Federal Aviation Administration February 15, 2006 – Federal Register Recent Federal Regulation Documents

Proposed Revision of Class E Airspace; Middleton Island, AK
Document Number: E6-2190
Type: Proposed Rule
Date: 2006-02-15
Agency: Federal Aviation Administration, Department of Transportation
This action proposes to revise Class E airspace at Middleton Island, AK. Two Standard Instrument Approach Procedures (SIAPs) are being revised, and two SIAPs are being produced for the Middleton Island Airport. Adoption of this proposal would result in revision of Class E airspace upward from 700 feet (ft.) and 1,200 ft. above the surface at Middleton Island, AK.
Proposed Establishment of Class E Airspace; Ugnu-Kuparuk, AK
Document Number: E6-2186
Type: Proposed Rule
Date: 2006-02-15
Agency: Federal Aviation Administration, Department of Transportation
This action proposes to establish Class E airspace at Ugnu- Kuparuk, AK. Five Special Standard Instrument Approach Procedures (SIAPs) are being revised, and three Special SIAPs are being produced for the Ugnu-Kuparuk Airport. Adoption of this proposal would result in establishment of Class E airspace upward from 700 feet (ft.) above the surface at Ugnu-Kuparuk, AK.
Proposed Revision of Class E Airspace; Togiak, AK
Document Number: E6-2182
Type: Proposed Rule
Date: 2006-02-15
Agency: Federal Aviation Administration, Department of Transportation
This action proposes to revise Class E airspace at Togiak, AK. Two Standard Instrument Approach Procedures (SIAPs) are being revised and two SIAPs are being produced for the Togiak Airport. Adoption of this proposal would result in revision of Class E airspace upward from 700 feet (ft.) above the surface at Togiak, AK.
Reduction of Fuel Tank Flammability in Transport Category Airplanes
Document Number: E6-2181
Type: Notice
Date: 2006-02-15
Agency: Federal Aviation Administration, Department of Transportation
This notice announces the availability of and request for comments on the report, ``Assessment of the Effectiveness of Special Federal Aviation Regulation (SFAR) 88 Airworthiness Directives (ADs) in Preventing Ignition Sources.'' The FAA is making available this report, which supports its Notice of Proposed Rulemaking (NPRM) entitled ``Reduction of Fuel Tank Flammability in Transport Category Airplanes.'' The report can be found at the DOT Docket Web site, at https://dms.dot.gov, Docket No. FAA-2005-22997.
Proposed Establishment of Class E Airspace; Galbraith Lake, AK
Document Number: E6-2180
Type: Proposed Rule
Date: 2006-02-15
Agency: Federal Aviation Administration, Department of Transportation
This action proposes to establish Class E airspace at Galbraith Lake, AK. Two Standard Instrument Approach Procedures (SIAPs) are being published for the Galbraith Lake Airport. Adoption of this proposal would result in establishment of Class E airspace upward from 700 feet (ft.) above the surface at Galbraith Lake, AK.
FAA (Aircraft Certification Service) Information Sharing and Listening Session
Document Number: E6-2179
Type: Notice
Date: 2006-02-15
Agency: Federal Aviation Administration, Department of Transportation
This notice announces a meeting to discuss various FAA rotorcraft safety initiatives and to gather any relevant information that will help to reduce general aviation rotorcraft accidents. This meeting supports the FAA's Flight Plan initiative to reduce general aviation accidents.
Mode S Transponder Requirements in the National Airspace System
Document Number: E6-2178
Type: Proposed Rule
Date: 2006-02-15
Agency: Federal Aviation Administration, Department of Transportation
On October 7, 2005, the Federal Aviation Administration (FAA) published a document in the Federal Register announcing its long-term policy for Mode S transponder equipment requirements. The policy also sought comment on the proposed termination date of March 1, 2007, for operators currently exempted from the Mode S transponder requirement of 14 CFR parts 121 and 135. This action responds to the comments and adopts the proposed date for which all applicable exemptions will terminate.
