Federal Aviation Administration 2005 – Federal Register Recent Federal Regulation Documents
Results 1,851 - 1,900 of 2,027
Aging Airplane Safety
This action adopts the interim final rule published on December 6, 2002, as a final rule with changes. The IFR imposed statutory requirements from the Aging Aircraft Safety Act of 1991 for certain airplanes to undergo inspections and records reviews after their 14th year in service and at specified intervals after that. Also, the rule imposed a requirement to include supplemental inspections by specified deadlines in the maintenance programs for these airplanes. With this action, the FAA responds to comments to the IFR, further clarifies parts of the rule language, and substantially revises the supplemental inspection requirements.
Airworthiness Directives; Boeing Model 747 Series Airplanes
This amendment adopts a new airworthiness directive (AD), applicable to all Boeing Model 747 series airplanes, that requires repetitive inspections of the nacelle strut-to-wing attachment structure, and repetitive overhaul of the diagonal brace and spring beam load paths, to maintain damage tolerance requirements and ensure long-term structural integrity; and follow-on and corrective actions if necessary. This action is necessary to ensure the structural integrity of the strut-to-wing load path and prevent separation of the strut and engine from the airplane. This action is intended to address the identified unsafe condition.
Airworthiness Directives; Pacific Aerospace Corporation, Ltd. Model 750XL Airplanes
The FAA adopts a new airworthiness directive (AD) for all Pacific Aerospace Corporation, Ltd. (Pacific Aerospace) Model 750XL airplanes. This AD requires you to replace any type TLP-D or TLED rivets on the aileron pushrod ends and elevator control pushrod ends. This AD results from mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for New Zealand. We are issuing this AD to replace the above identified rivets on the aileron pushrod ends and elevator control pushrod ends, which, if not replaced, could result in loose mechanical elements in the control systems. This could lead to control anomalies and loss of airplane control.
Airworthiness Directives; Boeing Model 737-300, -400, and -500 Series Airplanes; and Model 757-200 and -200CB Series Airplanes
This amendment adopts a new airworthiness directive (AD), applicable to certain Boeing Model 737-300, -400, and -500 series airplanes; and Model 757-200 and -200CB series airplanes, that requires inspection of the applicable body station frames for open body station frames and related investigative/corrective actions; and installation of lanyard hook brackets and lanyard assemblies under the air conditioning overhead ducts, as applicable. This action is necessary to prevent loosened or disconnected overhead ducts from causing ceiling panels to drop below the minimum height of the evacuation zone for the passenger cabin, which could result in inadequate height for safe exit in the event of an emergency evacuation. This action is intended to address the identified unsafe condition.
Airworthiness Directives; Aerospatiale Model ATR42-200, -300, and -320 Series Airplanes
The FAA proposes to adopt a new airworthiness directive (AD) for certain Aerospatiale Model ATR42-200, -300, and -320 series airplanes. This proposed AD would require doing repetitive inspections of the upper arms of the MLG side braces for missing or inadequately bonded identification plates; replacing the upper arm if necessary; and replacing the side brace assembly with a modified part. This proposed AD is prompted by an operator who reported experiencing an unlock warning for the MLG on the right side of the airplane. We are proposing this AD to prevent cracking of the upper arms of the side braces of the MLG, which could result in failure of the MLG during landing and possible damage to the airplane and injury to the flightcrew and passengers.
Airworthiness Directives; Bombardier Model DHC-8-102, -103, -106, -201, -202, -301, -311, and -315 Airplanes
The FAA proposes to adopt a new airworthiness directive (AD) for certain Bombardier Model DHC-8-102, -103, -106, -201, -202, -301, - 311, and -315 airplanes. The subject of this proposed AD is the pilot's static system. This proposed AD would require revising the airplane flight manual to include applicable procedures to follow when the flightcrew receives abnormal indications of airspeed, altitude, or vertical airspeed. This proposed AD would also require modifying the static system. This proposed AD is prompted by a report of a leak in the static pressure system, which could result in loss of the static systems and consequent erroneous data displayed on the pilot's flight instruments. We are proposing this AD to advise the flightcrew of applicable procedures in the event of abnormal indications of airspeed, altitude, or vertical airspeed; and to prevent leaks in the static system, which could result in the loss of critical flight information that could result in reduced controllability of the airplane or controlled flight into terrain.
