Enhancing Airline Passenger Protections: Full Fare Price Advertising Requirements
This document confirms the effective date of the direct final rule amending the time period for compliance with the full fare and other advertising requirements in 14 CFR 399.84 from January 24, 2012, to January 26, 2012.
Airworthiness Directives; The Boeing Company Airplanes
We propose to adopt a new airworthiness directive (AD) for certain Model 737 airplanes. This proposed AD would incorporate design changes to improve the reliability of the cabin altitude warning system by requiring installation of a redundant switch of the cabin altitude pressure, replacing the aural warning module (AWM) with a new or reworked AWM, changing certain wire bundles, and connecting certain previously capped and stowed wires, as necessary. This proposed AD, for certain airplanes, would also require modifying the instrument panels, installing light assemblies, modifying the wire bundles, and installing a new circuit breaker, as necessary. This proposed AD was prompted by a report of a lack of cabin pressurization event caused by the flightcrew not receiving an aural warning because of the failure of the cabin altitude pressure switch. We are proposing this AD to prevent failure of the flightcrew to recognize and react to a lack of cabin pressurization, which could result in incapacitation of the flightcrew due to hypoxia (lack of oxygen in the body), and consequent loss of control of the airplane.
Amendment of Class E Airspace; Show Low, AZ
This action modifies Class E airspace at Show Low Regional Airport, Show Low, AZ. Controlled airspace is necessary to accommodate aircraft using Area Navigation (RNAV) Global Positioning System (GPS) standard instrument approach procedures at Show Low Regional Airport. This improves the safety and management of Instrument Flight Rules (IFR) operations at the airport.
Airworthiness Directives; Cessna Aircraft Company Airplanes
We propose to adopt a new airworthiness directive (AD) for certain Cessna Aircraft Company Model 560XL airplanes. This proposed AD was prompted by reports of jammed or stiff rudder control due to water freezing on the rudder bias cables and pulleys of the stinger. This proposed AD would require modification of the drain installation of the tailcone stinger on the aft canted bulkhead, inspections for drain holes in the forward and aft frames, and modification of the drain holes. We are proposing this AD to prevent ice accumulation on the cables and pulleys of the stinger, which could result in jamming of the rudder and consequent reduced controllability of the airplane.
Public Notice for Release of Aeronautical Property at Erie International Airport (ERI), Erie, PA
The Federal Aviation Administration is requesting public comment on the Erie Regional Airport Authority's request to release airport property for use by the Pennsylvania Department of Transportation (PennDOT) to construct and maintain additional roadway and drainage facilities along the west side of Asbury Road. The request contains five (5) components consisting of a permanent release of land, release of land for drainage easement, release of land for temporary construction easement, release of land for substitute right-of-way, and release of land for permanent gas line easement.
Airworthiness Directives; The Boeing Company Airplanes
We propose to adopt a new airworthiness directive (AD) for certain The Boeing Company Model 777-200 and -300 series airplanes. This proposed AD was prompted by reports of cracked retract actuator fuse pins that can fail earlier than the previously determined safe life limit of the pins. A fractured retract actuator fuse pin can cause the main landing gear (MLG) to extend without restriction and attempt to lock into position under high dynamic loads. This proposed AD would require an inspection for the part number of the fuse pin, and replacement of the pin if necessary. We are proposing this AD to prevent structural damage to the side and drag brace lock assemblies, which could result in landing gear collapse during touchdown, rollout, or taxi.
Airworthiness Directives; International Aero Engines AG Turbofan Engines
We propose to supersede an existing airworthiness directive (AD), for all International Aero Engines AG (IAE) V2500-A1, V2525-D5 and V2528-D5 turbofan engines, and certain serial numbers (S/Ns) of IAE V2522-A5, V2524-A5, V2527-A5, V2527E-A5, V2527M-A5, V2530-A5, and V2533-A5 turbofan engines. The existing AD currently requires initial and repetitive on-wing ultrasonic inspections (USIs) of certain high- pressure compressor (HPC) stage 3 to 8 drums, and replacement of drum attachment nuts. This proposed AD would expand the affected population for initial and repetitive on-wing inspections of the HPC stage 3 to 8 drum, introduce an eddy current inspection (ECI) procedure, and require additional cleaning and repetitive on-wing USI or ECI of some HPC stage 3 to 8 drums. We are proposing this AD to prevent failure of the HPC stage 3 to 8 drum, uncontained engine failure, and damage to the airplane.
