Federal Aviation Administration 2005 – Federal Register Recent Federal Regulation Documents

Results 601 - 650 of 2,027
Establishment of Class E5 Airspace; Gardner, KS
Document Number: 05-18159
Type: Rule
Date: 2005-09-13
Agency: Federal Aviation Administration, Department of Transportation
This rule establishes a Class E surface area airspace area extending upward from 700 feet above the surface at Gardner, KS. The effect of this rule is to provide appropriate controlled Class E airspace for aircraft departing from and executing approach procedures to, Gardner Municipal Airport, KS and to segregate aircraft using instrument approach procedures in instrument conditions from aircraft operating in visual conditions.
Modification of Class E Airspace; Norfolk, NE; Correction
Document Number: 05-18158
Type: Rule
Date: 2005-09-13
Agency: Federal Aviation Administration, Department of Transportation
This action corrects a direct final rule; request for comments that was published in the Federal Register on Friday, July 29, 2005, (70 FR 43745) [FR Doc. 05-21872].
Modification of Class E Airspace; Lincoln, NE
Document Number: 05-18157
Type: Rule
Date: 2005-09-13
Agency: Federal Aviation Administration, Department of Transportation
This action corrects a direct final rule; request for comments that was published in the Federal Register on Friday, July 29, 2005 (70 FR 43741) [FR Doc. 05-21707].
RTCA Special Committee 147: Minimum Operational Performance Standards for Traffic Alert and Collision Avoidance Systems Airborne Equipment
Document Number: 05-18156
Type: Notice
Date: 2005-09-13
Agency: Federal Aviation Administration, Department of Transportation
The FAA is issuing this notice to advise the public of a meeting of RTCA Special Committee 147: Minimum Operational Performance Standards for Traffic Alert and Collision Avoidance Systems Airborne Equipment.
Establishment of Class E Airspace; Golovin, AK
Document Number: 05-18155
Type: Rule
Date: 2005-09-13
Agency: Federal Aviation Administration, Department of Transportation
This action establishes Class E airspace at Golovin, AK to provide adequate controlled airspace to contain aircraft executing two new Standard Instrument Approach Procedures (SIAPs) and one new departure procedure. This rule results in new Class E airspace upward from 700 feet (ft.) and 1,200 ft. above the surface at Golovin, AK.
Revision of Class E Airspace; Cordova, AK
Document Number: 05-18154
Type: Rule
Date: 2005-09-13
Agency: Federal Aviation Administration, Department of Transportation
This action revises Class E airspace at Cordova, AK to provide adequate controlled airspace to contain aircraft executing new and revised Standard Instrument Approach Procedures (SIAPs). This rule results in a revised Class E surface area and Class E airspace upward from 700 feet (ft.) and 1,200 ft. above the surface at Cordova, AK.
Revision of Class E Airspace; Prospect Creek, AK
Document Number: 05-18153
Type: Rule
Date: 2005-09-13
Agency: Federal Aviation Administration, Department of Transportation
This action revises Class E airspace at Prospect Creek, AK to provide adequate controlled airspace to contain aircraft executing Special Instrument Approach Procedures (SIAPs). This rule results in revised Class E airspace upward from 700 feet (ft.) above the surface at Prospect Creek, AK.
Availability of Changes to Advisory Circular 27-1B, Certification of Normal Category Rotorcraft, and Advisory Circular 29-2C, Certification of Transport Category Rotorcraft
Document Number: 05-18152
Type: Notice
Date: 2005-09-13
Agency: Federal Aviation Administration, Department of Transportation
This notice announces the availability of changes to AC 27-1B, Certification of Normal Category Rotorcraft, and AC 29-2C, Certification of Transport Category Rotorcraft for AC paragraphs 27.351 and AC 29.351B, Yawing Conditions. These AC paragraphs are final and replace the existing AC paragraphs dated 9/30/99. These AC paragraphs will be included in the upcoming Change 2 update.
Noise Exposure Map Notice
Document Number: 05-18151
Type: Notice
Date: 2005-09-13
Agency: Federal Aviation Administration, Department of Transportation
The Federal Aviation Administration (FAA) announces its determination that the noise exposure maps submitted by the City of Dayton for the Dayton International 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.
Establishment of Class E Airspace; Chehalis, WA
Document Number: 05-18146
Type: Rule
Date: 2005-09-13
Agency: Federal Aviation Administration, Department of Transportation
This final rule will establish Class E airspace at Chehalis, WA. This additional Class E airspace is necessary to accommodate the new Area Navigation (RNAV) Global Positioning System (GPS) Standard Instrument Approach Procedure (SIAP) at Chehalis-Centralia Airport. This change will improve the safety of Instrument Flight rules (IFR) aircraft executing the new RNAV GPS SIAP at Chehalis-Centralia Airport, Chelialis, WA.