Airworthiness Directives; Empresa Brasileira de Aeronautica S.A. (EMBRAER) Model EMB-135 and -145 Series Airplanes
The FAA proposes to adopt a new airworthiness directive (AD) for certain EMBRAER Model EMB-135 and -145 series airplanes. This proposed AD would require repetitive detailed inspections for surface bruising of the main landing gear (MLG) trailing arms and integrity of the MLG pivot axle sealant, and corrective actions if necessary. This proposed AD would also provide for optional terminating action for the repetitive inspections. This proposed AD is prompted by a report of a fractured axle of the trailing arm of the MLG due to corrosion of the axle. We are proposing this AD to prevent a broken trailing arm and consequent failure of the MLG, which could lead to loss of control and damage to the airplane during take-off or landing.
Airworthiness Directives; Airbus Model A330, A340-200, and A340-300 Series Airplanes
The FAA proposes to adopt a new airworthiness directive (AD) for all Airbus Model A330, A340-200, and A340-300 series airplanes. This proposed AD would require inspecting to determine the part number and serial number of the left- and right-hand elevator assemblies, performing related investigative and corrective actions if necessary, and re-protecting the elevator assembly. This proposed AD is prompted by reports that areas on the top skin panel of the right-hand elevator have disbonded due to moisture penetration. We are proposing this AD to prevent disbonding of the elevator assembly, which could reduce the structural integrity of the elevator and result in reduced controllability of the airplane.
Airworthiness Directives; Empresa Brasileira de Aeronautica S.A. (EMBRAER) Model EMB-120 Series Airplanes
This document revises an earlier proposed airworthiness directive (AD), applicable to certain EMBRAER Model EMB-120 series airplanes that would have required initial and repetitive calibration testing of potentiometers to detect noisy signals and replacement of only those with noisy signals. This new action revises the proposed AD by reducing the compliance time for the repetitive calibration testing of the potentiometers and adding the requirement for reporting results of the calibration tests of the potentiometers and the readouts of the flight data recorder (FDR) to the airplane manufacturer. The actions specified by this new proposed AD are intended to prevent the potentiometers that provide information on the positions of the primary flight controls to the FDR from transmitting noisy signals or becoming improperly calibrated, resulting in the transmission of incomplete or inaccurate data to the FDR. This lack of reliable data could hamper discovery of the unsafe condition that caused an accident or incident and prevent the FAA from developing and mandating actions to prevent additional accidents or incidents caused by that same unsafe condition. This action is intended to address the identified unsafe condition.
Airworthiness Directives; Boeing Model 747 Airplanes
The FAA proposes to supersede an existing airworthiness directive (AD) that applies to certain Boeing Model 747-100, -200, - 300, and 747SP series airplanes. The existing AD currently requires certain inspections to find missing or alloy-steel taperlock fasteners (bolts) in the diagonal brace underwing fittings, and corrective actions if necessary. For airplanes with missing or alloy-steel fasteners, the existing AD also mandates replacement of certain fasteners with new fasteners, which constitutes terminating action for certain inspections. This proposed AD would expand the applicability to include additional airplane models and would require a new inspection to determine fastener material and to find missing or broken fasteners, and related investigative/corrective actions if necessary. This proposed AD is prompted by reports indicating that cracked fasteners made of A286 material were found on airplanes that had only fasteners made of A286 material installed in the area common to the diagonal brace underwing fittings. We are proposing this AD to prevent loss of the underwing fitting load path due to missing or damaged alloy-steel or A286 taperlock fasteners, which could result in separation of the engine and strut from the airplane.
