Federal Aviation Administration 2005 – Federal Register Recent Federal Regulation Documents

Results 201 - 250 of 2,027
Airworthiness Directives; Boeing Model 767-200 and -300 Series Airplanes
Document Number: 05-22791
Type: Rule
Date: 2005-11-21
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new airworthiness directive (AD) for certain Boeing Model 767-200 and -300 series airplanes. This AD requires replacing hinge assemblies with new hinge assemblies in the outboard overhead stowage bins and reworking hinge assemblies in the outboard overhead stowage bins that are adjacent to curtain tracks. This AD results from reports of hinge assemblies of outboard overhead stowage bins breaking or the stowage bin doors not latching properly. We are issuing this AD to prevent the outboard overhead stowage bins opening during flight and releasing baggage, and consequently injuring passengers and blocking the aisles during emergency egress.
Airworthiness Directives; British Aerospace Model HS 748 Airplanes
Document Number: 05-22790
Type: Rule
Date: 2005-11-21
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new airworthiness directive (AD) for all British Aerospace Model HS 748 airplanes. This AD requires repetitive inspections for fatigue cracking, corrosion, and other related discrepancies of the rear pressure bulkhead and associated areas, and the fin attachment fittings, particularly the fin link beam; and related investigative and corrective actions. This AD results from a structural integrity audit of the airplane that showed the importance of inspecting for fatigue cracking and corrosion of these areas. We are issuing this AD to detect and correct cracking, corrosion, and other related discrepancies of the rear pressure bulkhead and associated areas, and the fin attachment fittings, particularly the fin link beam, which could result in damage to the airplane structure or injury to airplane occupants.
Airworthiness Directives; Airbus Model A340-200 and A340-300 Series Airplanes
Document Number: 05-22789
Type: Rule
Date: 2005-11-21
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new airworthiness directive (AD) for all Airbus Model A340-200 and A340-300 series airplanes. This AD requires repetitive inspections for cracking of the junction between the thrust reverser forward frame and the 12 o'clock and 6 o'clock beams; the thrust reverser common fittings; and the thrust reverser J-ring structure at the 12 o'clock and 6 o'clock positions; and related investigative and corrective actions. This AD results from fatigue and damage tolerance testing of the engine thrust reversers which revealed fatigue cracking of the junction between the thrust reverser forward frame and the 12 o'clock beam, and of the thrust reverser J-ring structure. We are issuing this AD to detect and correct such fatigue cracking, which could result in rupture of the J-ring, forward frame, or common fittings; loss of the thrust reverser system; or inadvertent deployment of a thrust reverser in flight and consequent reduced controllability of the airplane.
Special Conditions; Garmin AT, Inc.; EFIS on the Raytheon Model B58; Protection of Systems for High Intensity Radiated Fields (HIRF)
Document Number: 05-22918
Type: Rule
Date: 2005-11-18
Agency: Federal Aviation Administration, Department of Transportation
These special conditions are issued to Garmin AT, Inc., 2345 Turner Rd., SE., Salem, Oregon 97302, for a Supplemental Type Certificate for the Raytheon Model B58. The 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 an electronic flight instrument system (EFIS) display, Model G-1000, manufactured by Garmin International Inc., for which 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; Garmin AT, Inc.; EFIS on the Raytheon A36; Protection of Systems for High Intensity Radiated Fields (HIRF)
Document Number: 05-22917
Type: Rule
Date: 2005-11-18
Agency: Federal Aviation Administration, Department of Transportation
These special conditions are issued to Garmin AT, Inc., 2345 Turner Rd. SE, Salem, OR 97302, for a Supplemental Type Certificate for the Raytheon A36. The 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 an electronic flight instrument system (EFIS) display, Model G-1000, manufactured by Garmin International Inc., for which 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.
Modification of Class E Airspace; Wellington Municipal Airport, KS
Document Number: 05-22916
Type: Rule
Date: 2005-11-18
Agency: Federal Aviation Administration, Department of Transportation
This document confirms the effective date of the direct final rule which revises Class E airspace at Wellington Municipal Airport, KS.
Modification of Class E Airspace; Sheldon Municipal Airport, IA
Document Number: 05-22915
Type: Rule
Date: 2005-11-18
Agency: Federal Aviation Administration, Department of Transportation
This document confirms the effective date of the direct final rule which revises Class E airspace at Sheldon Municipal Airport, IA.