Notice and Request for Comments
As required by the Paperwork Reduction Act of 1995, 44 U.S.C. 3501-3519 (PRA), the Surface Transportation Board (STB or Board) gives notice that it has submitted a request to the Office of Management and Budget (OMB) for an extension of approval with revision of a currently approved collection: Application to Open a Billing Account. The revision consists of a reduction in burden hours due to the agency's revised estimate of the number of annual respondents. The Board previously published a notice about this collection in the Federal Register on September 30, 2011, at 76 FR 60,964. That notice allowed for a 60-day public review and comment period. No comments were received. The application to open a billing account is described in detail below. Comments may now be submitted to OMB concerning: (1) The accuracy of the Board's burden estimates; (2) ways to enhance the quality, utility, and clarity of the information collected; (3) 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; and (4) whether this collection of information is necessary for the proper performance of the functions of the Board, including whether the collection has practical utility.
Airworthiness Directives; Thielert Aircraft Engines GmbH Reciprocating Engines
We are revising an existing airworthiness directive (AD) for Thielert Aircraft Engines GmbH models TAE 125-02-99 and TAE 125-01 reciprocating engines. That AD currently requires replacing the existing rail pressure control valve with an improved rail pressure control valve. This new AD requires the same actions but relaxes the initial compliance time from within 100 flight hours to within 600 flight hours for TAE 125-01 reciprocating engines. This AD was prompted by the determination that our AD was inadvertently more restrictive than European Aviation Safety Agency AD 2008-0128. We are issuing this AD to prevent engine in-flight shutdown, possibly resulting in reduced control of the aircraft.
Amendment of VOR Federal Airways V-320 and V-440; Alaska
This action amends two VHF Omnidirectional Range (VOR) Federal airways in Alaska, V-320 and V-440, due to the relocation of the Anchorage VOR navigation aid. The FAA is taking this action to ensure the continued safe and efficient management of Instrument Flight Rules (IFR) operations within the National Airspace System.
Hazardous Materials: Harmonization With the United Nations Recommendations on the Transport of Dangerous Goods: Model Regulations, International Maritime Dangerous Goods Code, and the International Civil Aviation Organization Technical Instructions for the Safe Transport of Dangerous Goods by Air
This document responds to administrative appeals, provides clarifications, and corrects typographical and other minor errors adopted in an international harmonization final rule published January 19, 2011 (HM-215K; 76 FR 3308). The final rule amended the Hazardous Materials Regulations (HMR) by revising, removing or adding proper shipping names, the hazard class of a material, packing group assignments, special provisions, packaging authorizations, packaging sections, air transport quantity limitations, and vessel stowage requirements. The amendments were necessary to align the HMR with recent revisions to international standards for the transport of hazardous materials by all modes.
Airworthiness Directives; Lockheed Martin Corporation/Lockheed Martin Aeronautics Company Airplanes
We are adopting a new airworthiness directive (AD) for certain Lockheed Martin Corporation/Lockheed Martin Aeronautics Company Model L-1011-385-1, L-1011-385-1-14, L-1011-385-1-15, and L-1011-385-3 airplanes. This AD was prompted by results from a damage tolerance analysis conducted by the manufacturer indicating that fatigue cracking could occur in wing rear spar and upper surface zones. This AD requires repetitive inspections for cracking of the wing rear spar and upper surface zones, and repair if necessary. We are issuing this AD to detect and correct such fatigue cracking, which could result in cracking that grows large enough to reduce the wing strength below certificated requirements and possibly cause fracture of the rear spar, resulting in extensive damage to the wing and possible fuel leaks.
Drivers of CMVs: Restricting the Use of Cellular Phones
FMCSA is correcting a Final Rule that appeared in the Federal Register on December 2, 2011 (76 FR 75470), which restricted the use of hand-held mobile telephones by drivers of commercial motor vehicles. That rule was jointly issued by FMCSA and Pipeline and Hazardous Materials Safety Administration (PHMSA), but this correction only affects an FMCSA regulation.