Airworthiness Directives; Saab Model SAAB 2000 Series Airplanes
The FAA proposes to adopt a new airworthiness directive (AD) for certain Saab Model SAAB 2000 series airplanes. This proposed AD would require a one-time inspection to detect a broken terminal stud on a main relay of the electrical power generator, and corrective action if necessary. This proposed AD is prompted by disconnection of an electrical power generator during an inspection flight, which was caused by a broken terminal stud on the main relay. We are proposing this AD to prevent a broken terminal stud on the main relay of an electrical power generator, which could reduce the redundancy of electrical power systems, result in increased pilot workload, and contribute to reduced controllability of the airplane.
Performance-Based Operations Aviation Rulemaking Committee
This document announces a public meeting in which the Federal Aviation Administration (FAA) and members of the Performance-Based Operations Aviation Rulemaking Committee (PARC) will discuss the activities of the PARC since the Federal Aviation Administrator chartered the group in February 2004.
Airworthiness Directives; Airbus Model A319, A320, and A321 Series Airplanes
The FAA proposes to adopt a new airworthiness directive (AD) for certain Airbus Model A319, A320, and A321 series airplanes. This proposed AD would require replacing the cargo ventilation extraction duct at frame 65 with a new duct, and relocating the temperature sensor in the aft cargo compartment. This proposed AD is prompted by a report indicating that, during a test of the fire extinguishing system, air leakage around the temperature sensor for the aft cargo compartment reduced the concentration of fire extinguishing agent to below the level required to suppress a fire. We are proposing this AD to prevent air leakage around the temperature sensor for the aft cargo compartment, which, in the event of a fire in the aft cargo compartment, could result in an insufficient concentration of fire extinguishing agent, and consequent inability of the fire extinguishing system to suppress the fire.
Carrying Candidates in Elections
This final rule allows an aircraft operator, other than one operating an aircraft as an air carrier or commercial operator, to receive payment for carrying a candidate seeking office in a State or local election during a campaign. Current regulations allow aircraft operators to receive payment for carrying candidates seeking office in Federal elections during a campaign without the aircraft operator having to meet the safety standards applicable to air carriers and other commercial operators. This rule meets a Congressional mandate that the FAA amend its rules to allow aircraft operators who transport State and local candidates for compensation, to do so without having to comply with FAA safety rules applicable to air carriers and other commercial operators.
Airworthiness Directives; McDonnell Douglas Model MD-11 and MD-11F Airplanes
The FAA is adopting a new airworthiness directive (AD) for certain McDonnell Douglas Model MD-11 and MD-11F airplanes. This AD requires inspecting the power feeder cables of the auxiliary power unit (APU) for chafing damage, and accomplishing any related corrective action. This AD also requires modifying the drain line of the fuel feed shroud of the horizontal stabilizer. This AD is prompted by a report of the drain line of the fuel feed shroud riding on the power feeder cables of the APU. We are issuing this AD to prevent chafing of the power feeder cables of the APU, which could result in electrical arcing to adjacent structure and consequent fire in the airplane.
Airworthiness Directives; Boeing Model 757 Series Airplanes Equipped With Rolls Royce Model RB211 Engines
This amendment adopts a new airworthiness directive (AD), applicable to certain Boeing Model 757 series airplanes, that requires repetitive detailed inspections of the support brackets and associated fasteners for the hydraulic lines located in the nacelle struts, and related investigative and corrective actions as necessary. This action also provides an optional terminating action for the repetitive inspections. This action is necessary to prevent flammable fluids from leaking into the interior compartment of the nacelle struts where ignition sources exist, which could result in the ignition of flammable fluids and an uncontained fire. This action is intended to address the identified unsafe condition.
Airworthiness Directives; McDonnell Douglas Model MD-11 and MD-11F Airplanes Equipped With Pratt & Whitney PW4000 Series Engines
The FAA is adopting a new airworthiness directive (AD) for certain McDonnell Douglas Model MD-11 and MD-11F airplanes equipped with Pratt & Whitney PW4000 series engines. This AD requires, for each engine, replacing, with a tube assembly, the existing hose assembly that connects the oil pressure transmitter to the main oil circuit. This AD is prompted by a report indicating that, for each engine, the existing hose assembly does not meet zero-flow fireproof capability requirements. We are issuing this AD to prevent, if there is an engine fire, failure of the oil pressure indicator and the low-oil pressure warning, which could result in an unannounced shutdown of that engine; and oil leakage, which may feed the engine fire.
