Federal Aviation Administration 2015 – Federal Register Recent Federal Regulation Documents
Results 351 - 400 of 1,097
Airworthiness Directives; Airbus Airplanes
We propose to adopt a new airworthiness directive (AD) for all Airbus Model A318, A319, A320, and A321 series airplanes. This proposed AD was prompted by an evaluation by the design approval holder (DAH) indicating that the fuselage skin repairs are subject to widespread fatigue damage (WFD). This proposed AD would require an inspection to determine whether any fuselage external skin (doubler) repairs have been accomplished, an inspection for cracking of certain repaired external fuselage skin areas in the fuselage, and repair if necessary. We are proposing this AD to detect and correct fatigue cracking of the fuselage skin, which could result in reduced structural integrity of the airplane.
Federal Contract Tower Safety Action Program (SAFER-FCT) and Air Traffic Safety Action Program for Engineers & Architects, Staff Support Specialists, Aviation Technical System Specialists (Series 2186) and Flight Procedures Team (ATSAP-X)
This action affirms the order published in the Federal Register on April 3, 2015, regarding the application of Title 14, Code of Federal Regulations (14 CFR) Part 193, Federal Contract Tower SAFER- FCT Program and the Air Traffic Organization Engineers and Architects, Staff Support Specialist (Series 2186) and Flight Procedures Team (hereinafter ``Region X'') ATSAP-X Program. The Notice proposed that safety information provided to the FAA under the SAFER-FCT and ATSAP-X programs be designated by an FAA Order as protected from public disclosure in accordance with the provisions of 14 CFR part 193, Protection of Voluntarily Submitted Information. The designation is intended to encourage persons to voluntarily provide information to the FAA under the SAFER-FCT and ATSAP-X, so the FAA can learn about and address aviation safety hazards and implement, as appropriate corrective measures for events or safety issues.
Airworthiness Directives; The Boeing Company Airplanes
We are revising an earlier proposed airworthiness directive (AD) for The Boeing Company Model 777-200 and -300 series airplanes, equipped with Rolls-Royce Model RB211-Trent 800 engines. The notice of proposed rulemaking (NPRM) proposed to require repetitive inspections of the thrust reverser (T/R) structure and sealant, and related investigative and corrective actions if necessary. The NPRM was prompted by reports of T/R events related to thermal damage of the T/R inner wall. This action revises the NPRM by proposing to add different repetitive inspections requirements for T/R halves with a thermal protective system installed. This action also revises the NPRM by proposing to require installation of serviceable T/R halves, which would terminate the repetitive inspections in this SNPRM. This SNPRM also proposes to revise the inspection or maintenance program by incorporating new airworthiness limitations. We are proposing this SNPRM to detect and correct a degraded T/R inner wall panel, which could lead to failure of the T/R and adjacent components and their consequent separation from the airplane, and which could result in a rejected takeoff (RTO) and cause asymmetric thrust and consequent loss of control of the airplane during reverse thrust operation. If a T/R inner wall overheats, separated components could cause structural damage to the airplane, damage to other airplanes, or possible injury to people on the ground. 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 Airbus Helicopters (Previously Eurocopter France)
We propose to supersede airworthiness directive (AD) 2014-12- 51 for Airbus Helicopters (previously Eurocopter France) Model EC130B4 and EC130T2 helicopters. AD 2014-12-51 currently requires repetitively inspecting the tailboom to Fenestron junction frame (junction frame) for a crack. This proposed AD would retain the requirements of AD 2014- 12-51, change the applicability from helicopters with certain hours time-in-service (TIS) to junction frames with certain hours TIS, and add a compliance time for sling cycles to the junction frame inspection interval. These proposed actions are intended to detect a crack and to prevent failure of the junction frame, which could result in loss of the Fenestron and subsequent loss of control of the helicopter.
Proposed Establishment of Class E Airspace; International Falls, MN
This action makes a correction to the NPRM published in the Federal Register of August 27, 2015, proposing to establish Class E en route domestic airspace in the International Falls, MN area. Exclusionary reference to Canadian airspace was omitted from the regulatory text.