Airworthiness Directives; General Electric Company (GE) GE90-110B1 and GE90-115B Turbofan Engines
We are adopting a new airworthiness directive (AD) for the products listed above, with certain part number (P/N) high-pressure compressor (HPC) stages 2-5 spools installed. This AD was prompted by an aborted takeoff caused by liberation of small pieces from the HPC stages 1-2 seal teeth and two shop findings of cracks in the seal teeth. This AD requires eddy current inspection (ECI) or spot fluorescent penetrant inspection (FPI) of the stages 1-2 seal teeth of the HPC stages 2-5 spool for cracks. This AD only allows installation of either HPC stator stage 1 interstage seals that are pregrooved or previously worn seals with acceptable wear marks to prevent heavy rubs. We are issuing this AD to detect cracks in the HPC stages 1-2 seal teeth due to heavy rubs that could result in failure of the seal of the HPC stages 2-5 spool, uncontained engine failure, and damage to the airplane.
Airworthiness Directives; The Boeing Company Airplanes
We are adopting a new airworthiness directive (AD) for all The Boeing Company Model 737-600, -700, -700C, -800, -900, and -900ER series airplanes. This AD was prompted by reports of excessive in- service wear damage of the thumbnail fairing edge seal, and of the panel rub strip and skin assembly of the fan cowl. This AD requires replacement of the thumbnail fairing edge seals on both sides of the engines with Nitronic 60 stainless steel alloy seals. We are issuing this AD to prevent failure of the fire seal, which could allow a fire in the fan compartment to spread beyond the firewall and reach the flammable fluid leakage zones, resulting in an uncontrolled fire.
Information Collection Activities: Submission for the Office of Management and Budget (OMB) Review; Request for Comment
In compliance with the Paperwork Reduction Act of 1995 (44 U.S.C. chapter 35), this notice announces that the Information Collection Request (ICR) abstracted below will be submitted to the Office of Management and Budget (OMB) for review. The ICR describes the nature of the information collection and its expected burden. A Federal Register Notice with a 60-day comment period soliciting public comments on the following information collection was published on June 13, 2011 (Federal Register/Vol. 76, No. 113/pp. 34290-34291).
Public Notice for Waiver of Aeronautical Land-Use Assurance; Ohio State University Airport, Columbus, OH
The Federal Aviation Administration (FAA) is considering a proposal to change a portion of the Ohio State University Airport from aeronautical use to non-aeronautical use and to authorize the swap of the airport property. The proposal consists of the swap of vacant, unimproved land owned by the State of Ohio (State) for land owned by the Board of Trustees of the Ohio State University (University). The State has requested from FAA a ``Release from Federal agreement obligated land covenants'' to swap one (1) parcel of property acquired by the State without Federal funding for three (3) parcels owned by the University. The above mentioned land is not needed for aeronautical use, as shown on the Airport Layout Plan. There are no impacts to the airport by allowing the State to dispose of the vacant property. Approval does not constitute a commitment by the FAA to financially assist in the disposal of the airport property nor a determination of eligibility for grant-in-aid funding from the FAA. The disposition of proceeds from the disposal of the 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. 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 the property to be used for an aeronautical purpose.
Public Notice for Waiver of Aeronautical Land-use Assurance; DuPage Airport, West Chicago, IL
The Federal Aviation Administration (FAA) is considering a proposal to change a portion of airport land from aeronautical use to non-aeronautical use and to authorize the sale of the airport property. The proposal consists of all or portions of Parcels 209A, 213, 217, 218, 219, 220, 221, 314, 315, 401, 402, 404, 406, 407, 408, 409, 410, 411, 412, 413, 414, and 416, totaling 605.3 acres. Presently the land is vacant and used as open land for control of FAR Part 77 surfaces and compatible land use and is not needed for aeronautical use, as shown on the Airport Layout Plan. The Parcels were acquired without Federal participation. It is the intent of the DuPage Airport Authority, as owner and operator of the DuPage Airport (DPA) to sell the aforementioned Parcels (605.3 Acres) in fee to the DuPage County (22.7 acres for Kress Creek floodplain control), the City of West Chicago (37.7 acres for the ownership and maintenance of existing roadways), the Illinois Department of Transportation (11.3 acres for the improvement of State Route 38), and to private entities (533.6 acres for corporate/industrial development). This notice announces that the FAA is considering the proposal to authorize the disposal of the subject airport property at the DuPage Airport, West Chicago, IL. Approval does not constitute a commitment by the FAA to financially assist in disposal of the subject airport property nor a determination that all measures covered by the program are eligible for grant-in-aid funding from the FAA. The disposition of proceeds from the disposal of the 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. 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 the property to be used for an aeronautical purpose.
