Department of Transportation 2005 – Federal Register Recent Federal Regulation Documents
Results 2,051 - 2,100 of 3,378
Special Conditions: Bombardier Aerospace Models BD-700-1A10 and BD-700-1A11 Global Express Airplanes, Enhanced Flight Visibility System (EFVS)
These special conditions are issued for the Bombardier Aerospace Models BD-700-1A10 and BD-700-1A11 Global Express airplanes. These airplanes, as modified by Bombardier Aerospace Corporation, will have an Enhanced Flight Visibility System (EFVS). The EFVS is a novel or unusual design feature which consists of a head up display (HUD) system modified to display forward-looking infrared (FLIR) imagery. The regulations applicable to pilot compartment view 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 provided by the existing airworthiness standards.
Proposed Amendment to VOR Federal Airway V-536; MT
This action proposes to modify Federal Airway V-536 by adding a route from the Great Falls, MT, Very High Frequency Omnidirectional Range/Tactical Air Navigation (VORTAC) to the SWEDD intersection. The purpose of the proposed airway segment is to enhance the management of aircraft transiting between Great Falls, MT, and Bozeman, MT.
Establishment of Class E Airspace; McGregor, MN
This action establishes Class E airspace at McGregor, MN. Standard Instrument Approach Procedures have been developed for McGregor/Isedor Iverson Airport, McGregor, MN. Controlled airspace extending upward from 700 feet or more above the surface of the earth is needed to contain aircraft executing these approach procedures. This action establishes an area of controlled airspace for McGregor/Isedor Iverson Airport.
Proposed Establishment of Class E Airspace; Chehalis, WA
This proposal would establish Class E airspace at Chehalis, WA. Additional Class E airspace is necessary to accommodate aircraft using a new Area Navigation (RNAV) Global Positioning System (GPS) Standard Instrument Approach Procedure (SIAP) at Chehalis-Centralia Airport. This action is proposed to improve the safety of Instrument Flight Rules (IFR) aircraft executing the new RNAV GPS SIAP at Chehalis-Centralia Airport, Chehalis, WA.
Proposed Amendment to Class E Airspace; Blairstown, NJ
This notice proposes to amend the Class E airspace area at Blairstown, NJ. The development of a Standard Instrument Approach Procedure (SIAP) based on area navigation (RNAV) to serve flights into Blairstown Airport, Blairstown, NJ under Instrument Flight Rules (IFR) has made this proposal necessary. Controlled airspace extending upward from 700 feet Above Ground Level (AGL) is needed to contain aircraft executing the approach. The area would be depicted on aeronautical charts for pilot reference.
Establishment of Prohibited Area 51; Bangor, WA
This action establishes a prohibited area (P-51) over the U.S. Naval Submarine Base, at Bangor, WA. The prohibited area replaces a Temporary Flight Restriction (TFR) that is currently in effect. The FAA is taking this action in response to a request from the U.S. Navy as part of its efforts to enhance the security of the Naval Submarine Base, Bangor, WA.
Modification of Class E Airspace; Boonville, MO
This document confirms the effective date of the direct final rule which revises Class E airspace at Boonville, MO.
Modification of Class E Airspace Monett, MO; Correction
This action withdraws the Direct final rule, confirmation of effective date of a rule that was published in the Federal Register on Thursday, May 5, 2005 (70 FR 23790). The action was inadvertently published as a Direct final rule, confirmation of effective date when it should have been published as a final rule. It is replaced with a final rule. This rule establishes a Class E surface area at Monett, MO. It also modifies the Class E airspace area extending upward from 700 feet above the surface at Monett, MO. The effect of this rule is to provide appropriate controlled Class E airspace for aircraft departing from and executing instrument approach procedures to Monett Municipal Airport and to segregate aircraft using instrument approach procedures in instrument conditions from aircraft operating in visual conditions.
Modification of Class E Airspace; Washington, KS
This document confirms the effective date of the direct final rule which revises Class E airspace at Washington, KS.
Special Conditions: Embraer Model ERJ 190 Series Airplanes; Sudden Engine Stoppage, Interaction of Systems and Structures, Operation Without Normal Electrical Power, Electronic Flight Control Systems, Automatic Takeoff Thrust Control System (ATTCS), and Protection From Effects of High Intensity Radiated Fields (HIRF)
This notice proposes special conditions for the Embraer Model ERJ 190 series 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. These design features are associated with (1) engine size and torque load which affect sudden engine stoppage, (2) electrical and electronic systems which perform critical functions, and (3) an Automatic Takeoff Thrust Control Systems (ATTCS). These proposed special conditions also pertain to the effects of such novel or unusual design features, such as their effects on the structural performance of the airplane. The applicable airworthiness regulations do not contain adequate or appropriate safety standards for these design features. 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.
