Federal Aviation Administration June 2005 – Federal Register Recent Federal Regulation Documents

Relief for U.S. Military and Civilian Personnel Who Are Assigned Outside the United States in Support of U.S. Armed Forces Operations
Document Number: 05-12930
Type: Rule
Date: 2005-06-30
Agency: Federal Aviation Administration, Department of Transportation
This final rule replaces Special Federal Aviation Regulation 100 (SFAR 100). SFAR 100 allowed Flight Standards District Offices (FSDO) to accept expired flight instructor certificates, expired inspection authorizations for renewals, and expired airman written test reports for certain practical tests from U.S. military and civilian personnel (U.S. personnel) who are assigned outside the United States in support of U.S. Armed Forces operations. This action is necessary to avoid penalizing these U.S. personnel who are unable to meet the regulatory time limits of their flight instructor certificate, inspection authorization, or airman written test report because they are serving outside the United States. The effect of this action is to give these U.S. personnel extra time to meet the eligibility requirements under the current rules.
Notice of Availability of an Environmental Assessment (EA) and Finding of No Significant Impact/Record of Decision (FONSI/ROD) Executed by the Federal Aviation Administration (FAA) for the Evaluation of Environmental Impacts Associated With a Proposed Extension of Runway 10R/28L for the Capital City Airport Located in Lansing, MI
Document Number: 05-12885
Type: Notice
Date: 2005-06-30
Agency: Federal Aviation Administration, Department of Transportation
The FAA is making available an EA and FONSI/ROD for the evaluation of environmental impacts associated with a proposed extension to runway 10R/28L executed by the FAA, for the Capital City Airport located in Lansing, Michigan. Point of Contact: Mr. Brad Davidson, Environmental Protection Specialist, FAA Great Lakes Region, Detroit Airports District Office, 11677 South Wayne Road, Suite 107, Romulus, MI 48174 (734) 229-2900.
Notice of Proposed Information Collection.
Document Number: 05-12884
Type: Notice
Date: 2005-06-30
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 one new public information collection which will be submitted to OMB for approval.
Special Conditions: Gulfstream Aerospace Limited Partnership (GALP) Model G150 Airplane; Windshield Coating in Lieu of Wipers
Document Number: 05-12883
Type: Proposed Rule
Date: 2005-06-30
Agency: Federal Aviation Administration, Department of Transportation
This notice proposes special conditions for the Gulfstream Aerospace Limited Partnership (GALP) Model G150 airplane. This airplane will have a novel or unusual design feature associated with use of a hydrophobic coating, rather than windshield wipers, as the means to maintain a clear portion of the windshield during precipitation conditions, as required by the airworthiness standards for transport category airplanes. The applicable airworthiness regulations do not contain adequate or appropriate safety standards for this design feature. These proposed 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.
Special Conditions; Diamond Aircraft Industries, EFIS and Full Authority Digital Engine Control (FADEC) on the Diamond DA-42; Protection of Systems for High Intensity Radiated Fields (HIRF)
Document Number: 05-12882
Type: Rule
Date: 2005-06-30
Agency: Federal Aviation Administration, Department of Transportation
These special conditions are issued to Diamond Aircraft Industries GmbH, N.A. Otto-Strasse 5, A-2700 Wiener Neistadt, Austria; telephone: 43 2622 26 700; facsimile: 43 2622 26 780, as part of the FAA Type Validation of the Diamond Aircraft Industries Model DA-42. This airplane will have novel and unusual design features when compared to the state of technology envisaged in the applicable airworthiness standards. These novel and unusual design features include the installation of a Garmin Model G-1000 electronic flight instrument system (EFIS) display, and digital engine controls. The applicable regulations do not contain adequate or appropriate airworthiness standards for the protection of these systems from the effects of high intensity radiated fields (HIRF). These special conditions contain the additional safety standards that the Administrator considers necessary to establish a level of safety equivalent to the airworthiness standards applicable to these airplanes.
