Federal Aviation Administration March 18, 2005 – Federal Register Recent Federal Regulation Documents
Results 1 - 8 of 8
Standard Instrument Approach Procedures; Miscellaneous Amendments
This amendment establishes, amends, suspends, or revokes Standard Instrument Approach Procedures (SIAPs) for operations at certain airports. These regulatory actions are needed because of the adoption of new or revised criteria, or because of changes occurring in the National Airspace System, such as the commissioning of new navigational facilities, addition of new obstacles, or changes in air traffic requirements. These changes are designed to provide safe and efficient use of the navigable airspace and to promote safe flight operations under instrument flight rules at the affected airports.
Noise Exposure Map Notice: Receipt of Noise Compatibility Program and Request for Review
The Federal Aviation Administration (FAA) announces its determination that the noise exposure maps submitted by Capital Region Airport Authority for Capital City Airport under the provisions of 49 U.S.C. 47501 et seq. (Aviation Safety and Noise Abatement Act) and 14 CFR Part 150 are in compliance with applicable requirements. The FAA also announces that it is reviewing a proposed noise compatibility program that was submitted for Capital City Airport under Part 150 in conjunction with the noise exposure map, and that this program will be approved or disapproved on or before August 5, 2005.
Policy for Design Approval Procedures for Parts Manufacturer Approval of Critical Engine and Propeller Parts
The Federal Aviation Administration (FAA) announces the availability of policy for Design Approval Procedures for Parts Manufacturer Approval of Critical Engine and Propeller Parts.
Public Meeting With Interested Persons To Discuss the Proposed Federal Aviation Administration Policy (Draft Order 8110.RC) for the Certification of Restricted Category Aircraft
The FAA will hold three informational meetings to discuss the proposed policy (Draft Order 8110.RC) that the FAA's Aircraft Certification Service personnel, Flight Standards Service Personnel, persons designated by the Administrator, and organizations associated with the certification process required by Title 14 of the Code of Federal Regulations (14 CFR) will use during the certification evaluation of restricted category aircraft. These public meetings will be a continuation of information gathering for the evaluation of Restricted Category Aircraft Applications originally offered to the public for comments in the Federal Register, dated October 8, 2004, Page 60454 (Volume 69, Number 195). This meeting, the third and final public meeting will be held at the Federal Aviation Administration's (FAA) Orlando Florida's Flight Standards District Office, located at 5950 Hazeltine National Drive, Suite 500, Orlando, Florida. To obtain additional information and details about this meeting, please contact Mr. Graham Long via the information listed in the paragraph titled FOR FURTHER INFORMATION CONTACT. Notes from this informational meeting will be posted on the Internet at: https://www.faa.gov/Certification/ Aircraft/DraftDoc/Comments.htm.
Airworthiness Directives; McDonnell Douglas Model DC-8 Airplanes
The FAA is adopting a new airworthiness directive (AD) for all McDonnell Douglas Model DC-8 airplanes. This AD requires an inspection of the pushrod assemblies for the left and right elevator control tabs to determine if the pushrod assemblies are made of aluminum or steel, replacing any assembly made of aluminum with an assembly made of steel or modifying existing steel assemblies, and other specified actions. This AD also requires an inspection of the crank assemblies for the inboard and outboard geared tabs of the elevator to determine if the crank assemblies are made of aluminum or steel, replacing any assembly made of aluminum with an assembly made of steel, and other specified actions. This AD is prompted by an accident involving a DC-8 airplane. The probable cause of the accident was a loss of pitch control resulting from the disconnection of the pushrod for the right elevator control tab. The pushrod dropped down and jammed in front of the control tab crank, causing a large deflection of the control tab. We are issuing this AD to minimize the possibility of a control tab offset. A control tab offset could cause elevator deflection, an elevator airplane-nose-up condition, and reduced controllability of the airplane. This AD is also prompted by a report that the elevator on a McDonnell Douglas Model DC-8 airplane did not respond to command inputs from the flightcrew. We are also issuing this AD to minimize the possibility of crank assembly failure when the assembly is exposed to abnormal load conditions. Failure of a crank assembly could result in a jammed elevator and consequent reduced controllability of the airplane.
Airworthiness Directives; Airbus Model A319, A320, and A321 Series Airplanes
The FAA is adopting a new airworthiness directive (AD) for certain Airbus Model A319, A320, and A321 series airplanes. This AD requires modification of certain auxiliary power unit (APU) alternating current (AC) generators. This AD is prompted by a report of an explosion in the APU compartment, which blew open the compartment doors. We are issuing this AD to prevent oil vapor leakage from the APU AC generator, which, when combined with an electric arc at the electrical receptacle, could result in a fire or explosion in the APU compartment during flight.
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