Establishment of Class E Airspace; Poplarville-Pearl River County Airport, MS
This action establishes Class E Airspace at Poplarville, MS. to accommodate new Area Navigation (RNAV) Global Positioning System (GPS) Standard Instrument Approach Procedures (SIAPs) serving Poplarville-Pearl River County Airport. Controlled airspace is necessary for the safety and management of instrument flight rules (IFR) operations at the airport. The FAA found that Class E airspace already exists for another airport in Poplarville, MS, and, therefore, is changing the title and airspace designation in this final rule to include the airport name. Also, a minor adjustment is made to the geographic coordinates of the airport.
Amendment of Class E Airspace; Mackall AAF, NC
This action amends Class E Airspace at Mackall Army Airfield (AAF), NC, bringing current the regulatory text under the airspace designation for Mackall AAF, NC, by replacing the acronym ``NCB'' with ``NDB''. This is an administrative change to coincide with the FAA's aeronautical database.
Airworthiness Directives; Alpha Aviation Concept Limited Airplanes
We propose to adopt a new airworthiness directive (AD) for certain Alpha Aviation Concept Limited Model R2160 airplanes that would supersede AD 2008-09-01. This proposed AD results from mandatory continuing airworthiness information (MCAI) originated by an aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as a need to revise the maintenance program to include the revised airworthiness limitations for the internal wing structure and wing attachment inspections. We are issuing this proposed AD to require actions to address the unsafe condition on these products.
Airworthiness Directives; Sikorsky Aircraft Corporation (Sikorsky) Helicopters
We propose to supersede airworthiness directive (AD) 2014-07- 04R1 for certain Sikorsky Model S-92A helicopters. AD 2014-07-04R1 currently requires repetitive inspections in the upper deck area for incorrectly installed clamps and chafing between the electrical wires and the hydraulic lines and replacing any unairworthy wires or hydraulic lines. Since we issued AD 2014-07-04R1, the manufacturer has developed an alteration that corrects the unsafe condition described in AD 2014-07-04R1. This proposed AD would require altering the wiring system in the upper deck area. These proposed actions are intended to prevent a fire in an area of the helicopter without extinguishing capability and subsequent loss of control of the helicopter.
Revocation of Jet Route J-513; North Central United States
This action removes jet route J-513 in the north central United States. The FAA is taking this action to reflect and accommodate route changes made in Canadian airspace as part of Canada's Windsor- Toronto-Montreal (WTM) airspace redesign project.
Airworthiness Directives; Bombardier, Inc. Airplanes
We propose to supersede Airworthiness Directive (AD) 2014-20- 01, for certain Bombardier, Inc. Model CL-600-2B16 (CL-601-3A, CL-601- 3R, and CL-604 Variants) airplanes. AD 2014-20-01 currently requires repetitive inspections for any fuel leak in the right-hand landing lights compartment, and related investigative and corrective actions if necessary. AD 2014-20-01 also provides for an optional replacement of the connector of the fuel boost pump canister of the auxiliary power unit (APU), which terminates the repetitive inspections. Since we issued AD 2014-20-01, we have determined that a terminating action for the repetitive inspections is necessary. This proposed AD would retain the repetitive inspections for any fuel leak in the right-hand landing lights compartment and the related investigative and corrective actions, and would require replacing the connector of the fuel boost pump canister of the APU. We are proposing this AD to detect and correct fuel leaks in the right-hand landing lights compartment, which, in combination with the heat generated by the taxi lights and landing lights on the ground reaching the auto-ignition temperature of the fuel, could result in ignition of any fuel or fumes present in the right-hand landing lights compartment.
Amendment of Class C Airspace; Portland International Airport, OR
This action amends geographic coordinates of Portland International Airport, Portland, OR, under Class C airspace, due to recent surveys of the airport. This action also updates the name and geographic coordinates of satellite airports referenced in the Portland description. This action does not change the boundaries or operating requirements of the airspace.
Amendment of Class C Airspace; Burbank, CA
This action amends the name and geographic coordinates of the Burbank-Glendale-Pasadena Airport at Burbank, CA. The Burbank-Glendale- Pasadena Airport has been renamed Bob Hope Airport and geographic coordinates are updated to reflect recent surveys of the airport.
