Federal Aviation Administration 2005 – Federal Register Recent Federal Regulation Documents

The Federal Aviation Administration (FAA) is issuing this notice to advise the public that a Final Environmental Impact Statement (FEIS)Proposed New Runways and Associated Development at Washington Dulles International Airport, has been prepared and is available for public review and comment. The FEIS incorporates a Final Air Quality General Conformity Determination (FGCD), (Preliminary) Final Section 106 Historic Resources Report and a Virginia Coastal Zone Consistency Determination. Written requests for the FEIS and written comments on the FEIS and related documents can be submitted to the individual listed in the section FOR FURTHER INFORMATION CONTACT. The EPA 30-day Hold Period and FEIS comment period will commence on August 19, 2005, and will close on September 19, 2005. FEIS Availability: Copies of the FEIS and related documents may be viewed during regular business hours at the following locations: 1. Centreville Regional Library, 14200 St. Germaine Drive, Centreville, VA. 2. Chantilly Regional Library, 4000 Stringfellow Road, Chantilly, VA. 3. Great Falls Library, 9830 Georgetown Pike, Great Falls, VA. 4. Herndon Fortnightly Library, 768 Center Street, Herndon, VA. 5. Reston Regional Library, 11925 Bowman Towne Drive, Reston, VA. 6. Fairfax City Regional Library, 3915 Chain Bridge Road, Fairfax, VA. 7. Ashburn Library, 43316 Hay Road, Ashburn, VA. 8. Rust Library, 380 Old Waterford Road, Leesburg, VA. 9. Middleburg Library, 101 Reed Street, Middleburg, VA. 10. Purcellville Library, 220 E. Main Street, Purcellville, VA. 11. Sterling Library, 120 Enterprise Street, Sterling, VA. 12. Eastern Loudoun Regional Library, 21030 Whitfield Place, Sterling, VA. 13. Tysons-Pimmit Regional Library, 7584 Leesburg Pike, Falls Church, VA. A limited number of copies of the FEIS and related documents will also be available for review by appointment only at the following FAA/ Metropolitan Washington Airports Authority (MWAA) Offices. Please call to make arrangements for viewing: Federal Aviation Administration, Washington Airports District Office, 23723 Air Freight Lane, Suite 210, Dulles, VA, (703) 661-1368; Washington Dulles International Airport, Airport Managers Office, Main Terminal Baggage Claim Level, Dulles, VA, (703) 572-2710. An Executive Summary will be available August 13, 2005 on Dulles Airport's Web site at https://www.mwaa.com/dulles/ EnvironmentalStudies/RunwaysEIS.htm.

The Federal Aviation Administration (FAA) announces the availability of final policy on Replacing Restraint Systems on Forward and Aft Facing Seats.

The FAA proposes to adopt a new airworthiness directive (AD) for certain EMBRAER Model ERJ 170 airplanes. This proposed AD would require replacing the very high frequency (VHF) antenna located in position 1 of the fuselage with a new, improved VHF antenna. This proposed AD results from a report of the loss of all voice communications due to a lightning strike damaging all the VHF antennas. We are proposing this AD to prevent the loss of voice communication, which when combined with the complexity of the national airspace system, could result in reduced flightcrew situational awareness, increased flightcrew workload, and increased risk of human error, and consequent reduced ability to maintain safe flight and landing of the airplane.

In compliance with the Paperwork Reduction Act of 1995 (44 U.S.C. 3501 et seq.), this notice announces that the Information Collection Requests (ICR) abstracted below have been forwarded to the Office of Management and Budget (OMB) for extension of the currently approved collections. The ICR describes the nature of the information collection and the expected burden. The Federal Register Notice with a 60-day comment period soliciting comments on the following collections of information was published on May 25, 2005, page 30180.

The FAA proposes to adopt a new airworthiness directive (AD) for certain Shadin ADC-2000 air data computers (ADC) installed on airplanes. This proposed AD would require you to replace affected ADC- 2000 units with a modified unit. This proposed AD results from reports that certain ADC-2000 units display incorrect altitude information on the Electronic Flight Information System (EFIS) to the pilot. We are issuing this proposed AD to prevent ADC-2000 units, part numbers (P/Ns) 962830A-1-S-8, 962830A-2-S-8, and 962830A-3-S-8, configurations B, C, and D, from displaying incorrect altitude information. This could cause the flight crew to react to this incorrect flight information and possibly result in an unsafe operating condition.

The FAA is revising an earlier NPRM for an airworthiness directive (AD) that applies to certain EMBRAER airplane models as identified above. The original NPRM would have required modifying the total air temperature (TAT) sensor heating system. The original NPRM was prompted by a report indicating that the fully automated digital electronic control (FADEC) unit failed to compensate for ice accretion on the engine fan blades due to a false temperature signal from the TAT sensor to the FADEC. This action revises the original NPRM by requiring modification of additional electrical connections for the TAT sensor heating system. This action also would expand the applicability of the original NPRM because the additional electrical connections must be modified on airplanes that had the TAT sensor heating system modified previously (e.g., in production). This action also adds replacing the FADEC assemblies with new or modified assemblies as an additional means of compliance. We are proposing this supplemental NPRM to prevent failure of the TAT sensor, which could result in insufficient thrust to take off or (if coupled with the loss of an engine during takeoff) to abort the takeoff in a safe manner, and consequent reduced controllability of the airplane.