Airworthiness Directives; Empresa Brasileira de Aeronautica S.A. (EMBRAER) Model EMB-135BJ Series Airplanes
The FAA is adopting a new airworthiness directive (AD) for certain EMBRAER Model EMB-135BJ series airplanes. This AD requires modifying the electrical wiring for the ``stick pusher'' system. This AD is prompted by a report that the stick pushers are not being inhibited when the AP/PUSH/TRIM switches are activated, which can result in reduced controllability of the airplane if there is a system malfunction. We are issuing this AD to prevent reduced controllability of the airplane if the stick pusher system malfunctions.
Airworthiness Directives; Gippsland Aeronautics Pty. Ltd. Model GA8 Airplanes
The FAA adopts a new airworthiness directive (AD) for certain Gippsland Aeronautics Pty. Ltd. Model GA8 airplanes. This AD requires you to inspect the pilot and co-pilot control column wheels and aileron cable operating arm shafts for damage and, if damage is found, to repair the shafts or to replace the steel shafts with bronze shafts. We are issuing this AD to detect and correct damage of the pilot and co- pilot control wheels and aileron cable operating arm shafts. This damage could result in the aileron controls becoming stiff or locking, which could lead to loss of control of the airplane.
Airworthiness Directives; McDonnell Douglas Model DC-8-33 and -43 Airplanes; Model DC-8F-54 and DC-8F-55 Airplanes; and Model DC-8-50, -60, -60F, -70, and -70F Series Airplanes
The FAA proposes to supersede an existing airworthiness directive (AD) for certain McDonnell Douglas series airplanes. That AD currently requires repetitive inspections of the electrical connectors of the explosive cartridge wiring of the engine fire extinguisher containers to verify if the identification number labels are installed and legible; repetitive electrical tests of all explosive cartridge wiring of the engine fire extinguisher containers to verify proper installation and function; and corrective actions if necessary. This proposed AD would also require an inspection of the emergency shut off wire assembly; installation of lanyards on the electrical connectors for the engine fire extinguishing agent containers and for the auxiliary power unit fire extinguishing agent containers if applicable; and related investigative/corrective actions, as applicable. This proposed AD is prompted by reports of cross-wired electrical connectors of the engine fire extinguishing agent containers. We are proposing this AD to detect and correct cross-wired electrical connectors of the fire extinguishing system, which could release fire extinguishing agent into the incorrect engine nacelle in the event of an engine fire.
Airworthiness Directives; Boeing Model 757-200, -200PF, and -300 Series Airplanes, Powered by Pratt & Whitney PW2000 Series Engines
The FAA proposes to adopt a new airworthiness directive (AD) for certain Boeing Model 757 series airplanes. This proposed AD would require repetitive inspections for loose or damaged components of the support brackets and associated fasteners for the hydraulic lines located in the nacelle struts, and any related investigative and corrective actions. This proposed AD is prompted by reports of damage and subsequent failure of the support brackets and associated fasteners for the hydraulic lines located internal to the upper fairing cavity of the nacelle struts. We are proposing this AD to prevent flammable fluids from leaking into the interior compartment of the nacelle struts where ignition sources exist, which could result in the ignition of flammable fluids and an uncontained fire.
Airworthiness Directives; Boeing Model 757-200, -200PF, and -200CB Series Airplanes Equipped With Pratt & Whitney or Rolls Royce Engines
The FAA proposes to adopt a new airworthiness directive (AD) for certain Boeing Model 757-200, -200PF, and -200CB series airplanes. This proposed AD would require inspecting to determine the part number of the upper link forward fuse pins of the engine struts; and replacing the fuse pins as necessary. This proposed AD is prompted by a report indicating that, due to an incorrect listing in the illustrated parts catalog, persons performing maintenance on the engine strut(s) could have installed an incorrect upper link forward fuse pin. We are proposing this AD to prevent a ruptured wing box, due to the engine not separating safely during certain emergency landing conditions, which could lead to a fuel spill and consequent fire.