Receipt of Petition for Decision That Nonconforming 2000-2003 Kawasaki ZR750 Motorcycles Are Eligible for Importation
This document announces receipt by the National Highway Traffic Safety Administration (NHTSA) of a petition for a decision that nonconforming 2000-2003 Kawasaki ZR750 motorcycles that were not originally manufactured to comply with all applicable Federal Motor Vehicle Safety Standards (FMVSS) are eligible for importation into the United States because (1) they are substantially similar to vehicles that were originally manufactured for 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.
Airworthiness Directives; The Boeing Company Airplanes
We are revising an earlier proposed airworthiness directive (AD) for all The Boeing Company Model 747-100, 747-100B, 747-100B SUD, 747-200B, 747-200C, 747-200F, 747-300, 747-400, 747-400D, 747-400F, 747SR, and 747SP series airplanes. The original NPRM proposed a general visual inspection to identify any existing structural repair manual repairs of the upper main sill outer chord of the left and right side main entry door number 1, as applicable; repetitive detailed inspections for cracks in the upper main sill of the door(s); and related investigative and corrective actions, if necessary. The original NPRM also proposed repetitive inspections for airplanes on which a certain repair is done, and corrective actions if necessary. The original NPRM was prompted by reports of cracks in the main entry door number 1 upper main sill outer chord, along the bend radius of the chord on several airplanes. This action revises the original NPRM by reducing certain compliance times. We are proposing this supplemental NPRM to detect and correct cracks in the main entry door number 1 upper main sill outer chord, along the bend radius of the chord, which could result in loss of structural integrity of the airplane. Since these actions impose an additional burden over that proposed in the original NPRM, we are reopening the comment period to allow the public the chance to comment on these proposed changes.
Airworthiness Directives; Goodrich Evacuation Systems Approved Under Technical Standard Order (TSO) TSO-C69b and Installed on Airbus Airplanes
We are revising an earlier proposed airworthiness directive (AD) for Goodrich Evacuation Systems approved under Technical Standard Order (TSO) TSO-C69b and installed on Airbus Model A330-200 and -300 series airplanes, Model A340-200 and -300 series airplanes, and Model A340-500 and -600 series airplanes. That NPRM proposed to supersede an existing AD. That NPRM proposed inspecting to determine the part number of the pressure relief valves on the affected Goodrich evacuation systems, replacing certain pressure relief valves, and adding airplanes to the applicability. That NPRM was prompted by reports that during workshop testing, certain pressure relief valves, which were required by the existing AD, did not seal and allowed the pressure in certain slides/rafts to fall below the minimum raft mode pressure for the unit. This action revises that NPRM by adding certain airplanes to the applicability. We are proposing this supplemental NPRM to correct the unsafe condition on these products. Since these actions impose an additional burden over that proposed in the NPRM, we are reopening the comment period to allow the public the chance to comment on these proposed changes.
Airworthiness Directives; The Boeing Company Airplanes
We propose to supersede an existing airworthiness directive (AD) that applies to The Boeing Company Model 757-200, -200CB, and -300 series airplanes. The existing AD currently requires initial and repetitive inspections of the fuselage skin and bear strap at the forward, upper corner of the L1 entry door cutout for cracking, and repair if necessary. That action also provides an optional terminating action for the repetitive inspections. Since we issued that AD, we have received reports of additional cracking in the fuselage skin. This proposed AD would add inspections for airplanes having repairs or preventative modifications installed and supplemental inspections for certain airplanes. This proposed AD also would add airplanes to the applicability. We are proposing this AD to detect and correct cracking of the fuselage skin and bear strap at the forward, upper corner of the L1 entry door cutout, which could result in reduced structural integrity of the L1 entry door and consequent rapid decompression of the airplane.