Civil Penalties
This document proposes to increase the maximum aggregate civil penalties for violations of statutes and regulations administered by NHTSA pertaining to odometer tampering and disclosure requirements and for vehicle theft protection violations. This action would be taken pursuant to the Federal Civil Monetary Penalty Inflation Adjustment Act of 1990, as amended by the Debt Collection Improvement Act of 1996, which requires us to review and, as warranted, adjust penalties based on inflation at least every four years.
Notice of Receipt of Petition for Decision That Nonconforming 1991 Mercedes Benz 560 SEL Passenger Cars Are Eligible for Importation
This document announces receipt by the National Highway Traffic Safety Administration (NHTSA) of a petition for a decision that 1991 Mercedes Benz 560 SEL passenger cars that were not originally manufactured to comply with all applicable Federal motor vehicle safety standards are eligible for importation into the United States because (1) they are substantially similar to vehicles that were originally manufactured for importation into and sale in the United States and that were certified by their manufacturer as complying with the safety standards, and (2) they are capable of being readily altered to conform to the standards.
Beacon Port LLC, Liquefied Natural Gas Deepwater Port License Application
The Coast Guard and the Maritime Administration (MARAD) announce that they have received an application for the licensing of a natural gas deepwater port, and that the application appears to contain the required information. This notice summarizes the applicant's plans and the procedures that will be followed in considering the application.
Environmental Impact Statement for Improved Station Access and Additional Parking at the MTA Metro-North Railroad North White Plains Station, Westchester County, NY
The FTA, in cooperation with the Metropolitan Transportation Authority (MTA) Metro-North Railroad (Metro-North) and the Westchester County Department of Transportation (WCDOT), intend to prepare an Environmental Impact Statement (EIS) on a proposal to improve station access and provide additional parking at the Metro-North North White Plains Station, Westchester County, New York (Proposed Action). The FTA is the lead Federal agency under the National Environmental Policy Act of 1969 (NEPA). The Proposed Action is being developed by Metro-North and WCDOT, the co-sponsors of the Proposed Action. The EIS will be prepared in accordance with NEPA and the applicable regulations for implementing NEPA, as set forth in 23 CFR part 771 and 40 CFR parts 1500-1508. The EIS is being prepared to satisfy the requirements of the New York State Environmental Quality Review Act (SEQRA). Items that will be considered in the Proposed Action are: Expansion of parking capacity through the construction of a multi-level parking structure at Metro-North's North White Plains Station; Improved access to/from the proposed expanded parking facilities from the east side of the railroad tracks; Enhanced customer service facilities for intermodal connections and parking demand management strategies such as: Jitney services, feeder buses supported by park-and-ride lots, carpool and vanpool arrangements, bicycling and walking; Restoration of a portion of the Bronx River Parkway Reservation which is currently used for customer parking back to parkland; and Rerouting a portion of the Bronx River Parkway Reservation bike pathway in the study area. The EIS will evaluate a build alternative, comprising a multi-level parking structure and four possible access alternatives, a No Action Alternative and any additional reasonable alternatives generated by the scoping process. Scoping will be accomplished through meetings and correspondence with interested persons, organizations, and Federal, State, regional, and local agencies.