Airworthiness Directives; McDonnell Douglas Model MD-10-10F and MD-10-30F Airplanes and Model MD-11 and MD-11F Airplanes
Document Number: E6-2176
Type: Proposed Rule
Date: 2006-02-15
Agency: Federal Aviation Administration, Department of Transportation
The FAA proposes to supersede an existing airworthiness directive (AD) that applies to certain McDonnell Douglas Model MD-11 series airplanes. The existing AD currently requires a revision of the airplane flight manual (AFM) to alert the flightcrew that both flight management computers (FMC) must be installed and operational. The existing AD also requires an inspection to determine the serial number of the FMCs; and follow-on corrective actions, if necessary, which terminate the AFM revision. The existing AD also requires an inspection to verify if a certain modification is on the identification plates of the FMCs; and applicable follow-on and corrective actions. This proposed AD would require installation of upgraded flight management computer software, which would terminate the existing AD. This proposed AD would also add airplanes to the applicability, including adding Model MD-10-10F and MD-10-30F airplanes. This proposed AD results from a report that the FMC does not acknowledge the pre-set glareshield control panel (GCP) altitude when profile (PROF) mode is engaged in descent mode. We are proposing this AD to prevent the un-commanded descent of an airplane below the selected level-off altitude, which could result in an unacceptable reduction in the separation between the airplane and nearby air traffic or terrain.
Airworthiness Directives; Dassault Model Falcon 900EX Airplanes
Document Number: E6-2175
Type: Proposed Rule
Date: 2006-02-15
Agency: Federal Aviation Administration, Department of Transportation
The FAA proposes to adopt a new airworthiness directive (AD) for certain Dassault Model Falcon 900EX airplanes. This proposed AD would require inspecting the number 2 engine left- and right-hand forward mounts for missing rivets and installing rivets if necessary. This proposed AD results from reports of two missing rivets in the front section of the central engine mast discovered on airplanes in service and in production. We are proposing this AD to detect and correct missing rivets in the front section of the central engine mast, which could result in reduced structural integrity of the central engine mast, possible separation of the engine from the airplane during flight, and consequent loss of control of the airplane.
Airworthiness Directives; Goodrich Evacuation Systems Approved Under Technical Standard Order (TSO) TSO-C69b and Installed on Airbus Model A330-200 and -300 Series Airplanes; Model A340-200 and -300 Series Airplanes; and Model A340-541 and -642 Airplanes
Document Number: E6-2173
Type: Proposed Rule
Date: 2006-02-15
Agency: Federal Aviation Administration, Department of Transportation
The FAA proposes to adopt a new airworthiness directive (AD) for Goodrich Evacuation Systems approved under TSO-C69b and installed on certain Airbus Model A330-200 and -300 series airplanes; Model A340- 200 and -300 series airplanes; and Model A340-541 and -642 airplanes. This proposed AD would require inspecting to determine the part number of the pressure relief valves on the affected Goodrich evacuation systems, and corrective action if necessary. This proposed AD results from a report indicating that, during maintenance testing, the pressure relief valves on the affected Goodrich evacuation systems did not seal when activated, which caused the pressure in the escape slide/raft to drop below the minimum allowable raft mode pressure. We are proposing this AD to prevent loss of pressure in the escape slides/rafts after an emergency evacuation, which could result in inadequate buoyancy to support the raft's passenger capacity during ditching, and increase the chance for injury to raft passengers.
Airworthiness Directives; Airbus Model A318-111 Airplanes; A319-100 Series Airplanes; A320-111 Airplanes; A320-200 Series Airplanes; and A321-100 and -200 Series Airplanes
Document Number: E6-2172
Type: Proposed Rule
Date: 2006-02-15
Agency: Federal Aviation Administration, Department of Transportation
The FAA proposes to adopt a new airworthiness directive (AD) for certain Airbus transport category airplanes. This proposed AD would require inspecting to determine the part number of the twin motor actuators, and related investigative and corrective actions if necessary. This proposed AD results from a report of a low pressure valve of the twin motor actuator found partially open, although the valve detection system indicated that the valve was closed. Investigation revealed that the locating pin in the actuator was too short to engage with the valve slot, resulting in incorrect alignment of the actuator and the drive assembly, causing the valve to remain partially open. We are proposing this AD to ensure that, in the event of an engine fire, the valve actuator functions properly to delay or block the fuel flow to the engine and prevent an uncontrollable fire.
Airworthiness Directives; Boeing Model 747 Airplanes
Document Number: E6-2170
Type: Proposed Rule
Date: 2006-02-15
Agency: Federal Aviation Administration, Department of Transportation
The FAA proposes to supersede an existing airworthiness directive (AD) that applies to all Boeing Model 747 series airplanes. The existing AD currently requires repetitive inspections for cracking of the top and side panel webs and panel stiffeners of the nose wheel well (NWW), and corrective actions if necessary. This proposed AD would reduce the interval for certain repetitive inspections and remove a certain optional inspection. This proposed AD would also require replacing the NWW side and top panels with new panels. The replacement would terminate the repetitive inspections. This proposed AD results from the development of a new modification. We are proposing this AD to prevent fatigue cracks in the top and side panel webs and stiffeners of the NWW, which could compromise the structural integrity of the NWW and could lead to the rapid decompression of the airplane.