Aviation Financing Reauthorization
Document Number: 05-18145
Type: Notice
Date: 2005-09-13
Agency: Federal Aviation Administration, Department of Transportation
The current taxes and fees paid into the Aviation Trust Fund, which provide funding for the National Aviation System, are only authorized through September 30, 2007. Since there is only a small and declining balance in the Trust Fund, it is critical that the financing not be allowed to lapse. The new financing structure should generate stable and predictable revenue, maintain the appropriate levels of service, and enable FAA to make long-term investments and tie revenues raised for the system to the infrastructure and operational costs of the system. The FAA has developed a series of data packages in examining FAA costs, paid for through the Trust Fund, from a managerial reporting standpoint. These packages will advance everyone's understanding of FAA costs and what the Agency faces as it considers a range of future funding options. They are available at https:// www.faa.gov/about /officeorg/ headquartersoffices/aep/aatf/.
Airworthiness Directives; BAe Systems (Operations) Limited Model ATP Airplanes
Document Number: 05-18059
Type: Rule
Date: 2005-09-13
Agency: Federal Aviation Administration, Department of Transportation
The FAA is superseding an existing airworthiness directive (AD), which applies to all BAe Systems (Operations) Limited Model ATP airplanes. That AD currently requires revising the Airworthiness Limitations Section (ALS) of the Instructions for Continued Airworthiness to incorporate life limits for certain items and inspections to detect fatigue cracking in certain structures. This new AD requires a revision to the ALS of the Instructions for Continued Airworthiness to incorporate new inspections to detect fatigue cracking of certain significant structural items (SSIs) and to revise life limits for certain equipment and various components. This AD is prompted by a determination that existing inspection techniques are not adequate for certain SSIs and by the revision of certain life limits. We are issuing this AD to detect and correct fatigue cracking of certain structural elements, which could adversely affect the structural integrity of these airplanes.
Airworthiness Directives; Raytheon Aircraft Company Models 1900, 1900C, 1900C (C-12J), and 1900D Airplanes
Document Number: 05-17890
Type: Rule
Date: 2005-09-13
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new airworthiness directive (AD) for certain Raytheon Aircraft Company Models 1900, 1900C, 1900C (C-12J), and 1900D airplanes. This AD requires you to inspect all elevator hinge support attachments on both left and right elevators for loose and missing rivets, replace rivets if loose or missing rivets are found, inspect the elevator hinge joints for looseness and clearance of each elevator to its stabilizer, correct looseness and clearance if incorrect, and report results of the required inspections. This AD results from a report of excessive movement of the elevator and elevator trim. The hinge support attachment that attaches the elevator to the horizontal stabilizer was loose and had loose and missing rivets. The elevator counterweight horn showed evidence of rubbing against the horizontal stabilizer, indicating possible incorrect clearance. We are issuing this AD to detect and correct any looseness in the elevator hinge support attachments, which could result in binding of the elevator control system. This elevator binding could lead to loss of control of the airplane.
Airworthiness Directives; Raytheon Aircraft Company Model 390 Premier 1 Airplanes
Document Number: 05-17889
Type: Rule
Date: 2005-09-13
Agency: Federal Aviation Administration, Department of Transportation
The FAA adopts a new airworthiness directive (AD) for certain Raytheon Aircraft Company (Raytheon) Premier 1 390 airplanes. This AD requires you to verify minimum clearances to correct chafing conditions in the powerplant left-hand and right-hand engine installations. This AD results from reports of inadequate left-hand and right-hand engine assembly cable, wire, and hose routing clearance. We are issuing this AD to detect and correct chafing conditions in the engine installation, which could result in leaking flammable fluids near an ignition source. This failure could lead to fire damage or loss of airplane control.
Public Notice for Waiver of Aeronautical Land-Use Assurance Bolton Field Airport, Columbus, OH
Document Number: 05-17989
Type: Notice
Date: 2005-09-12
Agency: Federal Aviation Administration, Department of Transportation
The Federal Aviation Administration (FAA) is considering a proposal to change a portion of the airport designated aeronautical use to non-aeronautical use and to authorize the release of 1.5411 acres of airport property for an exchange of property between the Columbus Regional Airport Authority (CRAA) and the City of Columbus. The land currently houses a fire station that will remain on the site. The land was conveyed to the City of Columbus in Deed Volume 2806, page 644 of the Recorder's Office, Franklin County, Ohio. The land was acquired by the City of Columbus with funding from Federal Grant 8-39-0026-01. There are no impacts to the airport by allowing the airport to dispose of the property. Approval does not constitute a commitment by the FAA to financially assist in the disposal of the subject airport property nor a determination of eligibility for grant-in-aid funding from the FAA. In exchange, the CRAA will receive a parcel of land (43.562 acres) currently being used as a golf course facility adjacent to Port Columbus International Airport. This parcel is partially located in the existing Runway Protection Zone for Runway 10R-28L and is partially located in the Runway Protection Zone for future Runway 10R-28L as indicated on the approved Airport Layout Plan (ALP) for Port Columbus International Airport. In accordance with section 47107(h) of title 49, United States Code, this notice is required to be published in the Federal Register 30 days before modifying the land-use assurance that requires the property to be used for an aeronautical purpose.