Pursuant to FAA's rulemaking provisions governing the application, processing, and disposition of petitions for exemption part 11 of Title 14, Code of Federal Regulations (14 CFR), this notice contains a summary of certain petitions seeking relief from specified requirements of 14 CFR. The purpose of this notice is to improve the public's awareness of, and participation in, this aspect of FAA's regulatory activities. Neither publication of this notice nor the inclusion or omission of information in the summary is intended to affect the legal status of any petition or its final disposition.

The FAA is withdrawing a notice of proposed rulemaking (NPRM). That NPRM proposed a new airworthiness directive (AD) that applies to certain Rolls-Royce plc (RR) models RB211-535C-37, RB211-535E4-37, RB211-535E4-B-37, and RB211-535E4-B-75 turbofan engines. The NPRM had applied to those engines with radial drive steady bearing part number (P/N) LK76084 installed, with fewer than 3,000 engine operating hours on the bearing. That proposed action would have required initial and repetitive visual inspections of the engine oil scavenge filter for evidence of radial drive steady bearing failure. If after finding evidence, the proposed action would have required a visual inspection of the radial drive steady bearing for damage and evidence of bearing debris. Since we issued that NPRM, RR notified us that all at-risk radial drive steady bearings are removed from service. RR also notified us that remaining bearings in service are now well over the 3,000- engine-operating-hour threshold and are no longer at risk. Accordingly, we withdraw the proposed rule.

The FAA is requesting public comment on the City of Beverly, Massachusetts' request to change 10.3 acres of vacant land located in the approach to Runway 34 to industrial use. The land will be sold to an abutter for expansion of a manufacturing building. The land was acquired under FAAP 9-19-026-D603. 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.

The Federal Aviation Administration (FAA) is giving notice that a portion of the airport property will be exchanged with the Southern Illinois University. A portion of the property to be exchanged (.0254 acre) was originally acquired in fee on July 20, 1948, with partial Federal funding. The remaining property (.7266 acre was acquired by Southern Illinois Airport Authority (SIAA) on August 16, 2001, in a previous exchange with the Southern Illinois University (SIU). This release will be an even exchange of land (.752+/-acre) between SIAA and SIU. The Exhibit `A' Property Line Map (Exhibit 1) and the Airport Layout Plan (Exhibit 2) depicts the exchange. The University proposes to construct four (4) buildings which will result in the new Transportation Education Center at the airport. The sponsor anticipates greater future opportunities for the airport due to the reputation of the University and its renowned programs. It has been determined that one of the buildings will cause a line-of-site obstruction with the Air Traffic Control Tower if it is built in its proposed location. In order to eliminate the conflict, an even exchange of the property and a different construction location has been proposed. In accordance with section 47107(h) of title 49, United States Code, this notice is required to be published in the Federal Register 30 days before modifying the land-use assurance that requires that property to be used for an aeronautical purpose.

The FAA is adopting a new airworthiness directive (AD) for all Gulfstream Model G-IV and GV series airplanes, and certain GIV-X and GV-SP series airplanes. This AD requires a one-time inspection to determine if a certain floor heater pad system is installed, and deactivation of the subject floor heater pad system if it is installed. This AD results from an incident of short-circuiting of the floor heater pads, in which no circuit breakers tripped in response to the short-circuiting. We are issuing this AD to prevent short-circuiting of the floor heater pad system, which could result in a fire in the airplane cabin.

The FAA adopts a new airworthiness directive (AD) for all Pilatus Aircraft Ltd. (Pilatus) (also identified as Fairchild Republic Company and Fairchild Heli Porter) Model PC-6 airplanes. This AD requires you to repetitively inspect the stabilizer-trim attachment and structural components for cracks, corrosion, and discrepancies and replace any defective part with a new part. This AD also requires you to replace all Fairchild connecting pieces, part number (P/N) 6232.0026.XX, with a Pilatus connecting piece and requires you to replace fittings without an index after the P/N with an improved part. This AD results from mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Switzerland. We are issuing this AD to detect and correct defective stabilizer-trim attachments and surrounding structural components, which could result in failure of the stabilizer-trim attachment. This failure could lead to loss of control of the airplane.

This notice announces the availability of AC 45-2C, Identification and Registration Marking. AC 45-2C provides information and guidance concerning the requirements for identifying aircraft and related products with identification plates, and identifying aircraft with nationality and registration marks. The requirements are detailed in Title 14, Code of Federal Regulations (14 CFR), part 45, Identification and Registration Marking.