Airworthiness Directives; CENTRAIR 101 Series Gliders
Document Number: 05-22872
Type: Rule
Date: 2005-11-18
Agency: Federal Aviation Administration, Department of Transportation
The FAA adopts a new airworthiness directive (AD) for all CENTRAIR 101 series gliders. This AD requires you to make pen and ink changes to the Limitations Section of the glider maintenance manual to eliminate contradictory information concerning the structural life limit. This AD results from a review by FAA of the Limitations Section of the CENTRAIR Model 101AP glider maintenance manual that revealed conflicting information concerning the structural life limit. We are issuing this AD to assure that the published life limit is adhered to and to prevent structural failure of the glider once this life limit is reached.
Proposed Establishment of Class E Airspace; Toksook Bay, AK
Document Number: 05-22775
Type: Proposed Rule
Date: 2005-11-17
Agency: Federal Aviation Administration, Department of Transportation
This action proposes to establish Class E airspace at Toksook Bay, AK. A new Standard Instrument Approach Procedure (SIAP) is being published for the Toksook Bay Airport. Adoption of this proposal would result in establishment of Class E airspace upward from 700 feet (ft.) and 1,200 ft. above the surface at Toksook Bay, AK.
Proposed Revision of Class E Airspace; Holy Cross, AK
Document Number: 05-22774
Type: Proposed Rule
Date: 2005-11-17
Agency: Federal Aviation Administration, Department of Transportation
This action proposes to revise the Class E airspace at Holy Cross, AK. Two new Standard Instrument Approach Procedures (SIAPs) and a revised Departure Procedure (DP) are being published for the Holy Cross Airport. Adoption of this proposal would result in revised Class E airspace upward from 700 feet (ft.) above the surface at Holy Cross, AK.
Proposed Establishment of Class E Airspace; Chignik, AK
Document Number: 05-22773
Type: Proposed Rule
Date: 2005-11-17
Agency: Federal Aviation Administration, Department of Transportation
This action proposes to establish Class E airspace at Chignik, AK. A new Standard Instrument Approach Procedure (SIAP) is being published for the Chignik Airport. Adoption of this proposal would result in creation of new Class E airspace upward from 700 feet (ft.) and 1,200 ft. above the surface at Chignik, AK.
Proposed Establishment of Class E Airspace; Koyuk, AK
Document Number: 05-22772
Type: Proposed Rule
Date: 2005-11-17
Agency: Federal Aviation Administration, Department of Transportation
This action proposes to establish new Class E airspace at Koyuk, AK. Two revised procedures and one new Standard Instrument Approach Procedure (SIAP) are being published for the Koyuk Airport. Additional Class E Airspace is needed to contain aircraft executing instrument approaches at Koyuk Airport. Additionally, one small section of Class G airspace surrounded by Class E airspace will be converted to Class E airspace by this action. Adoption of this proposal would result in creation of additional Class E airspace upward from 700 feet (ft.) and 1,200 ft. above the surface at Koyuk, AK.
Establishment of Class E Airspace; Arctic Village, AK
Document Number: 05-22771
Type: Rule
Date: 2005-11-17
Agency: Federal Aviation Administration, Department of Transportation
This action establishes Class E airspace at Arctic Village, AK to provide adequate controlled airspace to contain aircraft executing two new Standard Instrument Approach Procedures (SIAPs) and one new Instrument Flight Rules (IFR) Departure Procedure (DP). This rule results in revised Class E airspace upward from 700 feet (ft.) above the surface and from 1,200 ft. above the surface at Arctic Village Airport, AK.
Revision of Class E Airspace; Nikolai, AK
Document Number: 05-22770
Type: Rule
Date: 2005-11-17
Agency: Federal Aviation Administration, Department of Transportation
This action establishes Class E airspace at Nikolai, 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.) above the surface at Nikolai Airport, AK.
Establishment of Class E Airspace; Nenana, AK
Document Number: 05-22767
Type: Rule
Date: 2005-11-17
Agency: Federal Aviation Administration, Department of Transportation
This action revises Class E airspace at Nenana, AK to provide adequate controlled airspace to contain aircraft executing Standard Instrument Approach Procedures (SIAPs). This rule results in revised Class E airspace upward from 700 feet (ft.) above the surface at Nenana Municipal Airport, AK.
Revision of Class E Airspace; Egegik, AK
Document Number: 05-22766
Type: Rule
Date: 2005-11-17
Agency: Federal Aviation Administration, Department of Transportation
This action modifies Class E airspace at Egegik, AK to provide adequate controlled airspace to contain aircraft executing two revised Standard Instrument Approach Procedures (SIAPs). This rule results in revised Class E airspace upward from 700 feet (ft.) above the surface at Egegik Airport, AK.