Commercial Space Transportation Advisory Committee; Public Teleconference
Pursuant to Section 10(a)(2) of the Federal Advisory Committee Act (Pub. L. 92-463, 5 U.S.C. App. 2), notice is hereby given of a teleconference of the Commercial Space Transportation Advisory Committee (COMSTAC) Risk Management Working Group. The teleconference will take place on Tuesday, January 24, 2012, starting at 1:30 p.m. Eastern Standard Time. Individuals who plan to participate should contact Susan Lender, Designated Federal Officer (DFO), (the Contact Person listed below) by phone or email for the teleconference call in number. The National Aeronautics and Space Administration (NASA) and the FAA Office of Commercial Space Transportation (AST) have agreed to prepare a study on the availability of commercial insurance sufficient to meet the needs of NASA's Commercial Crew Program commercial providers for missions transporting NASA astronauts to and from the International Space Station. NASA's Commercial Crew Program requested this study (via a signed memorandum of understanding with the FAA AST) be conducted by AST because of its knowledge and resources in the commercial space industry. The purpose of the teleconference is to: 1. Brief the COMSTAC Risk Management Working Group on the study, 2. Request assistance from the working group in preparing a response to NASA, and 3. Respond to any questions from the working group on the nature of this task. Interested members of the public may submit relevant written statements for the COMSTAC members to consider under the advisory process. Statements may concern the issues mentioned above or additional issues that may be relevant for the U.S. commercial space transportation industry. Interested parties wishing to submit written statements should contact Susan Lender, DFO, (the Contact Person listed below) in writing (mail or email) by January 17, 2012, so that the information can be made available to COMSTAC members for their review and consideration before the January 24, 2012, teleconference. Written statements should be supplied in the following formats: one hard copy with original signature or one electronic copy via email. This notice will be posted on the FAA Web site at http:// www.faa.gov/go/ast. Individuals who plan to participate and need special assistance should inform the Contact Person listed below in advance of the meeting.
Proposed Agency Information Collection Activities; Comment Request
In compliance with the Paperwork Reduction Act of 1995 (44 U.S.C. 3501 et seq.), this notice announces that the Information Collection Requirements (ICRs) abstracted below are being forwarded to the Office of Management and Budget (OMB) for review and comment. The ICRs describe the nature of the information collections and their expected burden. The Federal Register notice with a 60-day comment period soliciting comments on the following collections of information was published on October 17, 2011 (76 FR 64172).
Proposed Agency Information Collection Activities; Comment Request
In compliance with the Paperwork Reduction Act of 1995 (44 U.S.C. 3501 et seq.), this notice announces that the Information Collection Requirements (ICRs) abstracted below are being forwarded to the Office of Management and Budget (OMB) for review and comment. The ICRs describe the nature of the information collections and their expected burden. The Federal Register notice with a 60-day comment period soliciting comments on the following collections of information was published on October 14, 2011 (76 FR 63990).
Airworthiness Directives; Hawker Beechcraft Corporation Airplanes Equipped With a Certain Supplemental Type Certificate (STC)
We are adopting a new airworthiness directive (AD) for all Hawker Beechcraft Corporation Models 95-C55, D55, E55, 58, and 58A airplanes equipped with a certain STC. This AD requires assuring the airspeed indicator(s) and/or airspeed limitations placard(s) have the correct minimum control speed (VMC) markings for the STCs installed. This AD was prompted by information that suggests the affected airplane models with a certain STC installed may not have the appropriate VMC markings on the airspeed indicator(s). We are issuing this AD to correct the unsafe condition on these products.
Airworthiness Directives; Airbus Airplanes
We propose to adopt a new airworthiness directive (AD) for certain Airbus Model A330-200 freighter series airplanes; Model A330- 200 and -300 series airplanes; and Model A340-200 and -300 series airplanes. This proposed AD was prompted by a report of corrosion found on the main fitting of the nose landing gear (NLG) leg in the vicinity of the dowel pin bushes retaining the lower steering flange. This proposed AD would require modifying the NLG main fitting by adding primer paint to the cadmium around the dowel bush holes. We are proposing this AD to prevent NLG main fitting rupture, which could result in an NLG collapse.
