Department of Transportation April 7, 2005 – Federal Register Recent Federal Regulation Documents

Agency Information Collection; Activity Under OMB Review; Report of Financial and Operating Statistics for Large Certificated Air Carriers
Document Number: 05-6954
Type: Notice
Date: 2005-04-07
Agency: Department of Transportation, Research & Innovative Technology Administration, Research and Innovative Technology Administration
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 currently approved collections. The ICR describes the nature of the information collection and its expected burden. The Federal Register Notice with a 60-day comment period soliciting comments on the following collection of information was published on December 17, 2004 (69 FR 75603).
Agency Information Collection Activities; Request for Comments; Clearance of a New Information Collection; Freight Planning Noteworthy Practices
Document Number: 05-6951
Type: Notice
Date: 2005-04-07
Agency: Federal Highway Administration, Department of Transportation
The FHWA has forwarded the new information collection request described in this notice to the Office of Management and Budget (OMB) for review and approval. We published a Federal Register notice with a 60-day public comment period on this information collection on August 10, 2004 (69 FR 48556). We are required to publish this notice in the Federal Register by the Paperwork Reduction Act of 1995.
Release of Waybill Data
Document Number: 05-6927
Type: Notice
Date: 2005-04-07
Agency: Surface Transportation Board, Department of Transportation
Airworthiness Directives; Eurocopter France Model AS350B, BA, B1, B2, B3, D, and AS355E Helicopters
Document Number: 05-6917
Type: Proposed Rule
Date: 2005-04-07
Agency: Federal Aviation Administration, Department of Transportation
This document proposes adopting a new airworthiness directive (AD) for the specified Eurocopter France (ECF) model helicopters. This proposal would require replacing the hydraulic fluid at a specified time interval when operating in cold weather. This proposal is prompted by reports of ice forming due to condensation in some parts of the hydraulic system during cold weather operation. The actions specified by this proposed AD are intended to prevent ice from forming in the hydraulic system resulting in an unintended movement of the flight controls and subsequent loss of control of the helicopter.
Airworthiness Directives; Bombardier Model CL-600-2B16 (CL-604) Series Airplanes
Document Number: 05-6916
Type: Proposed Rule
Date: 2005-04-07
Agency: Federal Aviation Administration, Department of Transportation
The FAA withdraws a notice of proposed rulemaking (NPRM) that proposed a new airworthiness directive (AD) for certain Bombardier Model CL-600-2B16 (CL-604) series airplanes. The proposed AD would have required replacing the side-brace fitting shafts of the main landing gear (MLG) with new, improved side-brace fitting shafts; inspecting for corrosion of the MLG side-brace fitting shafts; and replacing the nut, washer, and cotter pin of the MLG side-brace fitting shafts with new parts; as applicable. Since the proposed AD was issued, we have received new data that the actions that would have been required by the proposed AD have already been accomplished on all of the affected airplanes. Accordingly, the proposed AD is withdrawn.
Airworthiness Directives; McDonnell Douglas Model DC-10-10, DC-10-10F, DC-10-15, DC-10-30, DC-10-30F (KC-10A and KDC-10), DC-10-40, DC-10-40F, MD-10-10F, MD-10-30F, MD-11, and MD-11F Airplanes
Document Number: 05-6910
Type: Proposed Rule
Date: 2005-04-07
Agency: Federal Aviation Administration, Department of Transportation
The FAA proposes to adopt a new airworthiness directive (AD) for certain McDonnell Douglas airplanes identified above. This proposed AD would require repetitive functional tests for noisy or improper operation of the exterior emergency control handle assemblies of the mid, overwing, and aft passenger doors, and corrective actions if necessary. This proposed AD also would provide for optional terminating action for the repetitive tests. This proposed AD is prompted by a report that the exterior emergency control mechanism handles were inoperative on a McDonnell Douglas MD-11 airplane. We are proposing this AD to prevent failure of the passenger doors to operate properly in an emergency condition, which could delay an emergency evacuation and possibly result in injury to passengers and flightcrew.