Airworthiness Directives; Airbus Model A300 B2 Series Airplanes, Model A300 B4 Series Airplanes, Model A310-200 Series Airplanes, Model A310-300 Series Airplanes, and Model A300 B4-600, B4-600R, and F4-600R Series Airplanes, and Model C4-605R Variant F Airplanes (Collectively Called A300-600 Series Airplanes)
Document Number: 05-17980
Type: Proposed Rule
Date: 2005-09-12
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 repetitive eddy current inspections for cracks of the stiffener fittings of the fuselage at frame (FR) 12A, and corrective actions if necessary. This proposed AD also provides a terminating action for the inspections. This proposed AD results from reports of cracks on the upper attachment fitting of the stiffener fitting at FR12A. We are proposing this AD to prevent failure of the stiffener fittings, which could result in the reduced structural integrity of the floor and rods around FR12A.
Airworthiness Directives; Boeing Model 747-100B SUD, 747-200B, 747-300, 747-400, and 747-400D Series Airplanes
Document Number: 05-17979
Type: Proposed Rule
Date: 2005-09-12
Agency: Federal Aviation Administration, Department of Transportation
The FAA proposes to adopt a new airworthiness directive (AD) for certain Boeing Model 747-100B SUD, 747-300, 747-400, and 747-400D series airplanes; and Model 747-200B series airplanes having a stretched upper deck. This proposed AD would require repetitively inspecting for cracking or discrepancies of the fasteners in the tension ties, shear webs, and frames at body stations 1120 through 1220, and related investigative and corrective actions if necessary. This proposed AD results from new reports of severed tension ties, as well as numerous reports of cracked tension ties, broken fasteners, and cracks in the frame, shear web, and shear ties adjacent to tension ties for the upper deck. We are proposing this AD to detect and correct cracking of the tension ties, shear webs, and frames of the upper deck, which could result in rapid decompression of the airplane.
Airworthiness Directives; Rolls-Royce plc RB211 Trent 875, 877, 884, 884B, 892, 892B, and 895 Series Turbofan Engines
Document Number: 05-17976
Type: Rule
Date: 2005-09-12
Agency: Federal Aviation Administration, Department of Transportation
The FAA is revising an existing airworthiness directive (AD) for Rolls-Royce plc (RR) RB211 Trent 875, 877, 884, 884B, 892, 892B, and 895 series turbofan engines with certain part number (P/N) low pressure compressor (LPC) fan blades installed. That AD currently requires initial and repetitive ultrasonic inspections of the fan blade dovetail roots and defines a specific terminating action to the repetitive blade inspection requirements. This AD requires the same actions but clarifies the terminating action. We are issuing this AD to prevent multiple LPC fan blade failures due to cracks, which could result in uncontained engine failure and possible damage to the airplane.
Petitions for Exemption; Dispositions of Petitions Issued
Document Number: 05-17909
Type: Notice
Date: 2005-09-09
Agency: Federal Aviation Administration, Department of Transportation
Pursuant to FAA's rulemaking provisions governing the application, processing, and disposition of petitions for exemption, part 11 of Title 14, Code of Federal Regulations (14 CFR), this notice contains the disposition of certain petitions previously received. The purpose of this notice is to improve the public's awareness of, and participation in, this aspect of FAA's regulatory activities. Neither publication of this notice nor the inclusion or omission of information in the summary is intended to affect the legal status of any petition or its final disposition.
Petitions for Exemption; Summary of Petitions Received
Document Number: 05-17908
Type: Notice
Date: 2005-09-09
Agency: Federal Aviation Administration, Department of Transportation
Pursuant to FAA's rulemaking provisions governing the application, processing, and disposition of petitions for exemption part 11 of Title 14, Code of Federal Regulations (14 CFR), this notice contains a summary of certain petitions seeking relief from specified requirements of 14 CFR. The purpose of this notice is to improve the public's awareness of, and participation in, this aspect of FAA's regulatory activities. Neither publication of this notice nor the inclusion or omission of information in the summary is intended to affect the legal status of any petition or its final disposition.