Special Conditions; Raytheon Model King Air H-90 (T-44A) Protection of Systems for High Intensity Radiated Fields (HIRF)
Document Number: 05-12879
Type: Rule
Date: 2005-06-30
Agency: Federal Aviation Administration, Department of Transportation
These special conditions are issued to ARINC Inc., 1632 S. Murray Blvd., Colorado Springs, CO 80916 for a Supplemental Type Certificate for the Raytheon Model King Air H-90 (T-44A) airplane. These airplanes will have novel and unusual design features when compared to the state of technology envisaged in the applicable airworthiness standards. The novel and unusual design features include the installation of the Rockwell Collins Pro Line 21 Avionics System. This system includes Electronic Flight Instrument Systems (EFIS), electronic displays, digital Air Data Computers (ADC), and supporting equipment. The applicable regulations do not contain adequate or appropriate airworthiness standards for the protection of these systems from the effects of high intensity radiated fields (HIRF). These special conditions contain the additional safety standards that the Administrator considers necessary to establish a level of safety equivalent to the airworthiness standards applicable to these airplanes.
Airworthiness Directives; Boeing Model 727 Airplanes, Equipped With an Auxiliary Fuel Tank Having a Fuel Pump Installed
Document Number: 05-12844
Type: Rule
Date: 2005-06-30
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new airworthiness directive (AD) for Boeing Model 727 airplanes equipped with an auxiliary fuel tank having a fuel pump installed. This AD requires revising the airplane flight manual to include limitations on operating the fuel pumps for the auxiliary fuel tank. This AD is prompted by a design review of the fuel pump installation, which revealed a potential unsafe condition related to the auxiliary fuel tank(s). We are issuing this AD to prevent dry operation of the fuel pumps for the auxiliary fuel tank, which could create a potential ignition source inside the auxiliary fuel tank that could result in a fire or explosion of the auxiliary fuel tank.
Airworthiness Directives; Boeing Model 747 and 767 Airplanes
Document Number: 05-12840
Type: Proposed Rule
Date: 2005-06-29
Agency: Federal Aviation Administration, Department of Transportation
The FAA proposes to adopt a new airworthiness directive (AD) for certain Boeing Model 747 and 767 airplanes. This proposed AD would require reworking the electrical bonding between the airplane structure and the pump housing of the outboard boost pumps in the main fuel tank of certain Boeing Model 747 airplanes, and between the airplane structure and the pump housing of the override/jettison pumps in the left and right wing center auxiliary fuel tanks of certain Boeing Model 767 airplanes. This proposed AD would also require related investigative actions and corrective actions if necessary. This proposed AD is prompted by the results of fuel system reviews conducted by the manufacturer. We are proposing this AD to prevent insufficient electrical bonding, which could result in a potential of ignition sources inside the fuel tanks, and which, in combination with flammable fuel vapors, could result in fuel tank explosions and consequent loss of the airplane.
Airworthiness Directives; Airbus Model A330 and A340 Series Airplanes
Document Number: 05-12839
Type: Proposed Rule
Date: 2005-06-29
Agency: Federal Aviation Administration, Department of Transportation
The FAA proposes to adopt a new airworthiness directive (AD) for certain Airbus Model A330 and A340 series airplanes. This proposed AD would require repetitive borescope inspections of the left and right fuel tanks of the trimmable horizontal stabilizers (trim tanks) for detached or damaged float valves; related investigative/corrective actions if necessary; and the eventual replacement of all float valves in the left and right trim tanks with new, improved float valves, which terminates the need for the repetitive inspections. This proposed AD would also require repetitive replacement of certain new, improved float valves. This proposed AD is prompted by reports of detached and damaged float valves in the trim tanks. We are proposing this AD to prevent, in the event of a lightning strike to the horizontal stabilizer, sparking of metal parts and debris from detached and damaged float valves, or a buildup of static electricity, which could result in ignition of fuel vapors and consequent fire or explosion.
Airworthiness Directives; Fokker Model F27 Mark 200, 400, 500, and 600 Airplanes
Document Number: 05-12838
Type: Proposed Rule
Date: 2005-06-29
Agency: Federal Aviation Administration, Department of Transportation
The FAA proposes to adopt a new airworthiness directive (AD) for certain Fokker Model F27 Mark 200, 400, 500, and 600 airplanes. This proposed AD would require 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 proposed AD is prompted by 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 proposing 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.
