Department of Transportation August 23, 2006 – Federal Register Recent Federal Regulation Documents

Requested Administrative Waiver of the Coastwise Trade Laws
Document Number: E6-13974
Type: Notice
Date: 2006-08-23
Agency: Maritime Administration, Department of Transportation
As authorized by Pub. L. 105-383 and Pub. L. 107-295, the Secretary of Transportation, as represented by the Maritime Administration (MARAD), is authorized to grant waivers of the U.S.- build requirement of the coastwise laws under certain circumstances. A request for such a waiver has been received by MARAD. The vessel, and a brief description of the proposed service, is listed below. The complete application is given in DOT docket 2006-25655 at https:// dms.dot.gov. Interested parties may comment on the effect this action may have on U.S. vessel builders or businesses in the U.S. that use U.S.-flag vessels. If MARAD determines, in accordance with Pub. L. 105- 383 and MARAD's regulations at 46 CFR Part 388 (68 FR 23084; April 30, 2003), that the issuance of the waiver will have an unduly adverse effect on a U.S.-vessel builder or a business that uses U.S.-flag vessels in that business, a waiver will not be granted. Comments should refer to the docket number of this notice and the vessel name in order for MARAD to properly consider the comments. Comments should also state the commenter's interest in the waiver application, and address the waiver criteria given in Sec. 388.4 of MARAD's regulations at 46 CFR Part 388.
Requested Administrative Waiver of the Coastwise Trade Laws
Document Number: E6-13973
Type: Notice
Date: 2006-08-23
Agency: Maritime Administration, Department of Transportation
As authorized by Pub. L. 105-383 and Pub. L. 107-295, the Secretary of Transportation, as represented by the Maritime Administration (MARAD), is authorized to grant waivers of the U.S.- build requirement of the coastwise laws under certain circumstances. A request for such a waiver has been received by MARAD. The vessel, and a brief description of the proposed service, is listed below. The complete application is given in DOT docket 2006-25656 at https:// dms.dot.gov. Interested parties may comment on the effect this action may have on U.S. vessel builders or businesses in the U.S. that use U.S.-flag vessels. If MARAD determines, in accordance with Pub. L. 105- 383 and MARAD's regulations at 46 CFR part 388 (68 FR 23084; April 30, 2003), that the issuance of the waiver will have an unduly adverse effect on a U.S.-vessel builder or a business that uses U.S.-flag vessels in that business, a waiver will not be granted. Comments should refer to the docket number of this notice and the vessel name in order for MARAD to properly consider the comments. Comments should also state the commenter's interest in the waiver application, and address the waiver criteria given in Sec. 388.4 of MARAD's regulations at 46 CFR part 388.
Maintenance and Repair Reimbursement Pilot Program
Document Number: E6-13971
Type: Proposed Rule
Date: 2006-08-23
Agency: Maritime Administration, Department of Transportation
The Maritime Administration (MARAD) is amending its regulations governing its pilot program for the reimbursement of costs of qualified maintenance and repair (M&R) of Maritime Security Program (MSP) vessels performed in United States shipyards. Under Public Law 109-163, the Secretary of Transportation, acting through the Maritime Administrator, is directed to implement regulations that, among other things, replace MARAD's voluntary M&R reimbursement program with a mandatory system. The notice of proposed rulemaking for this action was published in the Federal Register on February 8, 2006 (71 FR 6438). Several of the comments received argued that MARAD lacks authority to unilaterally add to existing MSP agreements the added obligation on the part of the MSP contractor to enter into an M&R Pilot Program agreement. In order to have a full airing of this fundamental issue, MARAD is hereby giving notice that we have decided to open a reply comment period for this rulemaking. Reply comments may address the issue highlighted above or any other issue raised in the original set of comments received in this docket.
Airworthiness Directives; Airbus Model A300 B2 and B4 Series Airplanes
Document Number: E6-13964
Type: Proposed Rule
Date: 2006-08-23
Agency: Federal Aviation Administration, Department of Transportation
The FAA proposes to adopt a new airworthiness directive (AD) for certain Airbus Model A300 B2 and B4 series airplanes. This proposed AD would require revising the airplane flight manual (AFM) to include procedures for resetting the trim and pitch trim levers after each landing, determining which servomotor moves the pitch trim control wheel, and doing applicable other specified actions. This proposed AD also provides for optional terminating actions for those requirements. This proposed AD results from a report of a sudden nose-up movement after disengagement of the autopilot in cruise. We are proposing this AD to ensure that the flightcrew is aware of the procedures for resetting the trim and pitch trim levers after each landing and to prevent failure of the servomotors of the pitch trim systems during flight. Failure of the servomotors of the pitch trim systems could result in uncommanded nose-up movement of the control surface of the pitch trim systems after disengagement of the autopilot in cruise.