Airworthiness Directives; Empresa Brasileira de Aeronautica S.A. (EMBRAER) Model ERJ 170 Series Airplanes
Document Number: 05-6909
Type: Rule
Date: 2005-04-07
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 series airplanes. This AD requires revising the Limitations section of the airplane flight manual to advise the flightcrew to make sure the correct instrument landing system (ILS) identifier is included on the flight management system (FMS) flight plan before the flightcrew initiates an approach to landing with the autopilot engaged. This AD is prompted by reports that the airplane's autopilot may apply large- amplitude control inputs while following ILS guidance to a runway that is not included on the FMS flight plan. We are issuing this AD to prevent hazardous maneuvers close to the ground, which could result in an impact with an obstacle or terrain.
Over-the-Road Bus Accessibility Program Grants
Document Number: 05-6856
Type: Notice
Date: 2005-04-07
Agency: Federal Transit Administration, Department of Transportation
The U.S. Department of Transportation (DOT) Federal Transit Administration (FTA) announces the availability of funds in fiscal year (FY) 2005 for the Over-the-Road Bus (OTRB) Accessibility Program, authorized by section 3038 of the Transportation Equity Act for the 21st Century (TEA-21). The OTRB Accessibility Program makes funds available to private operators of over-the-road buses to finance the incremental capital and training costs of complying with DOT's over- the-road bus accessibility final rule, 49 CFR part 37, published in a Federal Register notice on September 28, 1998 (63 FR 51670). The authorizing legislation calls for national solicitation of applications, with grantees to be selected on a competitive basis. Federal transit funds are available to intercity fixed-route providers and other OTRB providers at up to 90 percent of the project cost. In FY 2005, $5,208,000 was appropriated for intercity fixed-route service providers and $1,686,400 was appropriated for other over-the- road bus service providers. This announcement is available on the Internet on the FTA Web site at: https://www.fta.dot.gov. FTA will announce final selections on the Web site and in the Federal Register. A synopsis of this announcement will be posted in the FIND module of the government-wide electronic grants Web site at https://www.grants.gov. Applications may be submitted to FTA in hard copy or electronically through the GRANTS.GOV APPLY function.
Airworthiness Directives; Boeing Model 737-100, -200C, -300, -400, and -500 Series Airplanes
Document Number: 05-6763
Type: Rule
Date: 2005-04-07
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new airworthiness directive (AD) for all Boeing Model 737-100, -200, -200C, -300, -400, and -500 series airplanes. This AD requires repetitive inspections for cracks in the fuselage skin, doubler, bearstrap, and frames surrounding the main, forward, and aft cargo doors; and repair of any cracking. This AD also requires inspections of certain existing repairs for cracking, and related corrective action if cracking is found. This AD is prompted by reports of multiple fatigue cracks in the fuselage skin and bonded skin doubler, bearstrap, and doorway frames surrounding the forward and aft cargo doors. We are issuing this AD to find and fix fatigue cracking in the fuselage skin, doubler, bearstrap, and frames, which could result in reduced structural integrity of the frames, possible loss of a cargo door, and consequent rapid decompression of the fuselage.
Airworthiness Directives; Boeing Model 737-600, -700, -800, and -900 Series Airplanes
Document Number: 05-6762
Type: Rule
Date: 2005-04-07
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new airworthiness directive (AD) for certain Boeing Model 737-600, -700, -800, and -900 series airplanes. This AD requires installing and testing an updated version of the operational program software of the flight control computers. This AD is prompted by a report of an airplane pitching up with rapidly decreasing indicated airspeed after the flightcrew set a new altitude into the autopilot. We are issuing this AD to prevent anomalous autopilot operation that produces a hazardous combination of airplane attitude and airspeed, which could result in loss of control of the airplane.