Second-in-Command Pilot Type Rating
Document Number: 05-17896
Type: Rule
Date: 2005-09-09
Agency: Federal Aviation Administration, Department of Transportation
The FAA is establishing a compliance date for the final rule published in the Federal Register on August 4, 2005. The rule revised the pilot certification regulations to establish a second-in-command (SIC) pilot type rating and associated qualifying procedures. This action is necessary to give affected pilots time to prepare and file the paperwork necessary to obtain the SIC pilot type rating. We also are correcting the amendment number of the final rule.
Airworthiness Directives; Engine Components Inc. (ECi) Reciprocating Engine Cylinder Assemblies
Document Number: 05-17893
Type: Proposed Rule
Date: 2005-09-09
Agency: Federal Aviation Administration, Department of Transportation
The FAA proposes to adopt a new airworthiness directive (AD) for Lycoming Engines (formerly Textron Lycoming) models 320, 360, and 540 series, ``Parallel Valve'' reciprocating engines, with certain Engine Components Inc. (ECi) cylinder assemblies, part number (P/N) AEL65102 series ``Classic Cast,'' installed. This proposed AD would require replacing these ECi cylinder assemblies. This proposed AD results from reports of about 30 failures of the subject cylinder assemblies marketed by ECi. We are proposing this AD to prevent loss of engine power due to cracks in the cylinder assemblies and possible engine failure caused by separation of a cylinder head.
Proposed Establishment of Class E Airspace; Nikolai, AK
Document Number: 05-17839
Type: Proposed Rule
Date: 2005-09-09
Agency: Federal Aviation Administration, Department of Transportation
This action proposes to establish Class E airspace at Nikolai, AK to the size necessary to contain aircraft executing Standard Instrument Approach Procedures (SIAP). This action is proposed as a result of the development of two new SIAPs. Adoption of this proposal would result in establishing Class E airspace upward from 700 feet (ft.) above the surface at Nikolai, Alaska.
Proposed Revision of Class E Airspace; Nenana, AK
Document Number: 05-17838
Type: Proposed Rule
Date: 2005-09-09
Agency: Federal Aviation Administration, Department of Transportation
This action proposes to revise Class E airspace at Nenana Municipal Airport, AK to the size necessary to contain aircraft executing Standard Instrument Approach Procedures (SIAP) and a Departure Procedure (DP). This action is needed as a result of runway renumbering due to changes in magnetic variation. Adoption of this proposal would result in revising Class E airspace upward from 700 feet (ft.) above the surface at Nenana Municipal Airport, Alaska.
Proposed Revision of Class E Airspace; Egegik, AK
Document Number: 05-17837
Type: Proposed Rule
Date: 2005-09-09
Agency: Federal Aviation Administration, Department of Transportation
This action proposes to revise Class E airspace at Egegik, AK to the size necessary to contain aircraft executing Standard Instrument Approach Procedures (SIAP). Adoption of this proposal would result in revising Class E airspace upward from 700 feet (ft.) above the surface at Egegik, Alaska.
Proposed Establishment of Class E Airspace; Arctic Village, AK
Document Number: 05-17836
Type: Proposed Rule
Date: 2005-09-09
Agency: Federal Aviation Administration, Department of Transportation
This action proposes to establish Class E airspace at Arctic Village, AK to the size necessary to contain aircraft executing two new Standard Instrument Approach Procedures (SIAP) and an Instrument Flight Rules (IFR) departure procedure. Adoption of this proposal would result in establishing Class E airspace upward from 700 feet (ft.) above the surface and from 1,200 ft. above the surface at Arctic Village, Alaska.
State Court Decision Affecting Recordation of Artisan Liens
Document Number: 05-17835
Type: Notice
Date: 2005-09-09
Agency: Federal Aviation Administration, Department of Transportation
Consistent with Agency policy, the Federal Aviation Administration (FAA) gives notice of the holding in Creation Aviation, Inc., vs. Textron Financial Corporation, Florida District Court of Appeal, Fourth District, No. 4D04-2178, decided on April 27, 2005. The Court in Creston held that Federal law pertaining to recording with the FAA Aircraft Registry did not preempt a Florida statute requiring that an artisan lien for work on an aircraft first be filed in the county where the work was performed in order to enforce the lien under Florida law. Accordingly, the FAA is advising the public that recording an artisan lien with the FAA Aircraft Registry only, may be insufficient to enforce an artisan lien under Florida law.
Modification of Class D and Class E Airspace; Salina Municipal Airport, KS
Document Number: 05-17834
Type: Rule
Date: 2005-09-09
Agency: Federal Aviation Administration, Department of Transportation
This action corrects an error in the legal description of Class D airspace in a direct final rule, request for comments that was published in the Federal Register on Friday July 29, 2005 (70 FR 43742).