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.

The FAA is adopting a new airworthiness directive (AD) for Rolls-Royce Deutschland Ltd & Co KG (RRD) (formerly Rolls-Royce Deutschland GmbH, formerly BMW Rolls-Royce GmbH) model BR700-715A1-30, BR700-715B1-30, and BR700-715C1-30 turbofan engines. This AD requires a onetime inspection of the Independent Overspeed Protection (IOP) unit, part number (P/N) 112E9321G2, for 19 specific serial numbers (SNs), and removal from service of those units. This AD results from a report that incorrect capacitors were installed in 19 IOP units. The incorrect capacitor in the IOP unit can lead to an inadvertent IOP command resulting in an in-flight engine shutdown. We are issuing this AD to prevent inadvertent dual-engine in-flight shutdown.

The FAA is revising an earlier NPRM for an airworthiness directive (AD) that applies to certain EMBRAER Model EMB-135 and -145 series airplanes. The original NPRM would have required 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; and would also have provided for optional terminating action for the repetitive inspections. The original NPRM was prompted by a report of a fractured axle of the trailing arm of the MLG due to corrosion of the axle. This action revises the original NPRM by expanding the applicability and by providing final terminating action for the repetitive detailed inspections. We are proposing this supplemental NPRM 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 takeoff or landing.

The FAA is issuing this notice to advise the public of a meeting of RTCA Special Committee 200/EUROCAE Working Group 60: Modular Avionics.

This action proposes special conditions for a Boeing Model 747-400 airplane modified by Lufthansa Technik AG. This airplane will have a novel or unusual design feature associated with the installation of large non-structural glass items in the cabin area of an executive interior occupied by passengers and crew. The proposed installation of these items in a passenger compartment, which can be occupied during taxi, takeoff, and landing, is a novel or unusual design feature with respect to the material used. 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.

The FAA publishes a monthly notice, as appropriate, of PFC approvals and disapprovals under the provisions of the Aviation Safety and Capacity Expansion Act of 1990 (Title IX of the Omnibus Budget Reconciliation Act of 1990) (Pub. L. 101-508) and Part 158 of the Federal Aviation Regulations (14 CFR Part 158). This notice is published pursuant to paragraph d of Sec. 158.29.

In compliance with the Paperwork Reduction Act of 1995 (44 U.S.C. 3501 et seq.), this notice announces that the Information Collection Request (ICR) abstracted below has been forwarded to the Office of Management and Budget (OMB) for extension of the currently approved collections. The ICR describes the nature of the information collection and the expected burden. The Federal Register Notice with a 60-day comment period soliciting comments on the following collection of information was published on April 12, 2005, page 19144.

The FAA publishes a monthly notice, as appropriate, of PFC approvals and disapprovals under the provisions of the Aviation Safety and Capacity expansion Act of 1990 (Title IX of the Omnibus Budget Reconciliation Act of 1990) (Pub. L. 101-508) and Part 158 of the Federal Aviation Regulations (14 CFR Part 158). This notice is published pursuant to paragraph d of Sec. 158.29.

The FAA is revising an existing airworthiness directive (AD), which applies to certain Boeing Model 757-200, 757-200CB, and 757-200PF series airplanes. That AD currently requires repetitive inspections to detect horizontal or vertical movement of the shims at the joint of the mid-bulkhead and the upper link fittings; repetitive inspections for cracking of the mid-bulkhead; and corrective action if necessary. That AD also provides optional terminating action for the repetitive inspections. This AD continues to require the existing requirements and optional actions and clarifies certain terminating actions. This AD results from comments received in response to an existing AD, requesting clarification. We are issuing this AD to detect and correct migration of shims at the joint of the mid-bulkhead and the upper link fittings and cracking of the mid-bulkhead, which could result in cracking of the strut and consequent loss of the strut and engine.

The FAA proposes to adopt a new airworthiness directive (AD) for all Przedsiebiorstwo Doswiadczalno-Produkcyjne Szybownictwa ``PZL- Bielsko'' Model SZD-50-3 ``Puchacz'' gliders. This proposed AD would require you to perform a visual inspection of the turnbuckle link for cracks or wear and replace if cracks or wear is found. This proposed action would only apply to those gliders where the turnbuckle is directly connected to the pedal. This proposed AD results from mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Poland. We are issuing this proposed AD to detect and correct cracks in the turnbuckle link, which could result in failure of the rudder cable. This failure could lead to loss of control of the glider.

This notice proposes special conditions for the Airbus A380- 800 airplane. This airplane will have novel or unusual design features when compared to the state of technology envisioned in the airworthiness standards for transport category airplanes. Many of these novel or unusual design features are associated with the complex systems and the configuration of the airplane, including its full- length double deck. For these design features, the applicable airworthiness regulations do not contain adequate or appropriate safety standards regarding flotation and ditching. 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. Additional special conditions will be issued for other novel or unusual design features of the Airbus Model A380-800 airplane.