Amendment of Class E Airspace; Douglas, WY
This action modifies Class E airspace at Converse County Airport, Douglas, WY, to accommodate new Standard Instrument Approach Procedures (SIAPs) at Converse County Airport, and addresses an inaccuracy identified by FAA Airspace Policy and Support that V-19, which is no longer located in the area, is used in the legal description of the airspace. The geographic coordinates of the airport also are adjusted. The FAA is taking this action to enhance the safety and management of Instrument Flight Rules (IFR) operations at the airport.
Establishment of Class E Airspace, Delta, CO
This action establishes Class E airspace extending upward from 700 feet above the surface at Blake Field Airport, Delta CO, to accommodate new Area Navigation (RNAV) Global Positioning System (GPS) standard instrument approach procedures developed for the airport. This action enhances the safety and management of Instrument Flight Rules (IFR) operations at the airport.
Establishment of Class E Airspace; Iron Mountain, MI
This action establishes Class E airspace at the Iron Mountain VHF Omni-Directional Radio Range/Distance Measuring Equipment (VOR/ DME), Iron Mountain, MI, to facilitate vectoring of Instrument Flight Rules (IFR) aircraft under control of Minneapolis Air Route Traffic Control Center (ARTCC). This action enhances the safety and efficiency of aircraft operations within the National Airspace System (NAS). A minor change in the regulatory text is made to align the new Class E airspace with Minneapolis ARTCC's airspace.
Establishment of Class E Airspace; Newberry, MI
This action establishes Class E airspace at the Newberry VHF Omni-Directional Radio Range/Distance Measuring Equipment (VOR/DME), Newberry, MI, to facilitate vectoring of Instrument Flight Rules (IFR) aircraft under control of Minneapolis Air Route Traffic Control Center (ARTCC). This action enhances the safety and efficiency of aircraft operations within the National Airspace System (NAS). A minor change in the regulatory text is made to align the new Class E airspace with Minneapolis ARTCC's airspace.
Airworthiness Directives; Dassault Aviation Airplanes
We propose to adopt a new airworthiness directive (AD) for certain Dassault Aviation Model MYSTERE-FALCON 50, MYSTERE-FALCON 900, FALCON 900EX, FALCON 2000, and FALCON 2000EX airplanes. This proposed AD was prompted by a report of an in-flight lightning strike to the WHELEN anti-collision light located on the top of the vertical fin tip that caused severe damage and induced the loss of some airplane functions. This proposed AD would require modification of the anti- collision light bonding. We are proposing this AD to prevent loss of electrical power and essential functions, and possible reduced control of the airplane.
Research, Engineering and Development Advisory Committee Meeting
The FAA is issuing this notice to advise the public of the Research, Engineering and Development Advisory Committee meeting.
Notice of Submission Deadline for Schedule Information for Los Angeles International Airport, Chicago O'Hare International Airport, San Francisco International Airport, John F. Kennedy International Airport, and Newark Liberty International Airport for the Summer 2016 Scheduling Season
Under this notice, the FAA announces the submission deadline of October 8, 2015, for summer 2016 flight schedules at Los Angeles International Airport (LAX), Chicago O'Hare International Airport (ORD), San Francisco International Airport (SFO), John F. Kennedy International Airport (JFK), and Newark Liberty International Airport (EWR) in accordance with the International Air Transport Association (IATA) Worldwide Slot Guidelines. The deadline coincides with the schedule submission deadline for the IATA Slot Conference for the summer 2016 scheduling season.
Special Conditions: Honda Aircraft Company, Model HA-420 HondaJet, Lithium-ion Batteries
These special conditions are issued for the Honda Aircraft Company, Model HA-420 airplane. This airplane will have a novel or unusual design feature associated with the installation of lithium-ion (Li-ion) batteries. 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.
Special Conditions: Honda Aircraft Company (Honda) Model HA-420, HondaJet; Cruise Speed Control System
This action proposes special conditions for the Honda Aircraft Company HA-420 airplane. This airplane will have a novel or unusual design feature(s) associated with the use of a cruise speed control system. The applicable airworthiness regulations 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 established by the existing airworthiness standards.