Airworthiness Directives; McCauley Propeller Systems Models 3A32C406/82NDB-X and D3A32C409/82NDB-X Propellers
Document Number: 05-22712
Type: Proposed Rule
Date: 2005-11-16
Agency: Federal Aviation Administration, Department of Transportation
The FAA proposes to adopt a new airworthiness directive (AD) for McCauley Propeller Systems models 3A32C406/82NDB-X and D3A32C409/ 82NDB-X propellers, installed on Teledyne Continental Motors (TCM) IO- 520, TSIO-520, or IO-550 reciprocating engines. These propellers are herein referred to as C406 and C409 propellers, respectively. This proposed AD would require adding an operational revolutions per minute (rpm) restriction on the C406 and C409 propellers, and installing an rpm restriction placard in the cockpit. This proposed AD would also add a 10,000-hour total time-in-service (TIS) life limit for these propellers. This proposed AD would also remove from service any propeller that has 10,000 hours or more total TIS, or that has an unknown total TIS. Also, this proposed AD would require initial and repetitive propeller blade inspections for damage, and repair if necessary. This proposed AD results from testing by the manufacturer that identified stress conditions that affect the fatigue life and damage tolerance of C406 and C409 propellers, when installed on TCM IO- 520, TSIO-520, or IO-550 reciprocating engines. We are proposing this AD to prevent blade or hub failure that could result in separation of a propeller blade and loss of control of the airplane.
Notice of Availability of an Environmental Assessment (EA) and Finding of No Significant Impact (FONSI) Executed by the Federal Aviation Administration (FAA) for the Evaluation of Environmental Impacts Associated With a Proposed Corporate Hangar Construction at Cincinnati Municipal Airport-Lunken Field, Located in Cincinnati, OH
Document Number: 05-22652
Type: Notice
Date: 2005-11-16
Agency: Federal Aviation Administration, Department of Transportation
The FAA is making available an EA and FONSI for the evaluation of environmental impacts associated with a proposed corporate hangar construction at Cincinnati Municipal Airport-Lunken Field, located in Cincinnati, Ohio. 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.
Proposed Advisory Circular 25-17A Revision, Transport Airplane Cabin Interiors Crashworthiness Handbook
Document Number: 05-22651
Type: Notice
Date: 2005-11-16
Agency: Federal Aviation Administration, Department of Transportation
This notice announces the availability of and requests comments on a proposed advisory circular (AC) revision that sets forth acceptable methods of compliance with Title 14, Code of Federal Regulations (14 CFR), part 25, concerning the crashworthiness requirements as applied to cabin interiors. Like all ACs, it is not regulatory but provides guidance for applicants in demonstrating compliance with the objective safety standards set forth in part 25. This notice is necessary to give all interested persons an opportunity to present their views on the proposed AC.
Agency Information Collection Activity Under OMB Review, Request for Comments; Renewal of an Approved Information Collection Activity, Suspected Unapproved Parts Notification
Document Number: 05-22650
Type: Notice
Date: 2005-11-16
Agency: Federal Aviation Administration, Department of Transportation
The FAA invites public comments about our intention to request the Office of Management and Budget's (OMB) renewal of a current information collection. The information collected on the FAA Form 8120- 11 will be reported voluntarily by manufacturers, repair stations, aircraft owner/operators, air carriers, and the general public who wish to report suspected ``unapproved'' parts to the FAA for review. The information will be used to determine if an ``unapproved'' part investigation is warranted.
Agency Information Collection Activity Under OMB Review, Request for Comments; Renewal of an Approved Information Collection Activity, Agricultural Aircraft Operator Certificate Application
Document Number: 05-22649
Type: Notice
Date: 2005-11-16
Agency: Federal Aviation Administration, Department of Transportation
The FAA invites public comments about our intention to request the Office of Management and Budget's (OMB) renewal of a current information collection. Standards have been established for the operation of agricultural aircraft and for the dispensing of chemicals, pesticides, and toxic substances. Information collected shows applicant compliance and eligibility for certification by FAA.
Airworthiness Directives; Boeing Model 737-600, -700, -700C, -800, and -900 Series Airplanes
Document Number: 05-22593
Type: Rule
Date: 2005-11-16
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new airworthiness directive (AD) for certain Boeing Model 737-600, -700, -700C, -800, and -900 series airplanes. This AD requires modification of certain wire bundles located above the center fuel tank. This AD results from fuel system reviews conducted by the manufacturer. We are issuing this AD to prevent chafed wire bundles near the center fuel tank, which could cause electrical arcing through the tank wall and ignition of fuel vapor in the fuel tank, and result in a fuel tank explosion.