Notice of Order Extending Comment Period for Show-Cause; International Air Transport Association Tariff Conference Proceeding
Document Number: E6-13958
Type: Notice
Date: 2006-08-23
Agency: Office of the Secretary, Department of Transportation
The Department has directed all interested persons to show cause why it should not issue an order withdrawing its approval under 49 U.S.C. 41309 for an International Air Transport Association (``IATA'') agreement, the Provisions for the Conduct of the IATA Traffic Conferences, insofar as that agreement establishes tariff conferences whereby IATA's member carriers discuss and agree upon passenger fares and cargo rates for U.S.-Australia/Europe markets. The Department is extending the due date for comments on that order from August 21 to October 20, 2006. Replies will be due November 20, 2006.
Exemptions From Average Fuel Economy Standards; Passenger Automobile Average Fuel Economy Standards
Document Number: E6-13957
Type: Proposed Rule
Date: 2006-08-23
Agency: National Highway Traffic Safety Administration, Department of Transportation
This proposed decision responds to a petition filed by Spyker Automobielen B.V. (Spyker) requesting that it be exempted from the generally applicable average fuel economy standard of 27.5 miles per gallon (mpg) for model years 2006 and 2007, and that, for Spyker, lower alternative standards be established. In this document, NHTSA proposes that the requested exemption be granted to Spyker and that alternative standards of 18.9 mpg be established for MY's 2006 and 2007.
Procedures for Transportation Workplace Drug and Alcohol Testing Programs: Revision of Substance Abuse Professional Credential Requirement; Technical Amendments
Document Number: E6-13956
Type: Rule
Date: 2006-08-23
Agency: Office of the Secretary, Department of Transportation
The Department of Transportation is adding state-licensed or certified marriage and family therapists to the list of credentialed professionals eligible to serve as substance abuse professionals under subpart O of 49 CFR part 40. The Department is also making a series of technical amendments to its drug and alcohol testing procedural rule. The purpose of the technical amendments is to clarify certain provisions of the rule as well as address omissions and typographical errors which have been called to our attention since the publication of the final rule in December 2000.
Airworthiness Directives; RECARO Aircraft Seating GmbH & Co. (RECARO) Model 3410 Seats
Document Number: E6-13911
Type: Rule
Date: 2006-08-23
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new airworthiness directive (AD) for certain RECARO Model 3410 302, 303, 306, 307, 314, 316, 317, 791, 792, and 795 series seats. This AD requires replacing the existing attachment bolts for the seat belts with longer attachment bolts. This AD results from a report of short attachment bolts that don't allow enough thread to properly secure the locknuts. We are issuing this AD to prevent a seat belt from detaching due to a loose locknut and attachment bolt, which could result in injury to an occupant during emergency conditions.
Airworthiness Directives; Rolls-Royce plc RB211 Series Turbofan Engines
Document Number: E6-13910
Type: Rule
Date: 2006-08-23
Agency: Federal Aviation Administration, Department of Transportation
This amendment supersedes an existing airworthiness directive (AD), that is applicable to Rolls-Royce plc (RR) models RB211-535E4-37, RB211-535E437, RB211-535C-37, RB211-535E4-B-75, RB211-535E4-C, and RB211-22B-02 turbofan engines. That AD currently requires inspecting certain high pressure (HP) turbine discs, manufactured between 1989 and 1999, for cracks in the rim cooling air holes, and, if necessary, replacing the discs with serviceable parts. The manufacturer identified reaming-induced machining anomalies (RIMA) as the cause for the cracking. This amendment requires the same inspections, and reduces the compliance times for eddy current inspection (ECI) for the RR RB211- 22B-02 engines. This amendment results from the manufacturer reducing their recommended compliance times for inspections on RB211-22B-02 engines. We are issuing this AD to prevent possible disc failure, which could result in an uncontained engine failure and damage to the airplane.
Airworthiness Directives; Pratt & Whitney PW4077D, PW4084D, PW4090, and PW4090-3 Turbofan Engines
Document Number: E6-13909
Type: Rule
Date: 2006-08-23
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new airworthiness directive (AD) for Pratt & Whitney (PW) PW4077D, PW4084D, PW4090, and PW4090-3 turbofan engines that were reassembled with certain previously used high pressure compressor (HPC) exit brush seal assembly parts and certain new or refurbished HPC exit diffuser air seal inner lands. This AD requires replacing the HPC exit inner and outer brush seal packs with new brush seal packs, or replacing the HPC exit brush seal assembly with a new HPC exit brush seal assembly. This AD results from a report of oil leaking into the high pressure turbine (HPT) interstage cavity and igniting, leading to an engine case penetration and engine in- flight shutdown. Although liberated engine parts did not penetrate the engine nacelle, we are issuing this AD to prevent uncontained engine failure, damage to the airplane, and injury to passengers.