Notice of Intent To Release Certain Properties From All Terms, Conditions, Reservations and Restrictions of a Quitclaim Deed Agreement Between the County of Palm Beach and the Federal Aviation Administration for the Palm Beach International Airport, West Palm Beach, FL
The FAA hereby provides notice of intent to release approximately 0.21 acres at the Palm Beach International Airport, West Palm Beach, FL from the conditions, reservations, and restrictions as contained in a Quitclaim Deed agreement between the FAA and the County of Palm Beach, dated March 22, 1961. The release of property will allow the County of Palm Beach to dispose of the property for other than aeronautical purposes. The property is located along Florida Mango and Belvedere Road. The parcels are currently designated as non- aeronautical use. The property will be released of its federal obligations to grant an easement for right-of-way and stormwater retention. The fair market value of the right-of-way parcel and stormwater retention parcel has been determined to be $83,860 and $74,320, respectively. Documents reflecting the Sponsor's request are available, by appointment only, for inspection at the Palm Beach County Department of Airports at Palm Beach International Airport and the FAA Airports District Office.
Special Conditions: Cirrus Design Corporation, SF50; Full Authority Digital Engine Control (FADEC) System
These special conditions are issued for the Cirrus Design Corporation SF50 airplane. This airplane will have a novel or unusual design feature(s) associated with the use of an electronic engine control system instead of a traditional mechanical control system. 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.
Notice of Intent To Designate as Abandoned Normal Category Type Certificate: Silvercraft S.co.p.a., Type Certificate No. H2EU
This notice announces the FAA's intent to designate Silvercraft S.co.p.a. (Silvercraft) Type Certificate (TC) H2EU, issued in the normal category, as abandoned. The FAA has been unable to locate Silvercraft, the TC holder, concerning the continued airworthiness of the aircraft certificated under its TC. The Federal Aviation Regulations (regulations) require that TC holders report certain failures, malfunctions, and defects to the FAA. The regulations also require, upon request, that TC holders submit design changes to the FAA that are necessary to correct any unsafe condition in their products. The FAA is responsible for surveillance of Silvercraft's ability to perform continued operational safety management and oversight of the helicopter on its TC. This action is intended to ensure that Silvercraft Model SH-4 helicopters are under a TC that has active continued operational safety management and oversight by a TC holder that can be subject to periodic safety audits by the FAA.
Sixteenth Meeting: Special Committee (227) Standards of Navigation Performance (Navigation Information on Electronic Maps)
The FAA is issuing this notice to advise the public of the Sixteenth Special Committee 227 meeting.
Sixth Meeting: Special Committee (229) 406 MHz Emergency Locator Transmitters (ELTs)
The FAA is issuing this notice to advise the public of the sixth Special Committee 229 meeting.
Twenty-Fourth Meeting: Special Committee (214) Standards for Air Traffic Data Communication Services (Joint With EUROCAE WG-78)
The FAA is issuing this notice to advise the public of the twenty-fourth Special Committee 214 meeting.
Airworthiness Directives; Airbus Airplanes
We are superseding Airworthiness Directive (AD) 2011-19-04, for all Airbus Model A318, A319, A320, and A321 series airplanes. AD 2011-19-04 required repetitive inspections for cracking of the left- hand and right-hand inboard and outboard elevator servo-control rod eye-ends, and corrective actions if necessary. This new AD requires an inspection to determine if certain elevator servo-control parts are installed, and replacement if necessary. This AD was prompted by a determination that certain elevator servo-control parts that do not conform to the approved type design have been installed and may have the potential of cracks in the rod eye-end. We are issuing this AD to detect and correct rod eye-end cracking, which could result in uncontrolled elevator surface and consequent reduced control of the airplane.
Airworthiness Directives; The Boeing Company Airplanes
We are superseding Airworthiness Directive (AD) 2012-24-10 for certain The Boeing Company Model 747-400 and -400F series airplanes. AD 2012-24-10 required installing new software, replacing the duct assembly with a new duct assembly, making wiring changes, and routing certain wire bundles. This new AD retains the requirements of AD 2012- 24-10 and requires installing a new or serviceable pressure switch bracket and altitude pressure switch. This new AD also adds an airplane to the applicability. This AD was prompted by reports of intermittent or blank displays of a certain integrated display unit (IDU) that were due to an intermittent false electrical ground that was not addressed by the software installation or wiring changes required by AD 2012-24- 10. We are issuing this AD to prevent IDU malfunctions, which could affect the ability of the flightcrew to read primary displays for airplane attitude, altitude, or airspeed, and consequently reduce the ability of the flightcrew to maintain control of the airplane.