Airworthiness Directives; British Aerospace Model BAC 1-11 200 and 400 Series Airplanes
Document Number: 05-22592
Type: Rule
Date: 2005-11-16
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new airworthiness directive (AD) for all British Aerospace Model BAC 1-11 200 and 400 series airplanes. This AD requires revising the airplane flight manual (AFM) to contain applicable AFM amendments, which advise the flightcrew of information pertaining to safely operating the fuel system. The AD also requires revising the FAA-approved maintenance program to include certain repetitive maintenance tasks intended to improve the safety of the fuel system. This AD results from fuel system reviews conducted by the manufacturer. We are issuing this AD to prevent potential ignition sources inside the fuel system, which, in combination with flammable fuel vapors, could result in a fuel tank explosion and consequent loss of the airplane.
Airworthiness Directives; Boeing Model 737 Airplanes
Document Number: 05-22591
Type: Rule
Date: 2005-11-16
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new airworthiness directive (AD) for certain Boeing Model 737 airplanes. This AD requires, for certain airplanes, a one-time detailed inspection for interference between a clamp assembly and the wires behind the P15 refuel panel, and corrective actions if necessary. For certain other airplanes, this AD requires a one-time detailed inspection for discrepancies of the wires behind the P15 refuel panel; and corrective and related investigative actions if necessary. This AD is prompted by evidence of chafed wiring behind the P15 refuel panel and arcing to the back of the P15 refuel panel and adjacent wing structure. We are issuing this AD to detect and correct chafing of the wiring behind the P15 refuel panel, which could lead to arcing and fire with consequent airplane damage and injury to refueling personnel.
Airworthiness Directives; Fokker Model F27 Mark 050 Airplanes
Document Number: 05-22589
Type: Rule
Date: 2005-11-16
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new airworthiness directive (AD) for all Fokker Model F27 Mark 050 airplanes. This AD requires a one-time inspection of the bleed air supply ducts to determine if blanking plugs are present and a one-time inspection of the entire area of the engine nacelle for heat damage; and corrective actions if necessary. This AD also requires replacement of the blanking plugs with clamping devices. This AD results from heat damage in areas adjacent to the bleed air supply duct assembly. We are issuing this AD to prevent rupture of the bleed air supply duct, which could lead to hot bleed air leaking into the engine controls area and result in heat damage to control cables, electrical wiring, hydraulic components, and fuel lines, and consequent fire.
Revision of Jet Routes J-8, J-18, J-19, J-58, J-76, J-104 and J-244; and VOR Federal Airways V-60, V-190, V-263 and V-611; Las Vegas, NM
Document Number: 05-22578
Type: Rule
Date: 2005-11-16
Agency: Federal Aviation Administration, Department of Transportation
This action changes the effective date of a final rule published in the Federal Register on October 18, 2005 (70 FR 60424), Airspace Docket No. 05-ASW-1. In that rule, the effective date was inadvertently published as December 22, 2005. This action changes the effective date to April 13, 2006.
Airworthiness Directives; Bombardier Model CL-600-2B19 (Regional Jet Series 100 & 440) Airplanes
Document Number: 05-22590
Type: Proposed Rule
Date: 2005-11-15
Agency: Federal Aviation Administration, Department of Transportation
The FAA proposes to adopt a new airworthiness directive (AD) for certain Bombardier Model CL-600-2B19 (Regional Jet Series 100 & 440) airplanes. This proposed AD would require replacing the Camloc fasteners on the sidewall of the center pedestal. This proposed AD results from reports of the Camloc fasteners on the sidewall of the center pedestal disengaging and interfering with an inboard rudder pedal. We are proposing this AD to prevent these fasteners from disengaging and interfering with an inboard rudder pedal, which could reduce directional controllability of the airplane.
Airworthiness Directives; Airbus Model A330-200, A330-300, A340-200, and A340-300 Series Airplanes; and A340-541 and A340-642 Airplanes
Document Number: 05-22588
Type: Proposed Rule
Date: 2005-11-15
Agency: Federal Aviation Administration, Department of Transportation
The FAA proposes to adopt a new airworthiness directive (AD) for all Airbus Model A330-200, A330-300, A340-200, and A340-300 series airplanes; and A340-541 and A340-642 airplanes. This proposed AD would require operators to revise the Airworthiness Limitations section of the Instructions for Continued Airworthiness to incorporate new information. This information includes, for all affected airplanes, decreased life limit values for certain components; and for Model A330-200 and -300 series airplanes, new inspections, compliance times, and new repetitive intervals to detect fatigue cracking, accidental damage, or corrosion in certain structures. This proposed AD results from a revision to subsection 9-1 of the Airbus A330 and A340 Maintenance Planning Documents (MPD) for Life Limits/Monitored parts, and subsection 9-2 of the Airbus A330 MPD for Airworthiness Limitations Items. We are proposing this AD to ensure the continued structural integrity of these airplanes.