Availability of Draft General Reevaluation Report and Supplemental Environmental Impact Statement for the Poplar Island Environmental Restoration Project, Talbot County, MD
Document Number: C5-12307
Type: Notice
Date: 2005-06-28
Agency: Department of Defense, Federal Aviation Administration, Department of Transportation, Department of the Army, Department of the Army, Corps of Engineers, Engineers Corps, Army Department
Airworthiness Directives; Cessna Aircraft Company Models 401, 401A, 401B, 402, 402A, 402B, 411, and 411A Airplanes
Document Number: C5-11612
Type: Rule
Date: 2005-06-28
Agency: Federal Aviation Administration, Department of Transportation
Establish Class D Airspace; Front Range Airport, Denver, CO
Document Number: 05-12725
Type: Rule
Date: 2005-06-28
Agency: Federal Aviation Administration, Department of Transportation
This rule will establish Class D airspace at Front Range Airport, Denver, CO. An Airport Traffic Control Tower (ATCT) is being constructed at Front Range Airport, Denver, CO, which will meet criteria for Class D airspace. Class D airspace is required when the ATCT is open, and to contain and protect Standard Instrument Approach Procedures (SIAPs) and other Instrument Flight Rules (IFR) operations at the airport. This action would establish Class D airspace extending upward from the surface to 8,000 feet Mean Sea Level (MSL) within a 5.1 nautical mile radius of the airport.
Petitions for Exemption; Dispositions of Petitions Issued
Document Number: 05-12724
Type: Notice
Date: 2005-06-28
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.
Advisory Circular (AC) 150/5345-53C, Airport Lighting Equipment Certification Program; Proposed Update and Opportunity To Comment
Document Number: 05-12723
Type: Notice
Date: 2005-06-28
Agency: Federal Aviation Administration, Department of Transportation
The FAA proposes to replace AC150/5345-53B to AC150/5345-53C to clarify the criteria under the Airport Lighting Equipment Certification Program (ALECP) for acceptance of an organization as a third party certification body (third party certifier) and how manufactures may get equipment qualified under the program. The Secretary of Transportation is providing notice in the Federal Register of, and an opportunity for public comment on, AC150/535-43C, Airport Lighting Equipment Certification Program.
Modification of Class E Airspace; Columbus, NE
Document Number: 05-12722
Type: Rule
Date: 2005-06-28
Agency: Federal Aviation Administration, Department of Transportation
This document confirms the effective date of the direct final rule which revises Class E airspace at Columbus, NE.
Modification of Class E Airspace; Mc Cook, NE
Document Number: 05-12721
Type: Rule
Date: 2005-06-28
Agency: Federal Aviation Administration, Department of Transportation
This action amends Title 14 Code of Federal Regulations, part 71 (14 CFR 71) by revising Class E airspace areas at Mc Cook, NE. A review of the Class E airspace surface area and the Class E airspace area extending upward from 700 feet above ground level (AGL) at Mc Cook, NE reveals neither area complies with criteria in FAA Orders nor reflects the current airport name. These airspace areas and their legal descriptions are modified to conform to the criteria in FAA Orders.
Special Conditions: Diamond Aircraft Industries, DA-42; Diesel Cycle Engine Using Turbine (Jet) Fuel
Document Number: 05-12720
Type: Rule
Date: 2005-06-28
Agency: Federal Aviation Administration, Department of Transportation
These special conditions are issued for the Diamond Aircraft Industries (DAI) DA-42 airplane. This airplane will have a novel or unusual design feature(s) associated with the installation of a diesel cycle engine utilizing turbine (jet) fuel. The applicable airworthiness regulations do not contain adequate or appropriate safety standards for installation of this new technology engine. 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.
Proposed Establishment of Class E5 Airspace; Gardner, KS
Document Number: 05-12719
Type: Proposed Rule
Date: 2005-06-28
Agency: Federal Aviation Administration, Department of Transportation
This notice proposes to establish Class E5 airspace at Gardner, KS.
Noise Exposure Map Notice; Orlando Sanford International Airport, Sanford, FL
Document Number: 05-12718
Type: Notice
Date: 2005-06-28
Agency: Federal Aviation Administration, Department of Transportation
The Federal Aviation Administration (FAA) announces its determination that the noise exposure maps submitted by Sanford Airport Authority for Orlando Sanford 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.