Airworthiness Directives; Airbus Airplanes
We are revising an earlier proposed airworthiness directive (AD) for all Airbus Model A318, A319, A320, and A321 series airplanes. The NPRM proposed to supersede Airworthiness Directives (AD) 2011-13-11 and AD 2013-16-09. AD 2011-13-11 currently requires an amendment of the airplane flight manual (AFM), repetitive checks of specific centralized fault display system (CFDS) messages, an inspection of the opening sequence of the main landing gear (MLG) door actuator for discrepancies if certain messages are found, and corrective actions if necessary. AD 2013-16-09 currently requires an inspection to determine airplane configuration and part numbers of the landing gear control interface unit and MLG door actuators; and, for affected airplanes, repetitive inspections of the opening sequence of the MLG door actuator, and replacement of the MLG door actuator if necessary; and provides optional terminating action for the repetitive inspections. The NPRM was prompted by a determination that the interval of the MLG door opening sequence inspection must be reduced. The NPRM proposed to reduce the interval of the MLG door opening sequence inspection, and also to replace or modify certain MLG door actuators. This action revises the NPRM by adding a flushing procedure to be performed when installing a new MLG door actuator. We are proposing this supplemental NPRM (SNPRM) to detect and correct deterioration of the damping ring and associated retaining ring of the MLG door actuator, which can sufficiently increase the friction inside the actuator to restrict opening of the MLG door by gravity, during operation of the landing gear alternate (free-fall) extension system. This condition could prevent the full extension and/or down-locking of the MLG, possibly resulting in MLG collapse during landing and consequent damage to the airplane and injury to occupants. Since these actions impose an additional burden over those proposed in the NPRM, we are reopening the comment period to allow the public the chance to comment on these proposed changes.
Proposed Amendment of Class D and Class E Airspace; Salem, OR
This action proposes to modify Class D airspace, Class E surface area airspace, and Class E airspace extending upward from 700 feet above the surface at McNary Field, Salem, OR. After further review, the FAA found some airspace unnecessary for Standard Instrument Approach Procedures for Instrument Flight Rules (IFR) operations at the airport.
Commercial Space Transportation Advisory Committee; Open Meeting
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 meeting of the Commercial Space Transportation Advisory Committee (COMSTAC). The meeting will take place on Tuesday, October 20, 2015, from 8:00 a.m. to 5:00 p.m., and Wednesday, October 21, 2015, from 8:30 a.m. to 4:30 p.m. at the National Transportation Safety Board Conference Center, 429 L'Enfant Plaza SW., Washington, DC 20594. This will be the 61st meeting of the COMSTAC. The proposed schedule for the COMSTAC working group meetings on October 20 is below:
Aviation Rulemaking Advisory Committee-New Task
The FAA assigned the Aviation Rulemaking Advisory Committee (ARAC) a new task to provide recommendations on how the agency can utilize external training providers for its new-hire air traffic controller training program. The ongoing modernization of the air traffic control system, NextGen, will continually introduce advanced tools and procedures to enhance the safety and efficiency of the National Airspace System. Controllers will continue to need to know basic air traffic control skills but will also need to understand how to operate in the future operational environment. The FAA seeks to transform the air traffic controller training structure by shifting the Agency's focus from basic air traffic control qualification training to training the certified controller work force on advanced NextGen tools and procedures. This would mirror the changes that were required in the pilot community. The Agency is exploring alternative options to utilize external training provider capabilities that would expose prospective air traffic controllers to the profession. It would also provide a level of training commensurate to the current Air Traffic Basic Qualification Training, before or during the FAA controller hiring process. This notice informs the public of the new ARAC activity and solicits membership for the new Air Traffic Controller Basic Qualification Training Working Group.