Airworthiness Directives; Boeing Model 747-200B, -200C, -200F, and -400F Series Airplanes
The FAA proposes to adopt a new airworthiness directive (AD) for certain Boeing Model 747 series airplanes. This proposed AD would require repetitive detailed inspections for cracks in the crease beam and adjacent structure of the fuselage, and related investigative and corrective actions if necessary. This proposed AD is prompted by fatigue cracks found in the crease beam during a follow-on inspection of a previously installed modification. We are proposing this AD to find and fix fatigue cracking of the fuselage frame, which could result in reduced structural integrity of the frame and consequent rapid decompression of the airplane.
Program To Permit Cost-Sharing of Air Traffic Modernization Projects Guidance 2005
The FAA is authorized to approve up to 10 air traffic modernization cost share projects per year under Vision 100Century of Aviation Reauthorization Act, (Vision 100), Public Law 108-176, Section 183. The initial cost-share program was conducted under the authorization of Public Law 106-181, Section 304 of the Wendell H. Ford Aviation and Investment Reform Act for the 21st Century (AIR-21). Under the Vision 100, section 183 the FAA is now issuing program guidance based upon the lessons learned from the pilot program implementation. This guidance is to inform potential sponsors of the cost share program, the process to apply for the program and the criteria for approval for cost-sharing projects for this fiscal year. The purpose of Vision 100, Section 183 is to improve aviation safety and enhance mobility of the Nation's air transportation system by encouraging non- Federal investment in air traffic control facilities and equipment. Under this program, the Secretary of Transportation may make grants to eligible project sponsors. Each eligible project is limited to Federal funding as highlighted in section 2.3.1 with the Federal cost share not to exceed 33 percent of the project's facilities and equipment (excluding operations and maintenance) cost. A project sponsor means any major user of the National Airspace System as determined by the Secretary, including a public-use airport or a joint venture between a public-use airport and one or more U.S. air carriers.
Termination of Review of Noise Compatibility Program, Jackson International Airport, Jackson, MS
The Federal Aviation Administration (FAA) announces it has terminated its review of the noise compatibility program, at the request of the Jackson Municipal Airport Authority, under the provisions of 49 U.S.C. 47501 et seq., and 14 CFR Part 150.
Standard Instrument Approach Procedures; Miscellaneous Amendments
This amendment establishes, amends, suspends, or revokes Standard Instrument Approach Procedures (SIAPs) 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.
Airworthiness Directives; Airbus Model A319, A320, and A321 Series Airplanes
This amendment adopts a new airworthiness directive (AD), applicable to all Airbus Model A319, A320, and A321 series airplanes, that requires operators to revise the Airworthiness Limitations section (ALS) of the Instructions for Continued Airworthiness to incorporate new and more restrictive service life limits for certain items, and new and more restrictive inspections to detect fatigue cracking, accidental damage, or corrosion in certain structures. The actions specified by this AD are intended to ensure the continued structural integrity of these airplanes. This action is intended to address the identified unsafe condition.
Airworthiness Directives; Raytheon Aircraft Company 90, 99, 100, 200, and 300 Series Airplanes
This document makes a correction to Airworthiness Directive (AD) 2005-01-04, which was published in the Federal Register on January 6, 2005 (70 FR 1169) and applies to certain Raytheon Aircraft Company 90, 99, 100, 200, and 300 series airplanes. We incorrectly referenced an airplane model number in the applicability section of this AD. This action corrects the applicability section of AD 2005-01-04, Amendment 39-13928.
Notice of Intent To Rule on Application 05-10-C-00-PLN To Impose and Use the Revenue From a Passenger Facility Charge (PFC) at Pellston Regional Airport, Pellston, MI
The FAA proposes to rule and invites public comment on the application to impose and use the revenue from a PFC at Pellston Regional Airport under the provisions of the 49 U.S.C. 40117 and part 158 of the Federal Aviation Regulations (14 CFR part 158).