Notice of Intent To Rule on Application 05-12-C-00-MKE To Impose a Passenger Facility Charge (PFC) at General Mitchell International Airport and To Use the Revenue at General Mitchell International Airport and Lawrence J. Timmerman Airport, Milwaukee, WI
Document Number: 05-12717
Type: Notice
Date: 2005-06-28
Agency: Federal Aviation Administration, Department of Transportation
The FAA proposes to rule and invites public comment on the application to impose a PFC at General Mitchell International Airport and to use the revenue at General Mitchell International Airport and Lawrence J. Timmerman Airport under the provisions of the 49 U.S.C. 40117 and Part 158 of the Federal Aviation Regulations (14 CFR Part 158).
Airworthiness Directives; Turbomeca Arriel 1B, 1D, 1D1 and 1S1 Turboshaft Engines
Document Number: 05-12692
Type: Proposed Rule
Date: 2005-06-28
Agency: Federal Aviation Administration, Department of Transportation
The Federal Aviation Administration (FAA) proposes to adopt a new airworthiness directive (AD) that is applicable to certain Turbomeca Arriel 1B, 1D, 1D1 and 1S1 turboshaft engines. This proposal would require initial and repetitive position checks of the gas generator 2nd stage turbine blades on all Turbomeca Arriel 1B, 1D, 1D1 and 1S1 turboshaft engines, and replacement of 2nd stage turbines on 1B and 1D1 engines only. This proposal is prompted by the release of gas generator 2nd stage turbine blades while in service, with full containment of debris. We are proposing this AD to prevent an uncommanded engine in flight shutdown.
Airworthiness Directives; Bell Helicopter Textron Canada Model 206A, A-1, B, B-1, L, L-1, L-3, L-4 Helicopters
Document Number: 05-12690
Type: Proposed Rule
Date: 2005-06-28
Agency: Federal Aviation Administration, Department of Transportation
This document proposes adopting a new airworthiness directive (AD) for the specified Bell Helicopter Textron Canada (BHTC) model helicopters. This proposal would require, before the first flight of each day, checking the tail rotor blade (blade) root doublers (doublers) for an edge void or de-bond on both sides of each blade, and if an edge void or de-bond is found, replacing the unairworthy blade with an airworthy blade. This proposal would also require replacing any affected serial-numbered blade with an airworthy blade. This proposal is prompted by reports of de-bond of the doublers due to inadequate surface preparation resulting in poor adherence of the doublers. The actions specified by this proposed AD are intended to prevent loss of a blade, loss of tail rotor control, and subsequent loss of control of the helicopter.
Airworthiness Directives; Robinson Helicopter Company Model R22 Series Helicopters
Document Number: 05-12688
Type: Proposed Rule
Date: 2005-06-28
Agency: Federal Aviation Administration, Department of Transportation
This document proposes adopting a new airworthiness directive (AD) for the Robinson Helicopter Company (RHC) Model R22 series helicopters. The AD would require replacing each main rotor blade (blade) droop and teeter stop (stop) and teeter stop bracket (bracket) and associated hardware with redesigned and improved airworthy parts. This proposal is prompted by an in-flight break up of a helicopter on which both brackets failed. The actions specified by the proposed AD are intended to prevent failure of the stops and brackets, blade contact with the airframe, and subsequent loss of control of the helicopter.
Airworthiness Directives; The Lancair Company Model LC41-550FG Airplanes
Document Number: 05-12676
Type: Rule
Date: 2005-06-28
Agency: Federal Aviation Administration, Department of Transportation
This document makes a correction to Airworthiness Directive (AD) 2005-12-20, which was published in the Federal Register on June 20, 2005 (70 FR 35370), and applies to certain The Lancair Company (Lancair) Model LC41-550FG airplanes. We incorrectly referenced the affected airplane model as LC41-550F in the applicability section. The correct airplane model is LC41-550FG. This action corrects the regulatory text.