Airworthiness Directives; The Boeing Company Airplanes
We are revising an earlier proposed airworthiness directive (AD) that proposed to supersede AD 2006-22-15 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. AD 2006-22-15 requires repetitive inspections for cracking of certain panel webs and stiffeners of the nose wheel well (NWW), and corrective actions if necessary; and replacement of certain panels with new panels, which terminates the repetitive inspections. The notice of proposed rulemaking (NPRM) proposed to reduce a compliance time and add certain inspections and applicable repair. The NPRM was prompted by reports of fatigue cracking in the panel webs and stiffeners of the NWW found prior to the inspection threshold of AD 2006-22-15. This action revises the NPRM by specifying a repetitive inspection interval for a certain NWW area inspection. We are proposing this SNPRM to prevent fatigue cracking of the NWW side and top panels, which could result in a NWW depressurization event severe enough to reduce the structural integrity of the fuselage. 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; Airbus Airplanes
We propose to adopt a new airworthiness directive (AD) for certain Airbus Model A330-200 and -300 series airplanes; Model A330-200 Freighter series airplanes; and Model A340-200, -300, -500, and -600 series airplanes. This proposed AD was prompted by reports of chafed wiring at the upper left corner of the cockpit door. The affected wire bundle was not grounded on the cockpit door frame. This proposed AD would require modifying the cockpit door frame structure, installing bonding-leads to the upper cockpit door frame, and modifying the upper cockpit door plate cover. We are proposing this AD to prevent electrical shock injury to persons contacting the cockpit door.
Airworthiness Directives; Fokker Services B.V. Airplanes
We propose to adopt a new airworthiness directive (AD) for all Fokker Services B.V. Model F.27 Mark 200, 300, 400, 500, 600, and 700 airplanes. This proposed AD was prompted by a design review conducted by Fokker Services B.V. that indicated no controlled bonding provisions were present on many critical locations outside the fuel tank or connected to the fuel tank wall. This proposed AD would require installing the additional bonding provisions, and revising the maintenance or inspection program, as applicable, by incorporating fuel airworthiness limitation items and critical design configuration control limitations. We are proposing this AD to prevent an ignition source in the fuel tank vapor space, which could result in a fuel tank explosion and consequent loss of the airplane.
Airworthiness Directives; Airbus Airplanes
We propose to supersede Airworthiness Directive (AD) 2014-14- 06 for all Airbus Model A318-111 and -112 airplanes; Model A319-111, - 112, -113, -114, and -115 airplanes; Model A320-111, -211, -212, and - 214 airplanes; and Model A321-111, -112, -211, -212, and -213 airplanes. AD 2014-14-06 currently requires inspecting the aft engine mount retainers for surface finish, cracks, and failure, and replacement if necessary. Since we issued AD 2014-14-06, inspection results have shown that the main cause of crack initiation remains the vibration dynamic effect that affects both retainers, either with ``dull'' or ``bright'' surface finishes. This proposed AD would require repetitive inspections for damage, cracks, broken, and missing aft engine mount retainers, and replacement if necessary. We are proposing this AD to detect and correct failure of retainer brackets of the aft engine mount and consequent loss of the locking feature of the nuts of the inner and outer pins; loss of the pins will result in the aft mount engine link no longer being secured to the aft engine mount.
Amendment of Class E Airspace; Tracy, CA
This action corrects an error in a final rule published in the Federal Register of August 31, 2015, by amending the geographic coordinates of Tracy Municipal Airport, Tracy, CA, in Class E airspace. This does not affect the boundaries or operating requirements of the airspace.
Discontinuation of Airport Advisory Service in the Contiguous United States, Puerto Rico, and Hawaii
This action discontinues the availability Airport Advisory services within the contiguous United States, Puerto Rico, and Hawaii. The FAA is taking this action because the frequency of Remote Airport Advisories service use at the 19 locations within the contiguous United States, Puerto Rico, and Hawaii, no longer justifies the continuation of the service due to the lack of productivity.
IFR Altitudes; Miscellaneous Amendments
This amendment adopts miscellaneous amendments to the required IFR (instrument flight rules) altitudes and changeover points for certain Federal airways, jet routes, or direct routes for which a minimum or maximum en route authorized IFR altitude is prescribed. This regulatory action is needed because of changes occurring in the National Airspace System. These changes are designed to provide for the safe and efficient use of the navigable airspace under instrument conditions in the affected areas.
Agency Information Collection Activities: Requests for Comments; Clearance of Renewed Approval of Information Collection: Human Response to Aviation Noise in Protected Natural Areas Survey
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 June 22, 2015. This research is important for establishing the scientific basis for air tour management policy decisions in the National Parks as mandated by the National Parks Air Tour Management Act of 2000.
