Department of Transportation 2005 – Federal Register Recent Federal Regulation Documents

This action corrects an error in the legal description of a direct final rule, request for comments that was published in the Federal Register on Friday, July 29, 2005 (70 FR 43744).

The FAA is adopting a new airworthiness directive (AD) for certain Airbus Model A300 B4-620, A310-304, A310-324, and A310-325 airplanes. This AD requires installing fused adaptors between the external wiring harness and the in-tank wiring at the connectors on the fuel tank wall of the auxiliary center tank (ACT). This AD results from fuel system reviews conducted by the manufacturer. We are issuing this AD to prevent an ignition source in the ACT, which, in combination with flammable fuel vapors, could result in a fuel tank explosion and consequent loss of the airplane.

The FAA is adopting a new airworthiness directive (AD) for all BAE Systems (Operations) Limited Model ATP airplanes. This AD requires one-time inspections for corrosion of the engine sub-frame tubes in zone 1 and of the engine attachment struts in zone 5, and corrective action if necessary. This AD results from reports of reduced thickness in localized areas of the engine sub-frame tubes due to corrosion, and reports that corrosion may also exist in the engine attachment struts in zone 5. We are issuing this AD to prevent failure of the engine sub- frame tubes or the engine attachment struts, which could result in separation of an engine from the airplane.

The FAA is adopting a new airworthiness directive (AD) for certain Fokker Model F27 Mark 050 airplanes. This AD requires repetitive visual checks for oil leaks of both engines between the spinner and the engine cowling, and directly behind the heated intake lip of the engine; repetitive inspections for oil leaks at the feathering pump on both engines; and corrective actions if necessary. This AD results from reports of oil leakage at the engine feathering pump. We are issuing this AD to prevent oil loss from the feathering pump, which could cause the engine to shut down in flight.

The Federal Aviation Administration invites public comment on proposed Advisory Circular (AC) 25-XX, ``Subpart I, Continued Airworthiness and Safety Improvements.'' This proposed AC provides generic guidance, which is applicable to the safety initiatives in the proposed Subpart I (i.e., Enhanced Airworthiness Program for Airplane Systems, Reduction of Fuel Tank Flammability in Transport Category Airplanes, Aging Airplane Safety, and Widespread Fatigue Damage), on the roles and responsibilities of type certificate and supplemental type certificate holders, manufacturers, owners, and operators. 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.

This notice announces the availability of and requests comments on a proposed advisory circular (AC) that sets forth acceptable methods of compliance with Sec. 25.1362 concerning electrical wiring. This proposed AC complements revisions to the airworthiness standards that are being proposed by a separate notice. This notice is necessary to give all interested persons an opportunity to present their views on the proposed AC.

This notice announces the availability of and requests comments on a proposed advisory circular (AC) that sets forth acceptable methods of compliance with Sec. 25.1357 concerning electrical wiring. This proposed AC complements revisions to the airworthiness standards that are being proposed by a separate notice. This notice is necessary to give all interested persons an opportunity to present their views on the proposed AC.

This notice announces the availability of and requests comments on a proposed advisory circular (AC) that sets forth acceptable methods of compliance with Sec. 25.899 concerning electrical wiring. This proposed AC complements revisions to the airworthiness standards that are being proposed by a separate notice. This notice is necessary to give all interested persons an opportunity to present their views on the proposed AC.

This notice announces the availability of and requests comments on a proposed advisory circular (AC) that sets forth acceptable methods of developing a training program for electrical wiring interconnection systems. This proposed AC complements revisions to the airworthiness standards that are being proposed by a separate notice. This notice is necessary to give all interested persons an opportunity to present their views on the proposed AC.

This notice announces the availability of and requests comments on a proposed advisory circular (AC) that sets forth acceptable methods of compliance with 14 CFR part 25, subpart H, sections Sec. Sec. 25.1701 through 25.1739 and sections H25.4 and H25.5 of Appendix H to part 25. This proposed AC complements revisions to the airworthiness standards that are being proposed by a separate notice. This notice is necessary to give all interested persons an opportunity to present their views on the proposed AC.

This document presents interpretive guidance material for the Federal Motor Carrier Safety Regulations (FMCSRs). FMCSA issues new regulatory guidance for Forms MCS-90, MCS-90B, MCS-82, and MCS-82B used to establish minimum levels of financial responsibility of motor carriers. The questions and answers are applicable to motor carrier operations on a national basis. This guidance will provide the motor carrier and financial services industries and Federal, State, and local law enforcement officials with a clearer understanding of the applicability in particular situations of Forms MCS-90, MCS-90B, MCS- 82, and MCS-82B contained in the FMCSRs.

The FAA proposes to adopt a new airworthiness directive (AD) for certain Lycoming Engines (formerly Textron Lycoming) 360 and 540 series reciprocating engines with ECi connecting rods, part number (P/ N) AEL 11750, installed. This proposed AD would require replacing certain serial-numbered connecting rods, P/N AEL 11750. This proposed AD would also prohibit installing certain ECi connecting rods, P/N AEL 11750 into any Lycoming 360 or 540 series reciprocating engines. This proposed AD results from reports of connecting rods with excessive variation in circularity of the journal bores. We are proposing this AD to prevent fatigue failure of the connecting rod and uncommanded shutdown of the engine.

The FAA is rescinding an existing airworthiness directive (AD) that applies to Honeywell FMS one million word (1M or 700K) data bases (9104 cycle or earlier) as installed in, but not limited to McDonnell Douglas Model MD-11 and MD-11F airplanes, Boeing Model 747-400 series airplanes, and Boeing Model 757 and 767 airplanes. That AD requires a revision to the FAA-approved Airplane Flight Manual (AFM) and installation of a placard to prohibit the use of Nondirectional Beacon (NDB) approaches for landing. That AD was prompted by an anomaly in the Honeywell FMS one million word (1M or 700K) data bases (9104 cycle or earlier). We issued that AD to prevent an airplane deviating from the published approach to the runway, which could lead to premature ground contact before reaching the runway. Since we issued that AD, we have determined that the Honeywell FMS one million word (1M or 700K) databases (9104 cycle or earlier) no longer exist on any of the affected airplanes.