Airworthiness Directives; Boeing Model 777-200 and -300 Series Airplanes
Document Number: 05-12635
Type: Rule
Date: 2005-06-28
Agency: Federal Aviation Administration, Department of Transportation
This amendment adopts a new airworthiness directive (AD), applicable to certain Boeing Model 777-200 and -300 series airplanes, that requires replacing existing ceiling and sidewall light connectors in the passenger cabin with new connectors, and follow-on actions. This action is necessary to prevent overheating of the light connectors, which could result in smoke and a possible fire in the passenger cabin. This action is intended to address the identified unsafe condition.
Airworthiness Directives; BAE Systems (Operations) Limited Model BAe 146 and Avro 146-RJ Series Airplanes
Document Number: 05-12511
Type: Rule
Date: 2005-06-28
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new airworthiness directive (AD) for all BAE Systems (Operations) Limited Model BAe 146 and Avro 146-RJ series airplanes. This AD requires repetitive external eddy current inspections of the forward fuselage skin to detect cracking due to fatigue, and repair if necessary. This AD is prompted by evidence of cracking due to fatigue along the edges of the chemi-etched pockets in certain front fuselage canopy skin panels. We are issuing this AD to detect and correct this cracking, which could result in reduced structural integrity of the airplane fuselage.
Airworthiness Directives; Short Brothers Model SD3-60 Airplanes
Document Number: 05-12508
Type: Rule
Date: 2005-06-28
Agency: Federal Aviation Administration, Department of Transportation
This amendment adopts a new airworthiness directive (AD), applicable to all Short Brothers Model SD3-60 airplanes, that requires performing repetitive inspections of the shear attachment fittings of the vertical stabilizer for corrosion, and performing corrective actions if necessary. The actions specified by this AD are intended to detect and correct corrosion in the area of the main spar web fittings of the vertical stabilizer, which could result in reduced structural integrity of the vertical stabilizer. This action is intended to address the identified unsafe condition.
High Density Airports; Notice of Extension of the Lottery Allocation and Amended Policy for Reallocation Procedures for Slot Exemptions at LaGuardia Airport
Document Number: 05-12716
Type: Notice
Date: 2005-06-27
Agency: Federal Aviation Administration, Department of Transportation
The FAA is extending by fourteen months the current allocation of slot exemptions at LaGuardia Airport (LaGuardia) through December 31, 2006. This action maintains the current limit on scheduled operations at LaGuardia pending the adoption of a long-term solution for congestion management and the expiration of the High Density Traffic Airports Rule (High Density Rule) at LaGuardia on January 1, 2007. We also are amending the lottery reallocation procedures at LaGuardia in response to a petition submitted by Northwest Airlines, Inc. (Northwest). Air carriers that do not currently serve small hub/ non-hub airports from LaGuardia can now participate in any reallocation of AIR-21 slot exemptions that are returned to the FAA or become available through non-use.
Airworthiness Directives; Bombardier Model CL-600-2B19 (Regional Jet Series 100 & 440) Airplanes
Document Number: 05-12637
Type: Proposed Rule
Date: 2005-06-27
Agency: Federal Aviation Administration, Department of Transportation
This document revises an earlier proposed airworthiness directive (AD), applicable to certain Bombardier Model CL-600-2B19 (Regional Jet Series 100 & 440) airplanes, that would have required performing repetitive inspections of the electrical harnesses of the spoiler and the brake pressure sensor unit on both sides of the wing root to detect any chafing or wire damage, and repairing or replacing any damaged or chafed harness or wire with a new harness, as applicable. This new action revises the proposed rule by expanding the applicability to include additional airplanes, deleting the repetitive inspections, and by adding a terminating modification for the one-time inspection. The actions specified by this new proposed AD are intended to detect and correct chafing of the electrical cables of the spoiler and brake pressure sensor unit on both sides of the wing root, which could result in loss of flight control system and consequent reduced controllability of the airplane. This action is intended to address the identified unsafe condition.