Airworthiness Directives; Empresa Brasileira de Aeronautica S.A. (EMBRAER) Airplanes
We propose to supersede an existing airworthiness directive (AD) that applies to all EMBRAER Model ERJ 170 airplanes. The existing AD currently requires revising the Airworthiness Limitations Section (ALS) of the Instructions for Continued Airworthiness (ICA) to incorporate new structural inspection requirements. Since we issued that AD, during full scale fatigue testing, cracks were found in certain structural components of the airplane. Analysis of these cracks resulted in manufacturer modifications of the ALS of Embraer ERJ 170 Maintenance Review Board Report (MRBR), which include new inspections tasks, or modification of the current tasks and their respective thresholds and intervals. This proposed AD would revise the maintenance program to incorporate new or revised structural inspection requirements. We are proposing this AD to detect and correct fatigue cracking which could result in the loss of structural integrity of the airplane.
Airworthiness Directives; Saab AB, Saab Aerosystems Airplanes
We propose to adopt a new airworthiness directive (AD) for all Saab AB, Saab Aerosystems Model SAAB 2000 airplanes. This proposed AD was prompted by reports of hydraulic accumulator failure. This proposed AD would require replacing certain hydraulic accumulators with stainless steel hydraulic accumulators, and structural modifications in the nose landing gear bay. We are proposing this AD to prevent failure of hydraulic accumulators, which may result in damage to the airplane and injury to occupants.
Special Conditions: Gulfstream Aerospace LP (GALP) Model G280 Airplane, Operation Without Normal Electrical Power
These special conditions are issued for the Gulfstream Aerospace LP (GALP) Model G280 airplane. This airplane will have a novel or unusual design feature associated with operation without normal electrical power. The applicable airworthiness regulations do not contain adequate or appropriate safety standards for this design feature. 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.
Airworthiness Directives; Eurocopter France (Eurocopter) Helicopters
We propose to adopt a new airworthiness directive (AD) for the Eurocopter Model SA330F, G, J and AS332C, L, L1, and L2 helicopters. This proposed AD is prompted by two reports of jamming of one of the fuel shut-off control levers, which originated from solidified grease in the tangential gearbox (gearbox). Corrosion was also found in a gearbox. The proposed actions are intended to prevent jamming of a fuel shut-off control lever preventing the shut off of engine fuel and preventing the parallel-mounted electrical micro switches, normally activated by shutting off both of the fuel shut-off control levers, from switching off the electrical power system during an emergency shut down.
Hours of Service of Motorcoach Drivers
FMCSA announces that it will hold a public listening session to solicit information, concepts, ideas, and information on hours-of- service (HOS) requirements for motorcoach drivers. Specifically, the Agency would like to know what factors, issues, and data may be pertinent as it considers development of a rulemaking on these requirements. The session, which will be held in Grapevine, Texas, will allow interested persons to present comments, views, and relevant new research. This listening session will be recorded and a transcript of the public meeting will be placed in the docket for FMCSA's consideration, as well as all comments submitted during the session. The listening session will also be webcast via the Internet.
Hazardous Materials: Miscellaneous Amendments; Response to Appeals; Corrections
On July 20, 2011, PHMSA published a final rule under Docket Number PHMSA-2009-0151 (HM-218F) making miscellaneous amendments to the Hazardous Materials Regulations (HMR; 49 CFR parts 171-180). The amendments made by PHMSA in the July 20, 2011 final rule promote safer transportation practices; eliminate unnecessary regulatory requirements; finalize outstanding petitions for rulemaking; facilitate international commerce; and simplify the regulations. This final rule corrects errors in the pictorial display of labels, eliminates references to transitional provisions that were previously removed from the HMR, clarifies shipping paper amendments, corrects an editorial error, and extends the effective date of certain shipping paper amendments adopted in the July 20, 2011 final rule.