Airworthiness Directives; BAE Systems (Operations) Limited Model BAe 146 Airplanes
Document Number: 05-22587
Type: Proposed Rule
Date: 2005-11-15
Agency: Federal Aviation Administration, Department of Transportation
The FAA proposes to adopt a new airworthiness directive (AD) for certain BAE Systems (Operations) Limited Model BAe 146 airplanes. This proposed AD would require repetitive inspections to measure the depth of chafing or scoring in the skin along the full length of the fairing from forward to aft ends at the contact between the seal and fuselage, and related investigative/corrective actions if necessary. This proposed AD results from a report of chafing in this area. We are proposing this AD to ensure the structural integrity of the fuselage.
Public Notice for the Sale of Aeronautical Property at Manchester Airport, Manchester, NH
Document Number: 05-22577
Type: Notice
Date: 2005-11-15
Agency: Federal Aviation Administration, Department of Transportation
The FAA is requesting public comment on the City of Manchester, New Hampshire's request to sell a portion (3.98 acres) of Airport property. The property is located in the area of the Northeast Ramp off Perimeter Road and is identified as Tax Map 721, Lot 17E. The land is currently unimproved. The parcel will be swapped with another parcel of equal value needed for Airport development. Upon sale, the land will be utilized for hangar development. A portion of the property (2.58 acres) was acquired under the Surplus Property Act via deed dated August 16, 1968. The disposition of proceeds from the disposal of airport property will be in accordance with FAA's Policy and Procedures Concerning the Use of Airport Revenue, published in the Federal Register on February 16, 1999.
Standard Instrument Approach Procedures, Weather Takeoff Minimums; Miscellaneous Amendments
Document Number: 05-22494
Type: Rule
Date: 2005-11-15
Agency: Federal Aviation Administration, Department of Transportation
This amendment establishes, amends, suspends, or revokes Standard Instrument Approach Procedures (SIAPs) and/or Weather Takeoff Minimums for operations at certain airports. These regulatory actions are needed because of the adoption of new or revised criteria, or because of changes occurring in the National Airspace System, such as the commissioning of new navigational facilities, addition of new obstacles, or changes in air traffic requirements. These changes are designed to provide safe and efficient use of the navigable airspace and to promote safe flight operations under instrument flight rules at the affected airports.
Standard Instrument Approach Procedures; Miscellaneous Amendments
Document Number: 05-22493
Type: Rule
Date: 2005-11-15
Agency: Federal Aviation Administration, Department of Transportation
This amendment amends Standard Instrument Approach Procedures (SIAPs) for operations at certain airports. These regulatory actions are needed because of changes occurring in the National Airspace System, such as the commissioning of new navigational facilities, addition of new obstacles, or changes in air traffic requirements. These changes are designed to provide safe and efficient use of the navigable airspace and to promote safe flight operations under instrument flight rules at the affected airports.
Establishment of a Class E Enroute Domestic Airspace Area, San Luis Obispo, CA
Document Number: 05-22523
Type: Rule
Date: 2005-11-14
Agency: Federal Aviation Administration, Department of Transportation
This action establishes a Class E enroute domestic airspace area west of San Luis Obispo, CA, to replace existing Class G uncontrolled airspace.
Noise Exposure Map Notice; Receipt of Noise Compatibility Program and Request for Review; Collin County Regional Airport, McKinney, TX
Document Number: 05-22522
Type: Notice
Date: 2005-11-14
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 McKinney, Texas for Collin County Regional 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. The FAA also announces that it is reviewing a proposed noise compatibility program that was submitted for Collin County Regional Airport under Part 150 in conjunction with the noise exposure map, and that this program will be approved or disapproved on or before April 30, 2006.
Special Conditions: Cessna Model 650 Airplanes; High-Intensity Radiated Fields (HIRF)
Document Number: 05-22521
Type: Rule
Date: 2005-11-14
Agency: Federal Aviation Administration, Department of Transportation
These special conditions are issued for Cessna Model 650 airplanes modified by Elliott Aviation Technical Product Development, Inc. These modified airplanes will have a novel or unusual design feature when compared to the state of technology envisioned in the airworthiness standards for transport category airplanes. The modification incorporates the installation of electronic flight display systems manufactured by Universal Avionics Systems Corporation. The electronic flight display systems perform critical functions. The applicable airworthiness regulations do not contain adequate or appropriate safety 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 that established by the existing airworthiness standards.