Modification of the St. Louis Class B Airspace Area; MO
Document Number: 06-1429
Type: Rule
Date: 2006-02-15
Agency: Federal Aviation Administration, Department of Transportation, Docket No. Faa-2005-22509; Airspace Docket No. 03-Awa-2
This action modifies the St. Louis, MO, (STL) Class B airspace area to contain large, turbine-powered aircraft operations to and from the new Runway 11/29 at the Lambert-St. Louis International Airport (KSTL), St. Louis, MO. The FAA is taking this action to enhance safety and improve the management of aircraft operations in the KSTL terminal area. Further, this effort supports the FAA's national airspace redesign goal of optimizing terminal and en route airspace areas to reduce aircraft delays and improve system capacity.
Notice of Passenger Facility Charge (PFC) Approvals and Disapprovals
Document Number: 06-1428
Type: Notice
Date: 2006-02-15
Agency: Federal Aviation Administration, Department of Transportation
The FAA publishes a monthly notice, as appropriate, of PFC approvals and disapprovals under the provisions of the Aviation Safety and Capacity Expansion Act of 1990 (Title IX of the Omnibus Budget Reconciliation Act of 1990) (Pub. L. 101-508) and Part 158 of the Federal Aviation Regulations (14 CFR part 158). This notice is published pursuant to paragraph d of Sec. 158.29.
Establishment of High Altitude Area Navigation Routes; South Central United States
Document Number: 06-1427
Type: Rule
Date: 2006-02-15
Agency: Federal Aviation Administration, Department of Transportation
This action establishes 16 high altitude area navigation (RNAV) routes in the South Central United States in support of the High Altitude Redesign (HAR) program. The FAA is taking this action to enhance safety and to facilitate the more flexible and efficient use of the navigable airspace.
Notice of Intent To Rule on Application 05-04-C-00-BOS To Impose and Use the Revenue From a Passenger Facility Charge (PFC) at General Edward Lawrence Logan International Airport, East Boston, MA
Document Number: 06-1426
Type: Notice
Date: 2006-02-15
Agency: Federal Aviation Administration, Department of Transportation
The FAA proposes to rule and invites public comment on the application to impose and use the revenue from a PFC at General Edward Lawrence Logan International Airport under the provisions of the 49 U.S.C. 40117 and Part 158 of the Federal Aviation Regulations (14 CFR part 158).
Notice of Intent to Rule on Request to Release Airport Property at the City-County Airport, Madras, OR
Document Number: 06-1425
Type: Notice
Date: 2006-02-15
Agency: Federal Aviation Administration, Department of Transportation
The FAA proposed to rule and invite public comment on the release of land at City-County Airport under the provisions of Section 125 of the Wendell H. Ford Aviation Investment Reform Act for the 21st Century (AIR 21), now 49 U.S.C. 47107(h)(2).
Public Health Authority Notification
Document Number: 06-1424
Type: Notice
Date: 2006-02-15
Agency: Federal Aviation Administration, Department of Transportation
The FAA is publishing this notice to inform hospitals and other health care organizations of its status as a ``public health authority'' under the medical privacy requirements of the Health Insurance Portability and Accountability Act of 1996.
Airworthiness Directives; Bombardier Model CL-600-2C10 (Regional Jet Series 700, 701, & 702), CL-600-2D15 (Regional Jet Series 705), and CL-600-2D24 (Regional Jet Series 900) Airplanes
Document Number: 06-1295
Type: Rule
Date: 2006-02-15
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new airworthiness directive (AD) for certain Bombardier Model CL-600-2C10 (Regional Jet Series 700, 701, & 702), CL-600-2D15 (Regional Jet Series 705), and CL-600-2D24 (Regional Jet Series 900) airplanes. This AD requires repetitive inspections for cracking or fracturing of the output links of the power control unit (PCU) for the ailerons, and related investigative and corrective actions if necessary. This AD results from reports of fractured output links of the aileron PCU. We are issuing this AD to prevent failure of an output link of the aileron PCU, which, if both links on one aileron fail, could result in reduced lateral control of the airplane.
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