Notice of Opportunity To Self-Correct Annual Authorizations for Commercial Air Tour Operators Over National Parks and Tribal Lands Within or Abutting National Parks
On October 25, 2002, the Federal Aviation Administration (FAA) published the final rule for Title 14, Code of Federal Regulations (14 CFR) part 136, National Parks Air Tour Management (67 FR 65662). The rule became effective on January 23, 2003. In accordance with the provisions of the National Parks Air Tour Management Act of 2000, the final rule stated that the commercial air tour operators granted interim operating authority (IOA) would be published in the Federal Register for notice and the opportunity for comment. Based on information received from multiple sources and our own review, the FAA believes there may be some errors in the number of commercial air tours initially reported to the FAA. Thus, the FAA believes it is in the public interest to provide an opportunity for air tour operators to review and self-correct their annual authorizations prior to issuing the statutorily required notice. This notice announces the self- correcting opportunity and procedure. Responses should be provided to the contact person below by February 21, 2005.
Notice of Intent To Rule on Request To Release Airport Property Monroe Regional Airport, Monroe, LA
The FAA proposes to rule and invites public comment on the release of land at Monroe Regional Airport under the provisions of section 125 of the Wendell H. Ford Aviation Investment Reform Act for the 21st Century (AIR 21).
Airworthiness Directives; Pratt & Whitney JT8D-209, -217, -217A, -217C, and -219 Series Turbofan Engines
The FAA is superseding an existing airworthiness directive (AD) for Pratt & Whitney (PW) JT8D-209, -217, -217A, -217C, and -219 series turbofan engines. That AD currently requires torque inspection of the 3rd stage and 4th stage low pressure turbine (LPT) blades for shroud notch wear and replacement of the blade if wear limits are exceeded. This AD continues to require those torque inspections at shorter inspection intervals of the refurbished 3rd stage and 4th stage LPT blades, but the same or longer inspection intervals of the new 3rd stage and 4th stage LPT blades, for shroud notch wear and replacement of the blade if wear limits are exceeded. This AD also requires replacing LPT-to-exhaust case bolts and nuts with bolts and nuts made of Tinidur material. This AD results from reports of 194 blade fractures since 1991, with 37 of those blade fractures resulting in LPT case separation, and three reports of uncontained 3rd stage and 4th stage LPT blade failures with cowl penetration. We are issuing this AD to prevent an uncontained blade failure that could result in damage to the airplane.
Airworthiness Directives; Rolls-Royce plc RB211 Series Turbofan Engines
The FAA is superseding an existing airworthiness directive (AD) for Rolls-Royce (RR) plc RB211-535E4-37, RB211-535E4-B-37, and RB211-535E4-B-75 series turbofan engines. That AD currently requires initial and repetitive ultrasonic inspections of installed LPC fan blade roots on-wing and during overhaul using a surface wave ultrasonic probe, and relubrication, according to accumulated life cycles. That AD also adds the application of Metco 58 blade root coating as an optional terminating action. This AD requires the same actions, but changes the reference to Mandatory Service Bulletin (MSB) No. RB.211-72-C879 from Revision 3 to Revision 4. This AD results from RR issuing MSB No. RB.211-72-C879, Revision 4, which contains revised Accomplishment Instructions and consumable materials list. We are issuing this AD to detect cracks in low pressure compressor (LPC) fan blade roots, which if not detected, could lead to uncontained multiple fan blade failure, and damage to the airplane.
Proposed Establishment of Class E2 Airspace; and Modification of Class E5 Airspace; Newton, KS
This action corrects a notice of proposed rulemaking that was published in the Federal Register on Friday, January 7, 2005, (70 FR 1399) [FR Doc. 05-374]. It corrects errors in the legal descriptions of the proposed Class E airspace area designated as a surface area and the Class E airspace area extending upward from 700 feet above the surface at Newton, KS.