Approval of Noise Compatibility Program Update for Lehigh Valley International Airport, Allentown, PA
Document Number: 05-22492
Type: Notice
Date: 2005-11-14
Agency: Federal Aviation Administration, Department of Transportation
The Federal Aviation Administration (FAA) announces its findings on the noise compatibility program submitted by the Lehigh- Northampton Airport Authority under the provisions of 49 U.S.C. (the Aviation Safety and Noise Abatement Act, hereinafter referred to as ``the Act'') and 14 CFR Part 150. These findings are made in recognition of the description of Federal and nonfederal responsibilities in Senate Report No. 96-52 (1980). On May 14, 2004 the FAA determined that the noise exposure maps submitted by the Lehigh- Northampton Airport Authority under Part 150 were in compliance with applicable requirements. On October 7, 2005, the FAA approved the Lehigh Valley International Airport's updated noise compatibility program. Most of the recommendations of the program update were approved. One program element relating to revised flight procedures for noise abatement was proposed by the airport operator and was approved in part, as a voluntary measure, and disapproved in part. Only one noise abatement element was disapproved for purposes of Part 150 pending submission of additional information needed to make an informed analysis. The Lehigh-Northampton Airport Authority has also requested under FAR Part 150, section 150.35(f), that FAA determine that the revised five-year forecast condition NEM submitted with the noise compatibility program and showing noise contours as a result of the implementation of the noise compatibility program is in compliance with applicable requirements of FAR Part 150. The FAA announces its determination that the revised five-year forecast condition NEW for the Lehigh Valley International Airport for the year 2008 submitted with the noise compatibility program is in compliance with applicable requirements of FAR Part 150 effective October 31, 2005. The documentation that constitutes the revised five-year forecast condition NEM as defined in Sec. Sec. 150.7 and 150.101(e) of Part 150 includes but is not limited to: Sections 2.2 and 2.3, Figure 3, and Table 3 in the NCP Update, and Figure 11 and Figures 36 through 45 in the NEM volume. The FAA has determined that this revised five-year forecast condition NEM and accompanying documentation are in compliance with applicable requirements.
Airworthiness Directives; Empresa Brasileira de Aeronautica S.A. (EMBRAER) Model ERJ 170 Airplanes
Document Number: 05-22442
Type: Rule
Date: 2005-11-14
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new airworthiness directive (AD) for all Empresa Brasileira de Aeronautica S.A. (EMBRAER) Model ERJ 170 airplanes. This AD requires repetitively replacing the low-stage check valve and associated seals of the right-hand engine bleed system. This AD results from a report that an engine shut down during flight due to the failure of the low-stage check valve to close. We are issuing this AD to prevent failure of the low-stage check valve, which could result in an engine shutting down during flight.
Airworthiness Directives; Bombardier Model CL-600-2B19 (Regional Jet Series 100 & 440) Airplanes
Document Number: 05-22309
Type: Rule
Date: 2005-11-14
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new airworthiness directive (AD) for certain Bombardier Model CL-600-2B19 (Regional Jet Series 100 & 440) airplanes. This AD requires revising the Airworthiness Limitations section of the Instructions for Continued Airworthiness of the Canadair Regional Jet Maintenance Requirements Manual by incorporating new procedures for repetitive detailed and special detailed inspections for cracking of the aft pressure bulkhead. This AD results from a fatigue test, which revealed cracking of the aft pressure bulkhead; subsequent in-service reports show that fatigue cracking has been found on other airplanes. We are issuing this AD to detect and correct cracking in the aft pressure bulkhead, which could result in reduced structural integrity and rapid decompression of the airplane.
Airworthiness Directives; Empresa Brasileira de Aeronautica S.A. (EMBRAER) Model EMB-135 Airplanes, and Model EMB-145, -145ER, -145MR, -145LR, -145XR, -145MP, and -145EP Airplanes
Document Number: 05-22308
Type: Rule
Date: 2005-11-14
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new airworthiness directive (AD) for certain EMBRAER Model EMB-135 airplanes, and Model EMB-145, -145ER, - 145MR, -145LR, -145XR, -145MP, and -145EP airplanes. This AD requires modification of the logic of the steering system of the nose landing gear (NLG) wheel. This AD results from reports of the loss of directional control of the airplane on the ground after an internal failure of the NLG wheel steering system. We are issuing this AD to prevent failure of the NLG wheel steering system, which could result in reduced controllability of the airplane.