Airworthiness Directives; Bombardier Model DHC-8-400 Series Airplanes
Document Number: 05-17779
Type: Rule
Date: 2005-09-09
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new airworthiness directive (AD) for certain Bombardier Model DHC-8-400 series airplanes. This AD requires a one-time inspection of the fuel and hydraulic tubes, and corrective actions if necessary. This AD also requires modifying fairlead plate assemblies. This AD results from reports of chafing between fuel and hydraulic tubes and the fairlead plate where the tubes pass through the firewall. We are issuing this AD to prevent chafing of the fuel and hydraulic tubes, which could lead to fuel and/or hydraulic fluid leakage in the engine nacelle area and consequent fire or explosion.
Airworthiness Directives; Goodrich De-icing and Specialty Systems “FASTprop” Propeller De-icers
Document Number: 05-17773
Type: Rule
Date: 2005-09-09
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new airworthiness directive (AD) for Goodrich De-icing and Specialty Systems ``FASTprop'' propeller de- icers, part numbers P4E1188 series, P4E1601 series, P4E2200 series, P4E2271-10, P4E2575-7, P4E2575-10, P4E2598-10, P5855BSW, P6199SW, P6592SW, P6662SW, and P6975-11, installed. This AD requires inspection, repair, or replacement of those ``FASTprop'' propeller de-icers that fail daily visual checks. This AD results from reports of Goodrich ``FASTprop'' propeller de-icers becoming loose or debonded, and detaching from propeller blades during operation.
Airworthiness Directives; Boeing Model 757 Airplanes
Document Number: 05-17772
Type: Rule
Date: 2005-09-09
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new airworthiness directive (AD) for certain Boeing Model 757 airplanes. This AD requires inspections of certain wire bundles in the left and right engine-to-wing aft fairings for discrepancies; installation of back-to-back p-clamps between the wire and hydraulic supply tube at the aft end of the right-hand strut only; and associated re-routing of the wire bundles, if necessary. This AD results from a report indicating that a circuit breaker for the fuel shutoff valve tripped due to a wire that chafed against the structure in the flammable leakage zone of the aft fairing, causing a short circuit. We are issuing this AD to prevent chafing between the wire bundle and the structure of the aft fairing, which could result in electrical arcing and subsequent ignition of flammable vapors and possible uncontrollable fire.
Airworthiness Directives; Fokker Model F27 Mark 200, 400, 500, and 600 Airplanes
Document Number: 05-17771
Type: Rule
Date: 2005-09-09
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new airworthiness directive (AD) for certain Fokker Model F27 Mark 200, 400, 500, and 600 airplanes. This AD requires a general visual inspection of the rotary knobs for the fuel tank isolation valves to determine if the seal wire has been installed correctly, and corrective actions if necessary. This AD results from investigation of a recent accident, which found that the rotary knobs controlling the fuel tank isolating valves had been in the shut position. We are issuing this AD to ensure that the rotary knobs are not inadvertently moved to the shut position, which could result in fuel starvation to both engines and consequent inability to maintain controlled flight and landing.
Airworthiness Directives; Boeing Model 777 Airplanes
Document Number: 05-17762
Type: Rule
Date: 2005-09-09
Agency: Federal Aviation Administration, Department of Transportation
This document publishes in the Federal Register an amendment adopting airworthiness directive (AD) 2005-18-51 that was sent previously to all known U.S. owners and operators of Boeing Model 777 airplanes by individual notices. This AD supersedes an existing AD that applies to certain Boeing Model 777-200 and ``300 series airplanes. The existing AD currently requires modification of the operational program software (OPS) of the air data inertial reference unit (ADIRU). This new AD requires installing a certain OPS in the ADIRU, and revising the airplane flight manual to provide the flightcrew with operating instructions for possible ADIRU heading errors and for potential incorrect display of drift angle. This AD results from a recent report of a significant nose-up pitch event. We are issuing this AD to prevent the OPS from using data from faulted (failed) sensors, which could result in anomalies of the fly-by-wire primary flight control, autopilot, auto-throttle, pilot display, and auto-brake systems. These anomalies could result in high pilot workload, deviation from the intended flight path, and possible loss of control of the airplane.
Airworthiness Directives; Hartzell Propeller Inc. Propellers
Document Number: 05-17667
Type: Rule
Date: 2005-09-09
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new airworthiness directive (AD) for certain Hartzell Propeller Inc. propellers. This AD requires inspecting the propeller blades and other critical propeller parts for corrosion and mechanical damage. This AD results from two events where a ``Z- shank'' blade failed and separated and the results of teardown inspections that detected corrosion in the blade bore. We are issuing this AD to detect corrosion and mechanical damage that can cause failure of a propeller, which could result in loss of control of the airplane.