Notice of Intent To Release Certain Properties From all Terms, Conditions, Reservation and Restrictions of a Quitclaim Deed Agreement Between the City of Fernandina Beach and the Federal Aviation Administration for the Fernandina Beach Municipal Airport, Fernandina Beach, FL
The FAA hereby provides notice of intent to release certain airport properties (approximately 28.43 acres) at the Keystone Airpark, Starke, FL from the conditions, reservations, and restrictions as contained in a Quitclaim Deed agreement between the FAA and the Town of Keystone Heights, dated August 21, 1947. The release of property will allow the Keystone Airpark Authority to dispose of the property for other than aeronautical purposes. The property is located in the southwest corner of the airport west of State Road 100 in proximity to the approach of Runway 4. The parcel is currently designated as non- aeronautical use. The property will be disposed of for the purpose of conveying title to the United States Department of the Interior for the protection of the Florida National Scenic Trail. The fair market value of the property has been determined by appraisal to be $410,000. The airport will receive fair market value for the property, which will be subsequently reinvested in another eligible airport improvements project. Documents reflecting the Sponsor's request are available, by appointment only, for inspection at the Airpark Clerk's office and the FAA Airports District Office.
Airworthiness Directives; Boeing Model 767-200, -300, and -300F Series Airplanes
The FAA is adopting a new airworthiness directive (AD) for certain Boeing Model 767-200, -300, and -300F series airplanes. This AD requires repetitive high frequency eddy current inspections and detailed inspections of the left and right butt line (BL) 25 vertical chords for cracks, and corrective actions if necessary. This AD is prompted by findings of cracks in the fillet radii of the left and right BL 25 vertical chords common to the nose wheel well bulkhead at station 287. We are issuing this AD to detect and correct cracks in the left and right BL 25 vertical chords, which could grow downward into a critical area that serves as a primary load path for the nose landing gear (NLG) and result in the collapse of the NLG during landing.
Airworthiness Directives; Raytheon Model HS.125 Series 700A Airplanes, Model BAe.125 Series 800A Airplanes, and Model Hawker 800 and Hawker 800XP Airplanes
The FAA proposes to adopt a new airworthiness directive (AD) for certain Raytheon Model HS.125 series 700A airplanes, Model BAe.125 series 800A airplanes, and Model Hawker 800 and Hawker 800XP airplanes. This proposed AD would require an inspection to determine the current rating of the circuit breakers of certain cockpit ventilation and avionics cooling system blowers; and for replacing the circuit breakers and modifying the blower wiring, as applicable. This proposed AD is prompted by a report indicating that a blower motor seized up and gave off smoke. Investigation revealed inadequate short circuit protection on the blower motor electrical circuit. We are proposing this AD to prevent smoke and fumes in the cockpit in the event that a blower motor seizes and overheats due to excessive current draw.
Airworthiness Directives; Boeing Model 737-600, -700, -700C, -800, and -900 Series Airplanes
The FAA proposes to adopt a new airworthiness directive (AD) for certain Boeing Model 737-600, -700, -700C, -800, and -900 series airplanes. This proposed AD would require repetitive general visual inspections for dirt, debris, and drain blockage and cleaning of the aft fairing cavities of the engine struts; and modification of the aft fairings, which would terminate the repetitive general visual inspections. This proposed AD is prompted by a report indicating that water had accumulated in the cavities of the engine strut aft fairings. We are proposing this AD to prevent drain blockage by debris that, when combined with leaking, flammable fluid lines passing through the engine strut aft fairing, could allow flammable fluids to build up in the cavity of the aft fairing, and consequently could be ignited by the engine exhaust nozzle located below the engine strut, resulting in an explosion or uncontrolled fire.
Airworthiness Directives; Pratt & Whitney JT8D-200 Series Turbofan Engines; Correction
This document makes a correction to Airworthiness Directive (AD) 2004-26-04. That AD applies to Pratt & Whitney (PW) JT8D-200 series turbofan engines. That AD was published in the Federal Register on January 5, 2005 (70 FR 677). This document corrects a compliance time in Table 1 of the AD. In all other respects, the original document remains the same.
Airworthiness Directives; McDonnell Douglas Model MD-10-10F, MD-10-30F, MD-11F, DC-10-10F, and DC-10-30F Airplanes
The FAA is adopting a new airworthiness directive (AD) for the McDonnell Douglas airplanes listed above. This AD requires identifying the part number of the cargo compartment smoke detectors and, if necessary, revising the Limitations section of the airplane flight manual to include procedures for testing the smoke detection system after the last engine is started. This AD also provides for the optional replacement of the subject smoke detectors with modified smoke detectors, which would terminate the operational limitation. This AD is prompted by a report indicating that the cargo smoke detectors can ``lock up'' during electrical power transfer from the auxiliary power unit to the engines. We are issuing this AD to identify and provide corrective action for a potentially inoperative smoke detector in the cargo compartment and ensure that the flightcrew is alerted in the event of a cargo compartment fire.