Airworthiness Directives; Learjet Model 23, 24, 24A, 24B, 24B-A, 24C, 24D, 24D-A, 24E, 24F, 24F-A, 25, 25A, 25B, 25C, 25D, and 25F Airplanes
Document Number: 05-22220
Type: Rule
Date: 2005-11-14
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new airworthiness directive (AD) for certain Learjet Model 23, 24, 24A, 24B, 24B-A, 24C, 24D, 24D-A, 24E, 24F, 24F-A, 25, 25A, 25B, 25C, 25D, and 25F airplanes. This AD requires replacement of the spherical accumulator for the main hydraulic system with a new cylindrical accumulator. For certain airplanes, this AD also requires modification of the accumulator pressure gauge. This AD results from reports of the failure of two thrust reverser accumulators (which are similar to the main hydraulic system's spherical accumulator) and fatigue cracks found on four thrust reverser accumulators. We are issuing this AD to prevent failure of the spherical accumulator for the main hydraulic system, due to fatigue cracking on the threads, which could result in the loss of hydraulic power, damage to the surrounding airplane structure, and loss of airplane control. The failure of the accumulator could also result in injury to any persons in the surrounding area. The loss of hydraulic fluid could also leak onto a potential source of ignition and result in a consequent fire.
Airworthiness Directives; Airbus Model A319-100 Series Airplanes, Model A320-111 Airplanes, Model A320-200 Series Airplanes, and Model A321-100 Series Airplanes
Document Number: 05-22219
Type: Rule
Date: 2005-11-14
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new airworthiness directive (AD) for certain Airbus Model A319-100 series airplanes, Model A320-111 airplanes, Model A320-200 series airplanes, and Model A321-100 series airplanes equipped with any additional center tank (ACT). This AD requires identifying the part number of the ACT and, for certain ACTs, replacing the outer ACT manhole cover and seal. This AD results from reports of an ACT fuel transfer failure due to air leakage around the seal of the outer manhole covers of the ACTs. We are issuing this AD to prevent this leakage, which could result in fuel or fuel vapor leaking into the cargo compartment, and consequent increased risk of a fire in the cargo compartment.
Airworthiness Directives; Saab Model SAAB 2000 Airplanes
Document Number: 05-22218
Type: Rule
Date: 2005-11-14
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new airworthiness directive (AD) for certain Saab Model SAAB 2000 airplanes. This AD requires modifying the manual feather-and-unfeather system for the propellers to make the design of the system more robust. This AD results from reports of in- flight engine shutdown caused by uncommanded operation of the feather pump of the propeller. We are issuing this AD to prevent uncommanded feathering of the propeller, which could result in the shutdown of an engine during flight and consequent reduced controllability of the airplane.
Airworthiness Directives; Airbus Model A319-100, A320-200, and A321-100 and -200 Series Airplanes
Document Number: 05-22217
Type: Rule
Date: 2005-11-14
Agency: Federal Aviation Administration, Department of Transportation
The FAA is superseding an existing airworthiness directive (AD), which applies to certain Airbus Model A319-100, A320-200, and A321-100 and -200 series airplanes. That AD currently requires modification of the telescopic girt bar of the escape slide/raft assembly, and follow-on actions. This new AD requires a new modification of the telescopic girt bar and the installation of placards on the modified girt bars, which terminates the repetitive functional tests required by the existing AD. This AD results from development of a new, improved modification. We are issuing this AD to prevent failure of the escape slide/raft to deploy correctly, which could result in the slide being unusable during an emergency evacuation and consequent injury to passengers or airplane crewmembers.
Airworthiness Directives; Airbus Model A300 B4-600 and A300 B4-600R Series Airplanes; and A300 F4-605R and A300 C4-605R Variant F Airplanes
Document Number: 05-22216
Type: Rule
Date: 2005-11-14
Agency: Federal Aviation Administration, Department of Transportation
The FAA is superseding an existing airworthiness directive (AD), which applies to all Airbus Model A300 B4-600 and A300 B4-600R series airplanes, and all Model A300 F4-605R airplanes. That AD currently requires repetitive inspections to detect cracks of certain attachment holes, installation of new fasteners, follow-on inspections or repair if necessary, and modification of the angle fittings of fuselage frame FR47. This new AD revises certain inspection thresholds and intervals. This new AD also adds inspections to detect cracks of additional attachment holes. This AD results from reports of cracks found before the inspection thresholds in the existing AD and cracks found in nearby areas not inspected by the existing AD. We are issuing this AD to prevent fatigue cracking of the forward fitting of fuselage frame FR47, which could result in reduced structural integrity of the frame.
