Federal Aviation Administration March 17, 2006 – Federal Register Recent Federal Regulation Documents

Airworthiness Directives; Sicma Aero Seat, Passenger Seat Assemblies
Document Number: E6-3908
Type: Proposed Rule
Date: 2006-03-17
Agency: Federal Aviation Administration, Department of Transportation
The FAA proposes to adopt a new airworthiness directive (AD) for certain Sicma Aero Seat, passenger seat assemblies. This proposed AD would require modifying the aft track fittings on these passenger seat assemblies by installing new tab locks, and then torquing the aft track fitting locking bolts. This proposed AD results from reports of loose and unlocked aft track fittings on Sicma Aero Seat, passenger seat assemblies. We are proposing this AD to prevent detachment of passenger seat assemblies, especially during emergency conditions, leading to occupant injury.
Airworthiness Directives: Rolls-Royce plc RB211 Trent 800 Series Turbofan Engines
Document Number: E6-3907
Type: Proposed Rule
Date: 2006-03-17
Agency: Federal Aviation Administration, Department of Transportation
This action withdraws a notice of proposed rulemaking (NPRM). That NPRM proposed a new airworthiness directive (AD) that applies to Rolls-Royce plc (RR) RB211 Trent 800 series turbofan engines. That proposed action would have required initial and repetitive borescope inspections of the high pressure-and-intermediate pressure (HP-IP) turbine internal and external oil vent tubes for coking and carbon buildup, and cleaning or replacing the vent tubes if necessary. Since we issued that NPRM, RR notified us that the RB211 Trent 800 series turbofan engines are significantly less susceptible to vent tube carbon build-up than the RB211 Trent 700 series turbofan engines. Repeat on- wing inspections therefore, are not required to maintain fleet safety. Accordingly, we withdraw the proposed rule.
Ameriflight, Inc.; Extension of Comment Period
Document Number: E6-3856
Type: Notice
Date: 2006-03-17
Agency: Federal Aviation Administration, Department of Transportation
This action reopens the comment period for a proposed grant of exemption that was published on February 7, 2006. The purpose of that document was to improve the public's awareness of, and participation in the FAA's regulatory activities. This reopening is a result of a request from the Air Line Pilots Association, International (ALPA) to extend the comment period to the exemption.
Proposed Modification of VOR Federal Airways; and Establishment of Area Navigation Route; NC
Document Number: E6-3852
Type: Proposed Rule
Date: 2006-03-17
Agency: Federal Aviation Administration, Department of Transportation
This action proposes to modify Very High Frequency Omnidirectional Range (VOR) Federal Airways V-56 and V-290, NC; and Colored Federal Airway G-13, NC; to remove unusable airway segments. The affected airway segments are unusable because they are based on nondirectional beacon (NDB) navigation aids that have been permanently decommissioned. In addition, the FAA proposes to establish a new low altitude area navigation (RNAV) route, designated T-243, to enhance instrument flight rules (IFR) access to the Outer Banks area of North Carolina.
IFR Altitudes; Miscellaneous Amendments
Document Number: 06-2585
Type: Rule
Date: 2006-03-17
Agency: Federal Aviation Administration, Department of Transportation
This amendment adopts miscellaneous amendments to the required IFR (instrument flight rules) altitudes and changeover points for certain Federal airways, jet routes, or direct routes for which a minimum or maximum en route authorized IFR altitude is prescribed. This regulatory action is needed because of changes occurring in the National Airspace System. These changes are designed to provide for the safe and efficient use of the navigable airspace under instrument conditions in the affected areas.
Standard Instrument Approach Procedures, Weather Takeoff Minimums; Miscellaneous Amendments
Document Number: 06-2584
Type: Rule
Date: 2006-03-17
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.
Standard Instrument Approach Procedures; Miscellaneous Amendments
Document Number: 06-2583
Type: Rule
Date: 2006-03-17
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.
Airworthiness Directives; Boeing Model 720 and 720B Series Airplanes
Document Number: 06-2545
Type: Rule
Date: 2006-03-17
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new airworthiness directive (AD) for all Boeing Model 720 and 720B series airplanes. This AD requires repetitive inspections for any crack, corrosion, or sign of damage (e.g., finish scratches, blistering, or signs of fuel leaking) of the front spar upper chords under the fairing web, and repair if necessary. This AD results from a report that inspections required by a previous AD action are inadequate for Boeing Model 720 and 720B series airplanes. We are issuing this AD to detect and correct any crack, corrosion, or sign of damage of the front spar upper chords under the fairing web, which could result in structural failure of the wing.
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