Airworthiness Directives; Avions Marcel Dassault-Breguet Model Falcon 10 Airplanes
Document Number: 05-17598
Type: Rule
Date: 2005-09-09
Agency: Federal Aviation Administration, Department of Transportation
The FAA is superseding an existing airworthiness directive (AD) that applies to all Dassault Model Falcon 10 series airplanes. The existing AD currently requires revising the airplane flight manual (AFM) and installing a placard in the flight deck to prohibit flight into known or forecasted icing conditions. In lieu of the AFM revision and placard installation, that AD allows identifying the part number of each flexible hose in the wing (slat) anti-icing system, performing repetitive inspections of each hose for delamination, and performing corrective actions if necessary. This AD adds the following actions (also in lieu of the AFM revision and placard installation): New repetitive inspections for delamination at reduced intervals, corrective actions if necessary, and an additional AFM revision to include a statement to track flight cycles when the slat anti-icing system is activated. This AD also provides an option to repetitively replace the existing flexible hoses with improved flexible hoses, which terminates the repetitive inspection requirements. This AD results from a report of in-service delamination of a flexible hose in the slat anti-icing system at a time earlier than previously reported. We are issuing this AD to prevent collapse of the flexible hoses in the slat anti-icing system, which could lead to insufficient anti-icing capability and, if icing is encountered in this situation, could result in reduced controllability of the airplane.
Airworthiness Directives; General Electric Company CF34-3A1 Turbofan Engines
Document Number: 05-17761
Type: Rule
Date: 2005-09-08
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new airworthiness directive (AD) for General Electric Company (GE) CF34-3A1 turbofan engines installed on Bombardier series Regional Jets with certain high pressure turbine (HPT) rotating components installed. This AD requires removal from service of certain HPT components prior to the parts exceeding their designated life limits. This AD results from the discovery that the manufacturer removed certain part numbers of HPT rotating components from the Life Limits section of the CF34 Engine Manual, SEI-756. The effect of this manual change was the removal of life limits from certain components that are eligible for installation in GE CF34-3A1 engines. We are issuing this AD to impose life limits on these HPT rotating components to prevent low cycle fatigue (LCF) cracking and failure of those components, which could result in uncontained engine failure and damage to the airplane.
Notice of Availability of the Draft Environmental Impact Statement and DOT Section 4(f)/303(c) Evaluation for a Proposed Replacement Airport for the City of St. George, UT and Notice of Public Hearing Date, Time, and Location
Document Number: 05-17716
Type: Notice
Date: 2005-09-07
Agency: Federal Aviation Administration, Department of Transportation
The Federal Aviation Administration (FAA) is issuing this Notice of Availability to advise the public that a Draft Environmental Impact Statement (DEIS) containing a DOT Section 4(f)/303(c) evaluation will be available for public review beginning September 9, 2005. The DEIS details the proposed development of a replacement airport and related facilities for the city of St. George, Utah and addresses the environmental impacts associated with its development. The DEIS presents the purpose and need for the proposed project, a comprehensive analysis of the alternatives to the proposed project, and potential environmental impacts associated with the proposed development of the proposed replacement airport. The City of St. George, operator of the existing St. George Municipal Airport, has submitted an Airport Layout Plan, as revised, for approval. The DEIS assesses the potential impacts that may result from the development of a replacement airport with a 9,3000-foot Runway 01/19 and all support facilities (i.e., taxiways and associated lighting and NAVAIDS). This DEIS also assesses the federal action regarding installation of navigational aids, airspace use, approach and departure procedures, and associated terminal and landside projects. One historic site, the Little Black Mountain Petroglyph site, would potentially be affected. This document also assesses the potential noise impact on Zion National Park, Little Black Mountain Petroglyph site, and 42 other potentially noise sensitive properties in the vicinity. Public Comment and Information Meeting/Public Hearing: The public comment period on the DEIS and associated studies will start September 9, 2005 and will end on November 8, 2005. A Public Information Meeting and Public Hearing will be held on October 19, 2005 at The Dixie Center, 1835 Convention Center Drive, St. George, UT 84790. The Public Information Meeting will begin at 3 p.m. (MST) and will last until 7 p.m. (MST). The Public Hearing will be conducted concurrently with an information workshop. The public will be afforded the opportunity to present oral testimony and/or written testimony pertinent to the subject of the hearing. Testimony from an elected official, group or agency representative will be limited to 5 minutes. All others will be given 3 minutes. Forms for providing written comments will also be available at the Public Hearing. Comments received via fax or e-mail can only be accepted with the full name and address of the individual commenting. All comments are to be submitted to Mr. David Field of the FAA, at the address shown below, and the comments must be postmarked and email/fax must be sent by no later than midnight (MST), Tuesday, November 8, 2005. The DEIS may be reviewed for comment during regular business hours until November 8, 2005 at the following locations: 1. Cedar City Library, 303 North 100 East, Cedar City, UT 84720. 2. Hurricane Valley Branch, 36 South 300 West, Hurricane, UT 84737. 3. Santa Clara Branch, 1099 North Lava flow Drive, St. George, UT 84770. 4. Springdale Branch, 898 Zion Park Blvd, Spingdale, UT 84767-0509. 5. Washington County, 50 South Main, St. George, UT 84770. A limited number of copies of the DEIS and related documents will also be available for review by appointment only at the following FAA or City of St. George offices: 1. FAA, Northwest Mountain Region Office, 1601 Lind Avenue, S.W., Suite 315, Renton, WA 98055, (425) 227-2610. 2. FAA, Denver Airports District Office, 26805 East 68th Avenue, Suite 224, Denver, CO 80249, (303) 342-1254. 3. St. George Municipal Building, 175 East 200 North, St. George, UT 84770, (435) 634-5800. 4. St. George Airport, 620 S. Airport Road, St. George, UT 84770, (435) 634-5822. An electronic copy of the DEIS is available on the project Web site and can be accessed at https://www.airportsites.net/sgu-eis.