Airworthiness Directives; Bombardier Model CL-600-2B19 (Regional Jet Series 100 & 440) Airplanes
Document Number: E6-13831
Type: Rule
Date: 2006-08-23
Agency: Federal Aviation Administration, Department of Transportation
The FAA is superseding an existing airworthiness directive (AD) that applies to certain Bombardier Model CL-600-2B19 (Regional Jet Series 100 & 440) airplanes. The existing AD currently requires inspecting contactors 1K4XD, 2K4XD, and K4XA to determine the type of terminal base plate, and applying sealant on the terminal base plates, if necessary. This new AD revises the effective date of the existing AD. This AD results from incidents of short circuit failures of certain alternating current (AC) contactors located in the avionics bay. We are issuing this AD to prevent short circuit failures of certain AC contactors, which could result in arcing and consequent smoke or fire.
Airworthiness Directives; Bombardier Model DHC-8-100, DHC-8-200, and DHC-8-300 Series Airplanes
Document Number: E6-13829
Type: Rule
Date: 2006-08-23
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new airworthiness directive (AD) for certain Bombardier Model DHC-8-100, DHC-8-200, and DHC-8-300 series airplanes. This AD requires repetitive inspections of the fluorescent light tube assemblies of the cabin, lavatory, and sidewall, and corrective actions if necessary. This AD also provides for optional terminating action for the repetitive inspections. This AD results from reports of overheating due to arcing between the fluorescent tube pins and the lamp holder contacts. The tubes had not been properly seated during installation. We are issuing this AD to prevent fumes, traces of visible smoke, and fire at the fluorescent light tube assembly.
Airworthiness Directives; Boeing Model 767-400ER Series Airplanes and Model 777-200 and -300 Series Airplanes
Document Number: E6-13825
Type: Rule
Date: 2006-08-23
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new airworthiness directive (AD) for certain Boeing Model 767-400ER series airplanes and Model 777-200 and - 300 series airplanes. This AD requires, for certain airplanes, repetitive testing of the fill and safety fittings of the cargo fire extinguishing bottles in the forward cargo compartment for leaks; and repetitive application of a corrosion inhibiting compound (CIC) or replacement of the cargo fire extinguishing bottles with reworked fire extinguishing bottles, as necessary. For all airplanes, this AD requires replacement of the cargo fire extinguishing bottles with reworked fire extinguishing bottles, which ends the repetitive tests and CIC applications if applicable. This AD results from failure of the safety fittings for the cargo fire extinguishing bottles. We are issuing this AD to prevent failure of the safety fittings for the cargo fire extinguishing bottles due to corrosion, which could result in leakage of extinguishing agent. If a fire occurs in the cargo bay, the cargo fire extinguishing bottles could have less than enough extinguishing agent to control a fire.
Revision of Class E Airspace; Barter Island, AK
Document Number: E6-13803
Type: Rule
Date: 2006-08-23
Agency: Federal Aviation Administration, Department of Transportation
This action revises Class E airspace at Barter Island, AK to provide adequate controlled airspace to contain aircraft executing two new Standard Instrument Approach Procedures (SIAPs) and one amended SIAP. This rule results in revised Class E airspace established upward from 700 feet (ft.) and 1,200 ft. above the surface at Barter Island Airport, AK.
Canadian Charter Air Taxi Operators
Document Number: E6-13664
Type: Rule
Date: 2006-08-23
Agency: Office of the Secretary, Department of Transportation
DOT is updating its rule concerning Canadian charter air taxis to make the rule consistent with the 1995 U.S.-Canada bilateral aviation agreement. When promulgated in 1981, the rule comported with the 1974 U.S.-Canada bilateral aviation agreement governing non- scheduled air services. However, the rule has not been updated to reflect the more liberal 1995 bilateral. Consequently, the rule, in its current form, contains certain restrictions on Canadian charter air taxis that are contrary to the 1995 bilateral. This final rule eliminates or amends those provisions. It also makes several other technical changes to the rule and adds a provision making it clear that Canadian charter air taxis are exempt from the statutory requirement of foreign air carriers to file family assistance plans.
Modification of Class E Airspace; Half Moon Bay, CA
Document Number: 06-7062
Type: Rule
Date: 2006-08-23
Agency: Federal Aviation Administration, Department of Transportation
This action modifies the Class E airspace area at Half Moon Bay, CA. The establishment of an Area Navigation (RNAV) Global Positioning System (GPS) Z Instrument Approach Procedure (IAP) to Runway (RWY) 30 to Half Moon Bay Airport, Half Moon Bay, CA has made this action necessary. Additional controlled airspace extending upward from 700 feet or more above the surface of the earth is needed to contain aircraft executing this RNAV (GPS) ZIAP to RWY 30 at Half Moon Bay Airport. The intended effect of this action is to provide adequate controlled airspace for Instrument Flight Rules operations at Half Moon Bay Airport, Half Moon Bay, CA
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