Notice of Public Webinar on Implementation of Distribution Integrity Management Programs
Distribution pipeline operators were required to have prepared and implemented distribution integrity management plans (DIMP) by August 2, 2011. Federal and state regulators have begun inspecting those plans and their implementation. This webinar will be the first opportunity for the regulators to share their findings broadly with the regulated community. The webinar will also include discussion of analyses of the initial submissions of data concerning mechanical fitting failures in distribution pipelines.
Pipeline Safety: Information Collection Activities
In accordance with the Paperwork Reduction Act of 1995, PHMSA invites comments on an information collection under Office of Management and Budget (OMB) Control No. 2137-0584, ``Gas Pipeline Safety Program Certification and Hazardous Liquid Pipeline Safety Program Certification.'' PHMSA will request approval from OMB for a renewal of the current information collection with no revisions.
Agency Information Collection Activities: Proposed Collection; Comment Request; Generic Clearance for the Collection of Qualitative Feedback on Agency Service Delivery
As part of a Federal Government-wide effort to streamline the process to seek feedback from the public on service delivery, the Pipeline Hazardous Materials Safety Administration will submit a Generic Information Collection Request (Generic ICR): ``Generic Clearance for the Collection of Qualitative Feedback on Agency Service Delivery'' to the Office of Management and Budget (OMB) for approval under the Paperwork Reduction Act (PRA) (44 U.S.C. 3501 et seq.).
Petition for Exemption; Summary of Petition Received
This notice contains a summary of a petition seeking relief from specified requirements of title 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 the petition or its final disposition.
Aviation Rulemaking Advisory Committee-New Task
The FAA assigned the Aviation Rulemaking Advisory Committee (ARAC) a new task to develop a comprehensive program of voluntary accreditation for commercial air tour operators that are not required under parts 91 and 135 of Title 14 of the Code of Federal Regulations (14 CFR) to maintain their aircraft under a continuous airworthiness maintenance program (CAMP). This task addresses, in part, the ARAC recommendation developed by the Commercial Air Tours Maintenance (CATM) Working Group, which the FAA accepted on February 1, 2011. This notice informs the public of a new ARAC activity and solicits membership for the new Commercial Air Tour Voluntary Accreditation Program Working Group.
Clarification of Policy Regarding Approved Training Programs
This document announces the availability of an FAA Notice that would require FAA inspectors to review 14 CFR part 135 approved training programs to identify and correct those programs which erroneously issued credit for previous training or checking. The document also provides guidance on constructing reduced hour training programs based on previous experience. Upon review of the comments and any necessary revision, this document would cancel and replace FAA Order 8900.1, Volume 3, Chapter 19, Paragraph 3-1111.
Notice of Final Federal Agency Actions on Proposed Light Rail Project in Washington
This notice announces actions taken by FHWA and other Federal agencies that are final within the meaning of 23 U.S.C. 139(l)(1). The actions relate to the East Link Light Rail Transit Project in King County Washington. These actions grant licenses, permits, and approvals for the project.
Agency Information Collection Activities: Requests for Comments; Clearance of Renewed Approval of Information Collection: Training and Qualification Requirements for Check Airmen and Flight Instructors
In accordance with the Paperwork Reduction Act of 1995, FAA invites public comments about our intention to request the Office of Management and Budget (OMB) approval to renew an information collection. The Federal Register Notice with a 60-day comment period soliciting comments on the following collection of information was published on October 26, 2011, vol. 76, no. 207, page 66349. The rule allows some experienced pilots who would otherwise qualify as flight instructors or check airmen, but who are not medically eligible to hold the requisite medical certificate, to perform flight instructor or check airmen functions in a simulator.
Special Conditions: XtremeAir GmbH, XA42; Acrobatic Category Aerodynamic Stability
This action proposes special conditions for the XtremeAir GmbH XA42 airplane. The XA42 airplane has a novel or unusual design feature associated with its static stability. This airplane can perform at the highest level of aerobatic competition. To be competitive, the aircraft was designed with positive and, at some points, neutral stability within its flight envelope. Its lateral and directional axes are also decoupled from each other providing more precise maneuvering. 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. These special conditions are only applicable to aircraft certified solely in the acrobatic category.