Airworthiness Directives; Learjet Model 23, 24, 24A, 24B, 24B-A, 24D, 24D-A, 24E, 24F, 25, 25A, 25B, 25C, 25D, and 25F Airplanes Modified by Supplemental Type Certificate SA1731SW, SA1669SW, or SA1670SW
Document Number: 05-22215
Type: Rule
Date: 2005-11-14
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new airworthiness directive (AD) for certain Learjet Model 23, 24, 24A, 24B, 24B-A, 24D, 24D-A, 24E, 24F, 25, 25A, 25B, 25C, 25D, and 25F airplanes. This AD requires removing the thrust reverser accumulator, and making the thrust reverser hydraulic system and the thrust reversers inoperable. This AD results from reports of the failure of two thrust reverser accumulators. We are issuing this AD to prevent failure of the thrust reverser accumulators, due to fatigue cracking on the female threads, which could result in the loss of hydraulic power and damage to the surrounding airplane structure.
Airworthiness Directives; Airbus Model A330-200 and A330-300 Series Airplanes; and Model A340-200 and A340-300 Series Airplanes
Document Number: 05-22213
Type: Rule
Date: 2005-11-14
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new airworthiness directive (AD) for all Airbus Model A330-200 and A330-300 series airplanes; and Model A340-200 and A340-300 series airplanes. This AD requires an accelerated schedule of repetitive testing of the elevator servo control loops, and corrective actions if necessary. This AD results from reports of failed elevator servo controls due to broken guides. We are issuing this AD to ensure proper functioning of the elevator servo controls. Failure of the elevator servo controls during certain phases of takeoff could result in an unannounced loss of elevator control and consequent reduced controllability of the airplane.
Standard Airworthiness Certification of New Aircraft
Document Number: 05-22457
Type: Proposed Rule
Date: 2005-11-10
Agency: Federal Aviation Administration, Department of Transportation
The FAA is proposing language to supplement a proposal published in the Federal Register on February 15, 2005. This action is necessary to include in the proposal a provision from the recently enacted Safe, Accountable, Flexible, and Efficient Transportation Equity Act: A Legacy for Users. The supplemental language allows a person to manufacture one new aircraft based on a type certificate without holding the type certificate or having a licensing agreement from the type certificate holder, provided the manufacturing began before August 5, 2004.
Supplemental Oxygen
Document Number: 05-22456
Type: Rule
Date: 2005-11-10
Agency: Federal Aviation Administration, Department of Transportation
In this direct final rule, the FAA is amending its regulation on the use of pilot supplemental oxygen. The amendment changes the flight level at which the remaining pilot at the controls of the airplane must put on and use his oxygen mask if the other pilot at any time leaves his control station of the airplane. This amendment revises that altitude to ``above flight level 350'' from ``above flight level 250.'' It will also eliminate the needless use of oxygen that is not otherwise required to provide for safety in air carrier operations. This will reduce needless expenditures to replace oxygen equipment that is subject to excessive wear and tear.
Airworthiness Directives; Bombardier Model CL-600-1A11 (CL-600), CL-600-2A12 (CL-601), and CL-600-2B16 (CL-601-3A, CL-601-3R, and CL-604) Airplanes
Document Number: 05-22445
Type: Proposed Rule
Date: 2005-11-10
Agency: Federal Aviation Administration, Department of Transportation
The FAA proposes to adopt a new airworthiness directive (AD) for certain Bombardier Model CL-600-1A11 (CL-600), CL-600-2A12 (CL- 601), and CL-600-2B16 (CL-601-3A, CL-601-3R, & CL-604) airplanes. This proposed AD would require modifying the rudder balance spring assembly by installing a new adjustable balance spring, and rigging the assembly to suit the rudder of each airplane. This proposed AD results from production inspections that showed that the spring assembly that controls rudder balance may not have the correct pre-load on some airplanes. We are proposing this AD to prevent uncommanded yaw movements and consequent reduced controllability of the airplane.
Airworthiness Directives; Airbus Model A319-100 and A320-200 Series Airplanes
Document Number: 05-22444
Type: Proposed Rule
Date: 2005-11-10
Agency: Federal Aviation Administration, Department of Transportation
The FAA proposes to adopt a new airworthiness directive (AD) for certain Airbus Model A319-100 and A320-200 series airplanes. This proposed AD would require repetitive inspections of the wing-tank fuel pumps, canisters, and wing fuel tanks for detached identification labels, and corrective action if necessary. This proposed AD results from several incidents of detached plastic identification labels found floating in the wing fuel tanks. We are proposing this AD to prevent plastic identification labels being ingested into the fuel pumps and consequently entering the engine fuel feed system, which could result in an engine shutdown.