The FAA proposes to adopt a new airworthiness directive (AD) for all Glaser-Dirks Flugzeugbau GmbH Models DG-100 and DG-400 sailplanes and certain DG Flugzeugbau GmbH Models DG-500 Elan Series and DG-500M sailplanes. This proposed AD would require you to modify or replace the complete rudder mount assembly and ensure that the securing washer, castellated nut, and new split pins are installed. This proposed AD results from mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Germany. We are issuing this proposed AD to prevent the universal bearing of the lower rudder mounting from slipping out of the bearing support. The universal bearing slipping out could result in the rudder separating from its support. This failure could lead to loss of sailplane control during flight operations.

The FAA is adopting a new airworthiness directive (AD) for certain Boeing Model 737-100, -200, and -200C series airplanes. This AD requires a one-time detailed inspection for cracking of the lugs of the inboard attach fittings of the wing leading edge slat tracks at slat numbers 2 and 5; prior or concurrent actions for certain airplanes; repetitive high-frequency eddy current (HFEC) inspections for cracking of the lug surfaces of those inboard attach fittings if necessary; and replacement of the attach fittings with new, improved fittings. This AD results from reports of damage to the lugs of certain inboard attach fittings of the leading edge slat tracks. We are issuing this AD to prevent a lifted slat, which, if the airplane performs any non-normal maneuver during takeoff or landing at very high angles of attack, could lead to the loss of the slat and reduced control of the airplane.

The FAA is superseding two existing airworthiness directives (AD), which apply to certain Boeing transport category airplanes. One AD currently requires doing certain inspections to detect cracks and corrosion around the lower bearing of the actuator attach fittings of the inboard and outboard flaps; repairing if necessary; and either overhauling the fittings or replacing them, which ends certain repetitive inspections. The other AD currently requires certain other inspections to detect discrepancies of the actuator attach fittings of the flaps, and follow-on and corrective actions if necessary, which ends the repetitive inspections of the first AD. For certain airplanes, this AD requires new inspections for discrepancies of the actuator attach fittings of the flaps, and follow-on and corrective actions if necessary, which ends the repetitive inspections of both existing ADs. For all airplanes, this AD requires repetitive overhaul/replacements of the actuator attach fittings of both the inboard and outboard flaps. This AD results from reports of cracks of the actuator attach fittings of the trailing edge flaps. We are issuing this AD to prevent cracking and other damage of the actuator attach fittings of the trailing edge flaps, which could result in abnormal operation or retraction of a trailing edge flap, and possible loss of controllability of the airplane.

These special conditions are issued for Dassault-Aviation Mystere-Falcon 50 airplanes modified by Premier Air Center. 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 Universal Avionics EFI-890 Electronic Flight Displays and Rockwell Collins AHS-3000A Attitude Heading Reference Systems (AHRS) that 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.

These special conditions are issued for the Boeing Model 720B airplane. The airplane will have novel and unusual design features when compared to the state of technology envisioned in the airworthiness standards for transport category airplanes. The modification incorporates the installation of dual Honeywell AM-250 digital altimeters. 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 provided by the existing airworthiness standards.

This action proposes to revise a segment of Jet Route J-158 between the Malad City, ID, Very High Frequency Omni-directional Range/ Distance Measuring Equipment (VOR/DME) and the Muddy Mountain, WY, Very High Frequency Omni-directional Range/Tactical Air Navigation (VORTAC). Specifically, the FAA is proposing to realign the route from Malad City, ID, to Big Piney, WY, VOR/DME to Muddy Mountain, WY. This proposed action would replace the sector taken out of service, reduce controller workload, and enhance the National Airspace System.

The Coast Guard and the Maritime Administration (MARAD) announce the cancellation of an Environmental Assessment (EA) that they previously planned as a follow-up to MARAD's approval of the license application for the Port Pelican LLC Deepwater Port in the Gulf of Mexico off Louisiana. The EA would have assessed the environmental impact of related shoreside fabrication site activities in Texas. The Coast Guard and MARAD are canceling the EA, due to Port Pelican LLC's decision to defer these fabrication site activities indefinitely.

This document responds to a petition for reconsideration of the August 24, 2004 final rule that amended regulations pertaining to the importation by registered importers (RIs) of motor vehicles that were not originally manufactured to comply with all applicable Federal motor vehicle safety, bumper, and theft prevention standards. The agency is not adopting the changes requested in the petition, except for one asking the agency to allow RIs to import motor vehicles that have been modified to comply with the Theft Prevention Standard and one asking the agency to allow an imported nonconforming motor vehicle to be operated on public roads prior to bond release solely for the purpose of conducting required EPA testing. Also, the agency has decided to eliminate the requirement for applicants for RI status to submit to the agency the social security numbers of its principals.

The National Park Service (NPS) and Federal Aviation Administration (FAA), in accordance with the National Parks Air Tour Management Act of 2000, announce the next meeting of the National Parks Overflights Advisory Group Aviation Rulemaking Committee (NPOAG ARC. This notice informs the public of the date, location, and agenda for the meeting. Dates and Location: The NPOAG ARC will meet November 8-9, 2005, at the Stanley Hotel, Estes Park, 333 Wonderview Ave, Estes Park, CO 80517. The meeting will begin at 8 a.m. on Tuesday, November 8, 2005.