Frontal New Car Assessment Program
The Transportation Recall Enhancement, Accountability, and Documentation (TREAD) Act required that a safety rating for child restraints be established to provide practicable, readily understandable, and timely information to consumers. In addition, the TREAD Act directed the Secretary of Transportation to consider placing child restraints in the rear seat of vehicles crash-tested under NCAP. In response to this mandate, NHTSA established a consumer information program for add-on child restraints based on their ease of use, and announced that it would perform two pilot programs to gather additional information about other aspects of child passenger safety. One pilot program would subject child restraints to a 48 km/h (30 mph) sled test. This program focused on the protection provided by the child restraint. The second pilot program placed child restraints in the rear seat of vehicles in frontal NCAP tests. This program focused on the protection the vehicle provided to properly restrained children. Based on the data collected from both pilot programs, the agency has decided not to implement a dynamic child restraint system (CRS) rating based on sled tests, and to continue collecting data from NCAP frontal crash tests to resolve some outstanding technical issues and to gather additional data on the Hybrid III 6-year-old and 10-year-old child dummies. In addition, the agency will develop a better understanding of the real world data and its relationship to NCAP child results. The agency will make a decision on the merits of a vehicle child protection rating in conjunction with any possible revisions to the frontal testing program, which the agency is currently evaluating. Privacy Act: Anyone is able to search the electronic form of all submissions received into any of our dockets by the name of the individual submitting the petition (or signing the petition, if submitted on behalf of an association, business, labor union, etc.). You may review DOT's complete Privacy Act Statement in the Federal Register published on April 11, 2000, (Volume 65, Number 70; Pages 19477-78) or you may visit https://dms.dot.gov.
Airworthiness Directives; Boeing Model 747-200C and 747-200F Series Airplanes
The FAA is adopting a new airworthiness directive (AD) for all Boeing Model 747-200C and 747-200F series airplanes. This AD requires repetitive inspections for cracking of the left and right C-3 frame upper closure fittings of the nose cargo door, and corrective actions if necessary. This AD also provides an optional modification that, if done, terminates inspections in certain areas. This AD is prompted by reports indicating that fatigue cracking was found in the inboard flange above the flight deck floor on the C-3 frame upper closure fittings of the nose cargo door. We are issuing this AD to detect and correct cracking of the C-3 frame upper closure fittings, which could extend and result in rapid depressurization of the airplane.
Airworthiness Directives; AeroSpace Technologies of Australia Pty Ltd. Models N22B, N22S, and N24A Airplanes
The FAA adopts a new airworthiness directive (AD) to supersede AD 2003-14-20, which applies to all AeroSpace Technologies of Australia Pty Ltd. (ASTA) Models N22B and N24A airplanes. AD 2003-14-20 requires you to repetitively inspect, using either dye penetrant or magnetic particle methods, the rudder control lever shafts for cracks; inspect (one-time) all lever shaft side plates by measuring the thickness; and if cracks or discrepancies in thickness are found, replace unserviceable parts with new or serviceable parts. Since AD 2003-14-20 was issued, we determined that the AD should also affect Model N22S airplanes. The manufacturer has also revised the service information to include a rudder control lever shaft part number (P/N) that was not part of AD 2003-14-20. Consequently, this AD retains the actions of AD 2003-14-20, adds Model N22S airplanes to the applicability, and adds rudder control lever shaft P/N 1/N-45-1102 to the inspection requirements. We are issuing this AD to detect and correct cracks in the rudder control lever torque shafts and discrepancies in the thickness of the lever shaft side plates, which could result in failure of the rudder control lever torque shaft. Such failure could lead to reduced controllability of the airplane.
Airworthiness Directives; DG Flugzeugbau GmbH Model DG-500MB Sailplanes and Glaser-Dirks Flugzeugbau GmbH Model DG-800B Sailplanes
The FAA adopts a new airworthiness directive (AD) for all DG Flugzeugbau GmbH Model DG-500MB sailplanes equipped with a Solo engine and Glaser-Dirks Flugzeugbau GmbH Model DG-800B sailplanes equipped with a Solo engine. This AD requires you to inspect the propeller for damage, specifically foam core separation, and replace any damaged propeller. This AD results from mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Germany. We are issuing this AD to detect and correct damage to the propeller, which could result in failure of the propeller to perform properly. This failure could lead to reduced or loss of control of the sailplane.
Pipeline Safety: Meetings of the Pipeline Safety Advisory Committees
This notice announces public meetings of Pipeline and Hazardous Materials Safety Administration's (PHMSA) Technical Pipeline Safety Standards Committee (TPSSC) and Technical Hazardous Liquid Pipeline Safety Standards Committee (THLPSSC) to discuss various regulatory issues.
Request for Public Comments and Office of Management and Budget (OMB) Approval of an Existing Information Collection (2137-0593)
This notice seeks comments from the public regarding notices gas service line operators must send customers about the availability of excess flow valves (EFVs) and related records operators must keep. The notices give customers information to help them decide if they would like to have EFVs installed on their lines. Comments will help OMB evaluate the information collection involving EFVs.