Agency Information Collection Activities: Request for Comments; Revision of an Existing Information Collection: Medical Standards and Certification
In accordance with the Paperwork Reduction Act of 1995 and Office of Management and Budget (OMB) regulations, the FAA invites public comments about our intention to request OMB approval to revise an existing information collection. The Federal Register Notice with a 60-day comment period soliciting comments on the following collection of information was published on June 22, 2015. The information collected is used to determine if applicants are medically qualified to perform the duties associated with the class of airman medical certificate sought. The FAA intends to revise the information it is collecting via FAA form 8500-8, in part, to respond to recommendations made in an April 2014 General Services Administration report entitled ``FAA Should Improve Usability of its Online Application System and Clarity of the Pilot's Medical Form.'' This change will have a negligible effect on the estimated time to complete form 8500-8.
Agency Information Collection Activities: Requests for Comments; Clearance of Renewed Approval of Information Collection: Flight Plans
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. Flight plan information is used to govern the flight of aircraft for the protection and identification of aircraft, property, and persons on the ground. The Federal Register Notice with a 60-day comment period soliciting comments on the following collection of information was published on June 22, 2015. A comment was received suggesting that the original effective date of October 1, 2015 for the removal of form 7233-1 from public use is too soon to acclimate respondents to the process change. FAA has revised the effective date to October 1, 2016 for the civilian burden for flight plan information, both domestic and international to be collected via form 7233-4, FAA International Flight Plan.
Office of Hazardous Materials Safety
In preparation for the International Civil Aviation Organization's (ICAO) Dangerous Goods Panel (DGP) meeting to be held October 19-October 30, 2015, in Montreal, Canada, the Federal Aviation Administration's (FAA) Office of Hazardous Materials Safety and the Pipeline and Hazardous Materials Safety Administration's (PHMSA) Office of Hazardous Materials Safety announce a public meeting.
Airworthiness Directives; The Boeing Company Airplanes
We are adopting a new airworthiness directive (AD) for certain The Boeing Company Model 777 airplanes. This AD was prompted by reports of latently failed fuel shutoff valves discovered during fuel filter replacement. This AD requires revising the maintenance or inspection program to include a new airworthiness limitation. We are issuing this AD to detect and correct latent failures of the fuel shutoff valve to the engine, which could result in the inability to shut off fuel to the engine and, in case of certain engine fires, an uncontrollable fire that could lead to wing failure.
Airworthiness Directives; The Boeing Company
We are adopting a new airworthiness directive (AD) for all The Boeing Company Model 757 airplanes. This AD was prompted by reports of latently failed fuel shutoff valves discovered during fuel filter replacement. This AD requires revising the maintenance or inspection program to include new airworthiness limitations. We are issuing this AD to detect and correct latent failures of the fuel shutoff valve to the engine and auxiliary power unit (APU), which could result in the inability to shut off fuel to the engine and APU and, in case of certain fires, an uncontrollable fire that could lead to structural failure.
Airworthiness Directives; The Boeing Company Airplanes
We are adopting a new airworthiness directive (AD) for all The Boeing Company Model 767 airplanes. This AD was prompted by reports of latently failed fuel shutoff valves discovered during fuel filter replacement. This AD requires revising the maintenance or inspection program to include new airworthiness limitations. We are issuing this AD to detect and correct latent failures of the fuel shutoff valve to the engine and auxiliary power unit (APU), which could result in the inability to shut off fuel to the engine and APU and, in case of certain fires, an uncontrollable fire that could lead to structural failure.
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 latently failed fuel shutoff valves discovered during fuel filter replacement. This AD requires revising the maintenance or inspection program to include new airworthiness limitations. We are issuing this AD to detect and correct latent failures of the fuel shutoff valve to the engine, which could result in the inability to shut off fuel to the engine and, in case of certain engine fires, an uncontrollable fire that could lead to wing failure.
Special Conditions: Bombardier Aerospace Inc. Model BD-500-1A10 and BD-500-1A11 Airplanes; Flight-Envelope Protection, High Incidence Protection Function
These special conditions are issued for the Bombardier Aerospace Inc. Model BD-500-1A10 and -A11 airplanes. These airplanes will have a novel or unusual design feature when compared to the state of technology and design envisioned in the airworthiness standards for transport-category airplanes. This design feature is a high incidence protection system that limits the angle of attack at which the airplane can be flown during normal low-speed operation. 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.
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