Airworthiness Directives; Boeing Model 767-300 and -400ER Series Airplanes
Document Number: 05-6689
Type: Rule
Date: 2005-04-07
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new airworthiness directive (AD) for certain Boeing Model 767-300 and -400ER series airplanes. This AD requires replacing the in-flight entertainment cooling card, located in the P50 card file in the main equipment center, with a new, improved cooling card. This AD is prompted by a report of an improperly designed component on the in-flight entertainment (IFE) cooling card, which may cause the IFE cooling system to incorrectly interpret signals from airplane system interfaces. We are issuing this AD to prevent failure of the IFE cooling card to configure itself correctly in response to input signals from airplane system interfaces during a forward cargo fire, which could result in the IFE cooling fan causing smoke to penetrate occupied areas of the airplane.
Airworthiness Directives; Boeing Model 737-100, -200, -200C, -300, -400, and -500 Series Airplanes
Document Number: 05-6688
Type: Rule
Date: 2005-04-07
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new airworthiness directive (AD) for certain Boeing Model 737-100, -200, -200C, -300, -400, and -500 series airplanes. This AD requires repetitive detailed and eddy current inspections to detect cracking of the frame web around the cutout for the doorstop intercostal strap at the aft side of the body station 291.5 frame at stringer 16R, and corrective actions if necessary. This AD is prompted by reports of fatigue cracks in the web of the body station 291.5 frame near the forward galley door. We are issuing this AD to detect and correct fatigue cracking of the aft frame and frame support structure of the forward galley door, which could result in a severed fuselage frame web, rapid decompression of the airplane, and possible loss of the forward galley door.
Airworthiness Directives; Bombardier Model DHC-8-102, -103, -106, -201, -202, -301, -311, and -315 Airplanes
Document Number: 05-6687
Type: Rule
Date: 2005-04-07
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new airworthiness directive (AD) for certain Bombardier Model DHC-8-102, -103, -106, -201, -202, -301, -311, and-315 airplanes. This AD requires revising the airplane flight manual to include applicable procedures to follow when the flightcrew receives abnormal indications of airspeed, altitude, or vertical airspeed. This AD also requires modifying the static system. This 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 issuing 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; Bombardier Model CL-600-2B19 (Regional Jet Series 100 & 440) Airplanes
Document Number: 05-6686
Type: Rule
Date: 2005-04-07
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 and 440) airplanes. This AD requires modification of the Auxiliary Power Unit (APU) cooling air exhaust. This AD is prompted by reports of incomplete drainage of the APU enclosure. We are issuing this AD to prevent a negative pressure condition from developing in the APU enclosure when the APU is operating on the ground, which could create a potential fire hazard if flammable liquid leakage occurs inside the APU enclosure and cannot be drained overboard.
Airworthiness Directives; Airbus Model A318, A319, A320, and A321 Series Airplanes
Document Number: 05-6685
Type: Rule
Date: 2005-04-07
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new airworthiness directive (AD) for all Airbus Model A318, A319, A320, and A321 series airplanes. This AD requires an inspection of the spoiler servo control for certain part numbers, and corrective action if necessary. This AD is prompted by a report of a broken piston rod bearing of the spoiler servo control. We are issuing this AD to prevent breakage of the piston rod bearing, which could cause loss of the associated hydraulic system and spoiler extension, and could result in reduced controllability of the airplane.
Airworthiness Directives; Boeing Model 767-400ER, 777-200, and 777-300 Series Airplanes
Document Number: 05-6684
Type: Rule
Date: 2005-04-07
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new airworthiness directive (AD) for certain Boeing Model 767-400ER, 777-200, and 777-300 series airplanes. This AD requires replacing, with new parts, the existing tie-down fitting studs that secure galleys, purser work stations, and closets to the seat tracks. This AD is prompted by a report that tie-down fitting studs were found damaged. We are issuing this AD to prevent a galley, purser work station, or closet from detaching from the tie-down fitting studs during an emergency landing, which could injure passengers or crewmembers, or obstruct escape routes and impede emergency evacuation.
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