Pipeline Safety: Planning for Coordination of Emergency Response to Pipeline Emergencies
This document alerts pipeline operators about the need to preplan for emergency response with utilities whose proximity to the pipeline may impact the response. Coordination with electric and other utilities may be critical in responding to a pipeline emergency. Preplanning would facilitate actions that may be needed for safety, such as removing sources of ignition or reducing the amount of combustible material.
Request for Public Comments and Office of Management and Budget (OMB) Approval of an Existing Information Collection (2137-0594)
This notice seeks comments from the public regarding notices that gas pipeline operators must send customers about buried customer piping located downstream from service lines and the related records operators must keep. The notices inform customers about the need for proper maintenance of this piping. Comments will help OMB evaluate the information collection burden.
International Standards on the Transport of Dangerous Goods; Public Meetings
This notice is to advise interested persons that PHMSA will conduct public meetings in preparation for and to report the results of the 27th session of the United Nation's Sub-Committee of Experts on the Transport of Dangerous Goods (UNSCOE) to be held July 4-8, 2005 in Geneva, Switzerland.
Federal Motor Vehicle Safety Standards; Denial of Petition for Rulemaking
Based on the agency's evaluation, the National Highway Traffic Safety Administration (NHTSA) denies a petition for rulemaking from Mercedes-Benz to amend the Federal lighting standard to permit the use of optional use of stoplamps that would flash under higher levels of deceleration. Mercedes-Benz has not demonstrated that this manufacturer-installed option would result in reduced crashes. NHTSA is denying the petition because it would take away from NHTSA the ability to use a potentially valuable rear signal for a higher safety purpose sometime in the future. NHTSA concludes that it would require more in- depth information than provided on the safety benefit of any such change before it would initiate a rulemaking on what rear signal lamp performance changes are appropriate or necessary to reduce the incidence or rear-end crashes.
Galley Carts and Containers
This notice announces the availability of, and requests comment on proposed Technical Standard Order (TSO) C-175, Galley Carts and Containers. This proposed TSO tells persons seeking TSO authorization or letter of design approval what minimum performance standards (MPS) their galley carts and containers must meet to be identified with the appropriate TSO making.
Conducting Component Level Tests To Demonstrate Compliance
The Federal Aviation Administration (FAA) announces the availability of final policy on conducting component level tests in order demonstrate compliance with the requirements of Sec. Sec. 25.785(b) and (d).
Notice of Availability for the Draft O'Hare Modernization Section 303/4(f) and Section 6(f) Evaluation for Proposed New Runways and Associated Development at Chicago O'Hare International Airport, Chicago, IL
The Federal Aviation Administration (FAA) announces that the Draft O'Hare Modernization Section 303/4(f) and Section 6(f) Evaluation for the O'Hare Modernization Environmental Impact Statement is available for public review and comment. The Section 303/4(f) and Section 6(f) Evaluation can be obtained on the Web at https:// www.agl.faa.gov/OMP/DEIS.htm or the locations noted below. The Section 303/4(f) and Section 6(f) Evaluation documents the consideration of impacts to Section 303/4(f) lands and DOT Section 6(f) lands that could be impacted by build alternatives proposed at Chicago O'Hare International Airport. The proposed build alternatives are 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. The comment period is open as of the date of this Notice of Availability and closes July 5, 2005. Comments must be sent to Michael W. MacMullen of the FAA at the address shown below. Comments must be postmarked and emails must be sent no later than midnight, July 5, 2005.
Environmental Impact Statement: Nueces County, TX
The FHWA is issuing this notice to advise the public that an environmental impact statement (EIS) will be prepared for the proposed U.S. Highway (US) 181 Harbor Bridge replacement highway project in Nueces County, Texas.
Agency Information Collection Activities: Proposed Collections; Comment Request
The Surface Transportation Board (Board), as part of its continuing effort to reduce paperwork burdens, and as required by the Paperwork Reduction Act of 1995, 44 U.S.C. 3501 et seq. (PRA), gives notice that the Board proposes to request approval of the seven existing information collections described below. Office of Management and Budget (OMB) control numbers were obtained in the past, but have expired, for six of the seven information collections that are the subject of this notice. For the most part, the collections listed below continue current Board reporting requirements without revision. As described below, a minor revision has been made to Collection No. 1, Class I Railroad Annual Report. Comments are requested regarding any of the collections of information described below concerning (1) whether the particular collection of information is necessary for the proper performance of the functions of the Board, including whether the collection has practical utility; (2) the accuracy of the Board's burden estimates; (3) ways to enhance the quality, utility, and clarity of the information collected; and (4) ways to minimize the burden of the collection of information on the respondents, including the use of automated collection techniques or other forms of information technology, when appropriate. Submitted comments will be summarized and included in the Board's request for OMB approval.