Notice of Availability for the O'Hare Modernization Draft Environmental Impact Statement, Chicago O'Hare International Airport, Chicago, IL; Notice of Availability; and Notice of Public Hearing Dates, Times, and Locations
The Federal Aviation Administration (FAA) announces that the O'Hare Modernization Draft Environmental Impact Statement for Chicago O'Hare International Airport, Chicago, Illinois is available for public review and comment. The DEIS identifies alternatives intended to address the projected needs of the Chicago region by reducing delays at O'Hare, thereby enhancing capacity of the National Airspace System, and ensuring that terminal facilities and supporting infrastructure can efficiently accommodate airport users. All of the development alternatives would result in wetland, property acquisition, air quality and noise impacts, as well as other impacts. The FAA intends to host public hearings on the DEIS with the U.S. Army Corps of Engineers (USACE) and the Illinois Environmental Protection Agency (IEPA) Bureau of Water. The public hearings on the DEIS will be held on the following dates: Tuesday, February 22, 2005, at the Avalon Banquets, 1905 East Higgins Road, Elk Grove Village, Illinois 60007; Wednesday, February 23, 2005, at the Waterford Conference Center, 933 South Riverside Drive, Elmhurst, Illinois 60126; and Thursday, February 24, 2005, at the White Eagle, 6839 North Milwaukee Avenue, Niles, Illinois 60714. All three of these hearings will start at 2 p.m. (central standard time), and registration to participate in the hearings will conclude by 9 p.m. (central standard time). Repressentatives of FAA, USACE and IEPA will be available to provide information about the DEIS at an informational session held at the same time as the public hearings. Spanish language translators will be available at the hearings. The procedural rules governing the hearing are available from Michael W. MacMullen. The comment period is open as of the date of this Notice of Intent and closes Wednesday, March 23, 2005. All comments are to be submitted to Michael W. MacMullen of the FAA, at the address shown below. The USACE and IEPA have requested that the FAA be the recipient of all comments regarding their actions. These comments must be sent to Michael W. MacMullen of the FAA at the address shown below, and the comments must be postmarked and email must be sent by no later than midnight, Wednesday, March 23, 2005. The USACE is participating in the public hearings because implementation of any development alternatives, if selected, would require the USACE to approve issuance of a permit to fill wetlands under section 404 of the Clean Water Act Section. The IEPA is participating in the public hearings because implementation of any wetland development alternative, if selected, would also require IEPA to issue a Water Quality Certification under section 401 of the Clean Water Act.
Proposed Establishment of Class E Airspace; Cocoa Beach Patrick AFB, FL
This notice proposed to establish Class E4 airspace at Cocoa Beach Patrick AFB, FL. Class E4 airspace designated as an extension to Class D airspace is required when the control tower is open to contain existing Standard Instrument Approach Procedures (SIAPs) and other Instrument Flight Rules (IFR) operations at the airport. This action would establish a Class E4 airspace extension that is 6.8 miles wide and extends 7.3 miles northeast of the airport. This airspace is currently being protected by Notice to Airmen.
Availability of Final Environmental Impact Statement and Final Air Quality Conformity Determination for Los Angeles International Airport, Los Angeles, Los Angeles County, CA
The Federal Aviation Administration (FAA) along with the Federal Highway Administration is issuing this notice to advise the public that a Final Environmental Impact Statement (EIS) and Final General Conformity Determination has been prepared for the proposed Master Plan Improvements at Los Angeles International Airport (LAX), Los Angeles, Los Angeles County, California. FAA is seeking comments on revised and updated information and analyses disclosed in Volume A of the Final EIS and related appendices (Appendices A-1, A-2a, A-2b, A-3a, A-3b, A-3c, A-3d, and A-4).
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