Airworthiness Directives; Boeing Model 737-300, -400, and -500 Series Airplanes
Document Number: 05-12514
Type: Rule
Date: 2005-06-27
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new airworthiness directive (AD) for certain Boeing Model 737-300, -400, and -500 series airplanes. This AD requires repetitive inspections for cracking of the crown area of the fuselage skin, and corrective actions if necessary. This AD is prompted by a Model 737 fuselage structure test and fatigue analysis that indicate fuselage skin cracking could occur between 21,000 and 42,000 total flight cycles. We are issuing this AD to detect and correct fatigue cracking of the fuselage skin, which could cause the fuselage skin to fracture and fail, and could result in rapid decompression of the airplane.
Airworthiness Directives; McDonnell Douglas Model DC-9-10 Series Airplanes; Model DC-9-20 Series Airplanes; Model DC-9-30 Series Airplanes; Model DC-9-40 Series Airplanes; Model DC-9-50 Series Airplanes; Model DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83), and DC-9-87 (MD-87) Airplanes; and Model MD-88 Airplanes
Document Number: 05-12513
Type: Rule
Date: 2005-06-27
Agency: Federal Aviation Administration, Department of Transportation
The FAA is superseding an existing airworthiness directive (AD), which applies to certain SAFT America Inc. part number (P/N) 021929-000 (McDonnell Douglas P/N 43B034LB02) and P/N 021904-000 (McDonnell Douglas P/N 43B034LB03) nickel cadmium batteries. That AD currently requires replacing all battery terminal screws, verifying that the battery contains design specification cells, and replacing the cells if the battery contains non-design specification cells. This new AD requires an inspection for certain nickel cadmium batteries and, if necessary, replacing battery terminal screws with new hex head bolts and adding shims. This AD is prompted by a report of battery screws shearing off while under normal torque loads. We are issuing this AD to prevent internal shorting, arcing, and loss of emergency battery power due to failed battery screws, which could result in loss of emergency power to electrical flight components or other emergency power systems required in the event of loss of the aircraft primary power source.
Airworthiness Directives; Airbus Model A300 B2 and B4 Series Airplanes; Model A300 B4-600, B4-600R, and F4-600R Series Airplanes, and Model C4-605R Variant F Airplanes (Collectively Called A300-600 Series Airplanes); and Model A310-200 and -300 Series Airplanes
Document Number: 05-12512
Type: Rule
Date: 2005-06-27
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new airworthiness directive (AD) for certain Airbus models, as specified above. This AD requires installing safety signs on all passenger/crew doors, emergency exit doors, and cargo compartment doors. This AD is prompted by a report of injuries occurring on in-service airplanes when crewmembers forcibly initiated opening of passenger/crew doors against residual pressure causing the doors to rapidly open. We are issuing this AD to ensure that crewmembers are informed of the risks associated with forcibly opening passenger/crew, emergency exit, and cargo doors before an airplane is fully depressurized, which will prevent injury to crewmembers, and subsequent damage to the airplane caused by the rapid opening of the door.
Airworthiness Directives; Boeing Model 777-200 and -300 Series Airplanes
Document Number: 05-12510
Type: Rule
Date: 2005-06-27
Agency: Federal Aviation Administration, Department of Transportation
This amendment adopts a new airworthiness directive (AD), applicable to certain Boeing Model 777-200 and -300 series airplanes. This AD requires a one-time inspection of the clevis end of the vertical tie rods that support the center stowage bins to measure the exposed thread, installation of placards that advise of weight limits for certain electrical racks, a one-time inspection and records check to determine the amount of weight currently installed in those electrical racks, corrective actions, and replacement of the vertical tie rods for the center stowage bins or electrical racks with new improved tie rods, as applicable. The actions specified by this AD are intended to prevent failure of the vertical tie rods supporting certain electrical racks and the center stowage bins, which could cause the center stowage bins or electrical racks to fall onto passenger seats below during an emergency landing, impeding an emergency evacuation or injuring passengers. This action is intended to address the identified unsafe condition.
Airworthiness Directives; Boeing Model 777-200 and -300 Series Airplanes
Document Number: 05-12509
Type: Rule
Date: 2005-06-27
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new airworthiness directive (AD) for certain Boeing Model 777-200 and -300 series airplanes. This AD requires inspecting for the installation of the tie plate for the wire bundles routed from lower section 41 into the center control stand in the flight deck; inspecting for any wire chafing or damage and repair if necessary; and installing a tie plate if necessary. This AD is prompted by a report of missing tie plates for the wire bundles. We are issuing this AD to prevent wire chafing, which could result in the loss of flight control, communication, navigation, and engine fire control systems. Loss of these systems could consequently result in a significant reduction of safety margins, an increase in flight crew workload, and in the case where loss of engine fire control is combined with an engine fire, could result in an uncontrollable fire.