Federal Motor Vehicle Safety Standards
This document denies a petition from the Rubber Manufacturers Association (RMA) to conduct rulemaking to amend the Federal motor vehicle safety standard on tire selection and rims to require manufacturers of new motor vehicles to establish a recommended cold inflation pressure (placard pressure) for their vehicles using a tire pressure reserve. The tire pressure reserve would be based on the minimum pressure the RMA believes is necessary to support the vehicle's maximum load at the activation pressure of the installed tire pressure monitoring system (TPMS). The agency has decided to deny the petition because neither the RMA's nor the agency's data demonstrate a safety need for such a requirement.
Airworthiness Directives; The Cessna Aircraft Company Models 525, 525A, and 525B Airplanes
The FAA proposes to adopt a new airworthiness directive (AD) for certain The Cessna Aircraft Company (Cessna) Models 525, 525A, and 525B airplanes. This proposed AD would require you to install identification sleeves on the wiring for both engine fire extinguisher bottles. This proposed AD results from reports of incorrectly connecting the wires to the engine fire extinguisher bottles. We are issuing this proposed AD to prevent incorrect installation of the wires to the engine fire extinguisher bottles, which could result in failure of the engine fire extinguisher bottles to discharge when activated. This failure could lead to the inability to control an engine fire.
Airworthiness Directives; Turbomeca Arrius 2F Turboshaft Engines
This document publishes in the Federal Register an amendment adopting emergency airworthiness directive (AD) 2005-09-51 that we sent previously to all known U.S. owners and operators of certain Turbomeca Arrius 2F turboshaft engines. This AD requires before further flight, replacing the Module 2 on certain engines listed by serial number (SN) in this AD. This AD results from a report of the failure of a high pressure turbine (HPT) blade and damage to two other HPT blades in a Turbomeca Arrius 2F turboshaft engine. We are issuing this AD to prevent failure of the engine and subsequent loss of power.
Airworthiness Directives; Tiger Aircraft LLC Models AA-5, AA-5A, AA-5B, and AG-5B Airplanes
The FAA proposes to revise Airworthiness Directive (AD) 95-19- 15, which applies to all Tiger Aircraft LLC (Type Certificate A16EH formerly held by American General Aircraft Corporation and Grumman American Aviation Corporation) Models AA-5, AA-5A, AA-5B, and AG-5B airplanes. AD 95-19-15 currently requires you to inspect the wing attach shoulder bolts for fretting, scoring, wear, or enlarged or elongated mounting holes (known as damage from hereon); replace any damaged parts; repair any damaged areas; inspect the wing spar at the center spar clearance gap for excessive clearance; and shim the spar if excessive clearance is found. Since we issued AD 95-19-15, FAA has received and evaluated new service information that limits the serial numbers for the Model AG-5B airplanes of AD 95-19-15. Consequently, this proposed AD retains all the actions of AD 95-19-15 and includes the serial numbers for the Model AG-5B airplanes in the applicability section. We are issuing this proposed AD to prevent wing attach shoulder bolt failure, which, if not detected and corrected, could lead to structural damage of the wing/fuselage to the point of failure.
Federal Motor Vehicle Safety Standards; Occupant Crash Protection
This NPRM would amend Federal Motor Vehicle Safety Standard No. 208, Occupant crash protection, by proposing test procedures applicable to vehicles that have a child restraint anchorage system, commonly referred to as a ``LATCH'' system, in a front passenger seating position and that comply with advanced air bag requirements through the use of a suppression system. Beginning September 1, 2006, these vehicles must suppress the air bag in the presence of a child restraint system that is attached to the vehicle's LATCH system. The procedures proposed in this document specify a repeatable, reproducible, and realistic method of attaching child restraints to the LATCH system for the suppression test.
Airworthiness Directives; General Electric (GE) CF6-80E1 Series Turbofan Engines
The FAA is adopting a new airworthiness directive (AD) for General Electric (GE) CF6-80E1 series turbofan engines that have an electronic control unit (ECU) with software version E.1.M. or earlier installed. This AD requires installing improved software for the ECU. This AD results from an uncommanded engine acceleration event caused by a failure of the ECU digital interface unit (DIU). We are issuing this AD to prevent an undetected failure of the ECU DIU, which could result in uncommanded acceleration to the overspeed limit without response to throttle commands. The airplane could then experience asymmetric thrust.
