Federal Aviation Administration December 13, 2006 – Federal Register Recent Federal Regulation Documents

Special Conditions: Airbus Model A380-800 Airplane; Fire Protection
Document Number: E6-21191
Type: Rule
Date: 2006-12-13
Agency: Federal Aviation Administration, Department of Transportation
These special conditions are issued for the Airbus A380-800 airplane, which has novel and unusual design features, such as a full- length, double deck passenger cabin and electrical equipment bays distributed throughout the airplane. For these design features, the applicable airworthiness regulations do not contain adequate or appropriate safety standards regarding fire protection. These special conditions contain the additional safety standards that the Administrator considers necessary to establish a level of safety equivalent to that established by the existing airworthiness standards. Additional special conditions will be issued for other novel or unusual design features of the Airbus Model A380-800 airplane.
Special Conditions: Airbus Model A380-800 Airplane, Lithium Ion Battery Installation
Document Number: E6-21188
Type: Rule
Date: 2006-12-13
Agency: Federal Aviation Administration, Department of Transportation
These special conditions are issued for the Airbus A380-800 airplane. This airplane will have novel or unusual design features when compared to the state of technology envisioned in the airworthiness standards for transport category airplanes. The Airbus A380-800 will incorporate the use of high capacity lithium ion battery technology in on-board systems. For this design feature, the applicable airworthiness regulations do not contain adequate or appropriate safety standards regarding lithium ion batteries. These special conditions contain the additional safety standards that the Administrator considers necessary to establish a level of safety equivalent to that established by the existing airworthiness standards.
Airworthiness Directives; MT-Propeller Entwicklung GmbH Propellers
Document Number: E6-21184
Type: Proposed Rule
Date: 2006-12-13
Agency: Federal Aviation Administration, Department of Transportation
The FAA proposes to supersede an existing airworthiness directive (AD) for certain MT-Propeller Entwicklung GmbH variable pitch and fixed pitch propellers manufactured before 1995 which had not been overhauled since April 1994. That AD currently requires overhauling the propeller blades and performing initial and repetitive visual inspections of affected propeller blades. That AD also requires removing all propeller blades from service with damaged erosion sheath bonding or loose erosion sheaths and installing any missing or damaged polyurethane protective strips. This proposed AD would require the same actions. This proposed AD results from the need to clarify the population of affected propellers previously listed in AD 2006-05-05. We are proposing this AD to prevent erosion sheath separation leading to damage of the airplane.
Standard Instrument Approach Procedures; Miscellaneous Amendments
Document Number: E6-20941
Type: Rule
Date: 2006-12-13
Agency: Federal Aviation Administration, Department of Transportation
This amendment amends Standard Instrument Approach Procedures (SIAPs) for operations at certain airports. These regulatory actions are needed 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.
Standard Instrument Approach Procedures, Weather Takeoff Minimums; Miscellaneous Amendments
Document Number: E6-20919
Type: Rule
Date: 2006-12-13
Agency: Federal Aviation Administration, Department of Transportation
This amendment establishes, amends, suspends, or revokes Standard Instrument Approach Procedures (SIAPs) and/or Weather Takeoff Minimums 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.
Airworthiness Directives; General Electric Company (GE) CF6-80C2 Turbofan Engines
Document Number: 06-9674
Type: Proposed Rule
Date: 2006-12-13
Agency: Federal Aviation Administration, Department of Transportation
The FAA proposes to adopt a new airworthiness directive (AD) for GE CF6-80C2 series turbofan engines. This proposed AD would require replacing certain installed part number (P/N) and serial number (SN) cast titanium weld-repaired forward engine mount platforms and cast titanium forward mount yokes, with a forged titanium or a non-welded cast titanium part. This proposed AD results from the discovery of cracks, in a weld-repaired area on a forward engine mount platform and a forward engine mount yoke, found during a fluorescent penetrant inspection (FPI). These parts were weld-repaired during manufacture. We are proposing this AD to prevent cracks in the forward engine mount platform and forward engine mount yoke that could result in possible separation of the engine from the airplane.
Establishment of Class D Airspace; Eastman, GA; Correction
Document Number: 06-9662
Type: Rule
Date: 2006-12-13
Agency: Federal Aviation Administration, Department of Transportation
This document contains a correction to the final rule (FAA- 2006-25270; 06-ASO-9), which was published in the Federal Register on November 30, 2006 (71 FR 69191), establishing Class D airspace at Eastman, GA. This action corrects the effective date of the Class D airspace.
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