Airworthiness Directives; Airbus Model A300 B2 and B4 Series Airplanes
Document Number: 05-12505
Type: Rule
Date: 2005-06-27
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new airworthiness directive (AD) for certain Airbus Model A300 B2 and B4 series airplanes. This AD requires modifying the wiring of the autopilot pitch torque limiter switch. This AD is prompted by several reports of pitch trim disconnect caused by insufficient length in the wiring to the pitch torque limiter lever. We are issuing this AD to prevent possible trim loss when the flightcrew tries to override the autopilot pitch control, which could result in uncontrolled flight of the airplane.
Airworthiness Directives; Fokker Model F.28 Mark 1000, 2000, 3000, and 4000 Airplanes
Document Number: 05-12504
Type: Rule
Date: 2005-06-27
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new airworthiness directive (AD) for all Fokker Model F.28 Mark 1000, 2000, 3000, and 4000 airplanes. This AD requires a detailed inspection to determine the presence of incorrectly installed bushings in the attachment holes of the reinforcing strap of the left- and right-hand wings' lower skin, and corrective actions if necessary. This AD is prompted by a report that bushings were installed in accordance with improper procedures in the structural repair manual. We are issuing this AD to detect and correct improperly installed bushings, which could result in reduced tensile strength of the reinforcing strap of the wing's lower skin, and consequently a reduction of the structural capability of the wing and possible wing failure.
Airworthiness Directives; Boeing Model 737-100, -200, and -200C Series Airplanes
Document Number: 05-12503
Type: Rule
Date: 2005-06-27
Agency: Federal Aviation Administration, Department of Transportation
This amendment adopts a new airworthiness directive (AD), applicable to all Boeing Model 737-100, -200, and -200C series airplanes, that requires repetitive inspections to detect discrepancies of certain fuselage skin panels located just aft of the wheel well, and repair if necessary. The actions specified by this AD are intended to detect and correct fatigue cracking of the skin panels, which could cause rapid decompression of the airplane. This action is intended to address the identified unsafe condition.
Revision of Class E Airspace; Shishmaref, AK
Document Number: 05-12568
Type: Rule
Date: 2005-06-24
Agency: Federal Aviation Administration, Department of Transportation
This action revises Class E airspace at Shishmaref, AK to provide adequate controlled airspace to contain aircraft executing two new Standard Instrument Approach Procedures (SIAPs). This Rule results in new Class E airspace upward from 700 feet (ft.) and 1,200 ft. above the surface at Shishmaref, AK.
Establishment of Class E Airspace; Kaltag, AK
Document Number: 05-12567
Type: Rule
Date: 2005-06-24
Agency: Federal Aviation Administration, Department of Transportation
This action establishes Class E airspace at Kaltag, AK to provide adequate controlled airspace to contain aircraft executing two new Standard Instrument Approach Procedures (SIAPs) and two new departure procedures. This rule results in new Class E airspace upward from 700 feet (ft.) and 1,200 ft. above the surface at Kaltag, AK.
Revision of Class E Airspace; Emmonak, AK
Document Number: 05-12566
Type: Rule
Date: 2005-06-24
Agency: Federal Aviation Administration, Department of Transportation
This action revises Class E airspace at Emmonak, AK to provide adequate controlled airspace to contain aircraft executing amended Standard Instrument Approach Procedures (SIAPs). This rule results in new Class E airspace upward from 700 feet (ft.) above the surface at Emmonak, AK.
Establishment of Class E Airspace; Coldfoot, AK
Document Number: 05-12565
Type: Rule
Date: 2005-06-24
Agency: Federal Aviation Administration, Department of Transportation
This action establishes Class E airspace at Coldfoot, AK to provide adequate controlled airspace to contain aircraft executing two new Standard Instrument Approach Procedures (SIAPs) and a new departure procedure. This rule results in new Class E airspace upward from 700 feet (ft.) above the surface at Coldfoot, AK.