Airworthiness Directives; Boeing Model 767-200 and -300 Series Airplanes
Document Number: 05-17670
Type: Proposed Rule
Date: 2005-09-07
Agency: Federal Aviation Administration, Department of Transportation
The FAA proposes to adopt a new airworthiness directive (AD) for certain Boeing Model 767-200 and -300 series airplanes. This proposed AD would require replacing the placards on certain stowage bins with new placards, installing partial dividers in certain other stowage bins, and installing straps on stowage bins containing life rafts. For certain airplanes, this proposed AD would also require related concurrent actions. This proposed AD results from test data indicating that outboard overhead stowage bins are unable to withstand the 4.5g down-load standard intended to protect passengers during flight turbulence or a hard landing. We are proposing this AD to prevent the stowage bins from opening during flight turbulence or a hard landing, which could result in the contents of the stowage bins falling onto the passenger seats below and injuring passengers, or blocking the aisles, impeding the evacuation of passengers in an emergency.
Research, Engineering and Development Advisory Committee Meeting
Document Number: 05-17650
Type: Notice
Date: 2005-09-07
Agency: Federal Aviation Administration, Department of Transportation
Petitions for Exemption; Summary of Petitions Received
Document Number: 05-17649
Type: Notice
Date: 2005-09-07
Agency: Federal Aviation Administration, Department of Transportation
Pursuant to FAA's rulemaking provisions governing the application, processing, and disposition of petitions for exemption part 11 of Title 14, Code of Federal Regulations (14 CFR), this notice contains a summary of certain petitions seeking relief from specified requirements of 14 CFR, dispositions of certain petitions previously received, and corrections. The purpose of this notice is to improve the public's awareness of, and participation in, this aspect of FAA's regulatory activities. Neither publication of this notice nor the inclusion or omission of information in the summary is intended to affect the legal status of any petition or its final disposition.
Airworthiness Directives; Boeing Model 757-200 and -300 Series Airplanes and Model 767 Series Airplanes
Document Number: 05-17607
Type: Rule
Date: 2005-09-07
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new airworthiness directive (AD) for certain Boeing Model 757-200 and -300 series airplanes and Model 767 series airplanes. This AD requires replacing the existing operational software of the Pegasus flight management computer (FMC) system with new, improved operational software. This AD results from reports of ``old'' or expired air traffic control (ATC) clearance messages being displayed on the control display unit (CDU) of the FMC system during subsequent flights. We are issuing this AD to prevent display of ``old'' or expired ATC clearance messages on the CDU of subsequent flights, which could result in the airplane entering unauthorized airspace or following a flight path that does not provide minimum separation requirements between aircraft, and a consequent near miss or a mid-air collision.
Airworthiness Directives; Airbus Model A340-200 and A340-300 Series Airplanes
Document Number: 05-17606
Type: Rule
Date: 2005-09-07
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new airworthiness directive (AD) for certain Airbus Model A340-200 and A340-300 series airplanes. This AD requires a one-time inspection for discrepancies of the spotfacing for the pylon-to-engine attachment bolts on the pyramid forward fitting of the engine pylon, and repair if necessary. This AD results from a report that, during a routine inspection, it was found that the diameter of the spotfacings was too small for two of the pylon-to- engine attachment bolts on the pyramid forward fitting. We are issuing this AD to prevent reduced structural integrity of the pylon-to-engine attachment bolts on the pyramid forward fitting, which could result in separation of an engine from the airplane.
Airworthiness Directives; Israel Aircraft Industries, Ltd., Model 1124 and 1124A Airplanes
Document Number: 05-17600
Type: Rule
Date: 2005-09-07
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new airworthiness directive (AD) for all Israel Aircraft Industries, Ltd., Model 1124 and 1124A airplanes. This AD requires a one-time inspection for chafing of the electrical bundles in the overhead circuit breaker panel, and for adequate clearance between the fuselage frame and adjacent structures; and repair and rework if necessary. This AD results from reports of fire and smoke occurring in the passenger cabin. This AD also requires certain preventive actions. We are issuing this AD to prevent chafing of the electrical bundles in the overhead circuit breaker panel, which could result in a short circuit and consequent fire and smoke in the airplane.