Airworthiness Directives; Boeing Model 747 Airplanes
The FAA is superseding an existing airworthiness directive (AD), which applies to certain Boeing Model 747 airplanes. That AD currently requires inspections to detect cracks in the front spar pressure bulkhead chord, and repair if necessary. This new AD requires repetitive high frequency eddy current (HFEC) inspections of the body station (BS) 1000 bulkhead chord for cracks, repetitive detailed inspections of the bathtub fittings, if installed, for cracks, and corrective action if necessary. Initiation of the new inspections ends the inspections of the existing AD. This AD also revises the applicability of the existing AD to include additional airplanes. This AD is prompted by reports of cracks in the BS 1000 bulkhead chord. We are issuing this AD to detect and correct fatigue cracks in the BS 1000 bulkhead chord, which, if not repaired before they reach critical length, could result in the failure of the adjacent structure and skin and lead to in-flight depressurization of the airplane.
Airworthiness Directives; Boeing Model 747-100, -100B, -100B SUD, -200B, -200C, -300, -400, and -400D Series Airplanes; and Model 747SR Series Airplanes
The FAA is superseding an existing airworthiness directive (AD), which applies to certain Boeing Model 747 series airplanes. That AD currently requires a one-time inspection to determine the material type of the stop support fittings of the main entry doors (MEDs). That AD also currently requires repetitive detailed inspections to detect cracks of certain stop support fittings of the MEDs, and replacement of any cracked stop support fitting with a certain new stop support fitting. This new AD adds new inspections, and replacement if necessary, of the stop support fittings of MED 3, and adds airplanes to the applicability. This AD is prompted by reports of MED 3 having certain stop support fittings that are susceptible to stress corrosion cracking. We are issuing this AD to detect and correct stress corrosion cracking of the stop support fittings of the MEDs, which could result in damage to the adjacent forward edge frame of the door and consequent loss of a MED and rapid decompression of the airplane.
Airworthiness Directives; Boeing Model 777-200 and -300 Series Airplanes
This amendment adopts a new airworthiness directive (AD), applicable to certain Boeing Model 777-200 and -300 series airplanes, that requires modification of the bolt holes of the lower side of the body splice t-chord common to the paddle fittings of the lower wing panel. The modification includes performing a high frequency eddy current inspection of the fastener holes for cracks, repairing the hole if necessary, and replacing the fasteners with new inconel bolts. This action is necessary to prevent fatigue cracks in the lower t-chord at the bolt holes common to the paddle fittings that could result in fractures of one or more of the t-chord segments, which could lead to detachment of the lower wing panel and consequent loss of the wing. This action is intended to address the identified unsafe condition.
Airworthiness Directives; Boeing Model 747-100, 747-100B, 747-200B, 747-300, 747-400, 747-400D, 747SR, and 747SP Series Airplanes
The FAA is adopting a new airworthiness directive (AD) for certain Boeing Model 747-100, 747-100B, 747-200B, 747-300, 747-400, 747-400D, 747SR, and 747SP series airplanes. This AD requires replacing or modifying the control panels for the galley cart lift and modifying related electrical cable assemblies, as applicable. This AD is prompted by reports of injuries to catering personnel and flight attendants who were loading or unloading galley carts on one deck when, due to a disabled or malfunctioning safety interlock door switch, the galley cart lift unexpectedly moved when it was activated from the control panel on the other deck. We are issuing this AD to ensure that the galley cart lift can be sent only from the deck on which it is in use, which will prevent unexpected movement of the cart lift that could result in possible injury to catering personnel or flight attendants.
Airworthiness Directives; Boeing Model 777-200 Series Airplanes
The FAA is adopting a new airworthiness directive (AD) for certain Boeing Model 777-200 series airplanes. This AD requires replacing the pressure switches on the override/jettison fuel pumps with new pressure switches, and replacing the ship side electrical connectors for the pressure switches on override/jettison fuel pumps with new connectors. This AD is prompted by reports that the ``FUEL LOW CENTER'' message does not activate when the fuel level in the center tank is low. We are issuing this AD to prevent the fuel pumps in the center fuel tank from running dry and becoming a potential ignition source, which could result in a fuel tank explosion.
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