Establishment of Class E Airspace; Chalkyitsik, AK
Document Number: 05-12564
Type: Rule
Date: 2005-06-24
Agency: Federal Aviation Administration, Department of Transportation
This action establishes Class E airspace at Chalkyitsik, AK to provide adequate controlled airspace to contain aircraft executing two new Standard Instrument Approach Procedures (SIAPs). This rule results in new Class E airspace upward from 700 feet (ft.) and 1,200 ft. above the surface at Chalkyitsik, AK.
Establishment of Class E Airspace; Bob Baker Memorial Airport, Kiana, AK
Document Number: 05-12563
Type: Rule
Date: 2005-06-24
Agency: Federal Aviation Administration, Department of Transportation
This action establishes Class E airspace at Bob Baker Memorial Airport, Kiana, AK, to provide adequate controlled airspace to contain aircraft executing two new Standard Instrument Approach Procedures (SIAPs) and a departure procedure. This rule results in new Class E airspace upward from 700 feet (ft.) and 1,200 ft. above the surface at Bob Baker Memorial Airport, Kiana, AK.
Proposed Revision of Class E Airspace; Cordova, AK
Document Number: 05-12562
Type: Proposed Rule
Date: 2005-06-24
Agency: Federal Aviation Administration, Department of Transportation
This action proposes to revise the Class E airspace at Cordova, AK. New and revised Standard Instrument Approach Procedures (SIAPs) are being published for Cordova, AK. Additional Class E airspace is needed to contain aircraft executing instrument approaches at Merle K. (Mudhole) Smith Airport. Adoption of this proposal would result in additional Class E surface area and Class E airspace upward from 700 feet (ft.) and 1,200 ft. above the surface at Cordova, AK.
Proposed Revision of Class E Airspace; Yakutat, AK
Document Number: 05-12561
Type: Proposed Rule
Date: 2005-06-24
Agency: Federal Aviation Administration, Department of Transportation
This action proposes to revise the Class E airspace at Yakutat, AK. Three new Standard Instrument Approach Procedures (SIAPs) are being published for Yakutat, AK. Additional Class E airspace is needed to contain aircraft executing instrument approaches at Yakutat Airport. Adoption of this proposal would result in additional Class E airspace upward from 1,200 feet (ft.) above the surface at Yakutat, AK.
Proposed Establishment of Class E Airspace; Golovin, AK
Document Number: 05-12560
Type: Proposed Rule
Date: 2005-06-24
Agency: Federal Aviation Administration, Department of Transportation
This action proposes to establish new Class E airspace at Golovin, AK. Two new Standard Instrument Approach Procedures (SIAPs) and one departure procedure are being published for the Golovin Airport. There is no existing Class E airspace to contain aircraft executing the new instrument procedures at Golovin, AK. Adoption of this proposal would result in the establishment of Class E airspace upward from 700 feet (ft.) and 1,200 ft. above the surface at Golovin, AK.
Proposed Revision of Class E Airspace; Prospect Creek, AK
Document Number: 05-12559
Type: Proposed Rule
Date: 2005-06-24
Agency: Federal Aviation Administration, Department of Transportation
This action proposes to revise the Class E airspace at Prospect Creek, AK. An airspace evaluation has concluded that additional airspace is required to fully contain aircraft executing Special Instrument Approaches Procedures at Prospect Creek Airport. Adoption of this proposal would result in the revision of Class E airspace upward from 700 feet (ft.) above the surface at Prospect Creek, AK.
User Input to the Aviation Weather Technology Transfer (AWTT) Board
Document Number: 05-12558
Type: Proposed Rule
Date: 2005-06-24
Agency: Federal Aviation Administration, Department of Transportation
The FAA will hold an informal public meeting to seek aviation weather user input on icing products. Details: July 13, 2005; Northrop Grumman, Conference Room A, 475 School Street, SW., Washington, DC 20024; 9 a.m. to 5 p.m. The objective of this meeting is to provide an opportunity for interested Government and commercial sector representatives who use government-provided aviation weather information in operational decision-making to provide input on FAA's plans for implementing new icing weather products.