Airworthiness Directives; Dassault Model Falcon 2000EX Airplanes
Document Number: 05-17599
Type: Rule
Date: 2005-09-07
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new airworthiness directive (AD) for certain Dassault Model Falcon 2000EX airplanes. This AD requires revising the airplane flight manual (AFM) to extend runway length limits for takeoff and landing. This AD also provides for an optional terminating action for the AFM revision. This AD results from an event in which braking efficiency was temporarily lost during landing, but was recovered after the flightcrew fully released and then reapplied the brakes. We are issuing this AD to prevent a runway overrun in the event of loss of braking function, which could result in injury to passengers or flightcrew and damage to the airplane.
Airworthiness Directives; BAE Systems (Operations) Limited (Jetstream) Model 4101 Airplanes
Document Number: 05-17610
Type: Proposed Rule
Date: 2005-09-06
Agency: Federal Aviation Administration, Department of Transportation
The FAA proposes to adopt a new airworthiness directive (AD) for all BAE Systems (Operations) Limited (Jetstream) Model 4101 airplanes. This proposed AD would require modifying the wiring of the starter-generator terminal block. This proposed AD results from a report of total electrical failure just as the airplane landed. We are proposing this AD to prevent total electrical failure and consequent reduced controllability of the airplane.
Airworthiness Directives; Boeing Model 747-100, 747-100B, 747-200B, 747-200C, 747-200F, 747-400F, 747SR, and 747SP Series Airplanes
Document Number: 05-17609
Type: Proposed Rule
Date: 2005-09-06
Agency: Federal Aviation Administration, Department of Transportation
The FAA proposes to adopt a new airworthiness directive (AD) for certain Boeing Model 747-100, 747-100B, 747-200B, 747-200C, 747- 200F, 747-400F, 747SR, and 747SP series airplanes, without a stretched upper deck or stretched upper deck modification. This proposed AD would require detailed and high-frequency eddy current inspections for cracks at the outboard ends of each affected tension tie and of the surrounding structure, and related investigative and corrective actions if necessary. This proposed AD results from a report of a crack in the tension tie at the body station 820 frame connection, and cracks found on the Boeing 747SR fatigue-test airplane in both the tension ties and frames at the tension tie to frame connections at body stations 800, 820, and 840. We are proposing this AD to find and fix cracks in the tension ties, which could lead to cracks in the skin and body frame and result in rapid in-flight depressurization of the airplane.
Airworthiness Directives; Boeing Model 747-400 Series Airplanes
Document Number: 05-17608
Type: Proposed Rule
Date: 2005-09-06
Agency: Federal Aviation Administration, Department of Transportation
The FAA proposes to adopt a new airworthiness directive (AD) for certain Boeing Model 747-400 series airplanes. This proposed AD would require doing a conductivity test of the upper deck floor beam at station 400 to identify the floor beam material. If the floor beam is manufactured from 7050 aluminum alloy, this proposed AD would also require inspecting the upper deck floor beam and certain fastener holes at the floor beam upper chord for cracking; repairing any cracking if necessary; and doing a preventative modification. This proposed AD results from several reports indicating that fatigue cracking was found in upper deck floor beams made from 7050 aluminum alloy. We are proposing this AD to find and fix cracking in the upper deck floor beam, which could extend and sever the floor beam. A severed floor beam could result in loss of controllability and rapid decompression of the airplane.
Notice of Intent to Request Renewal From the Office of Management and Budget (OMB) of Five Current Public Collections of Information
Document Number: 05-17572
Type: Notice
Date: 2005-09-06
Agency: Federal Aviation Administration, Department of Transportation
In compliance with the Paperwork Reduction Act (44 U.S.C. 3501 et seq.) the FAA invites public comment on five currently approved public information collections which will be submitted to OMB for renewal.
Establishment of Class D Airspace; Eau Claire, WI
Document Number: 05-17571
Type: Rule
Date: 2005-09-06
Agency: Federal Aviation Administration, Department of Transportation
This document establishes Class D airspace at Eau Clair, WI. A control tower is currently under construction at Chippewa Valley Regional Airport. Controlled airspace extending upward from the surface is required when the control tower is operational. This action establishes a radius of controlled airspace for Eau Clair, WI.
Modification of Class E Airspace; Washington, MO
Document Number: 05-17570
Type: Rule
Date: 2005-09-06
Agency: Federal Aviation Administration, Department of Transportation
This document confirms the effective date of the direct final rule which revises Class E airspace at Washington, MO.
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