Department of Transportation 2016 – Federal Register Recent Federal Regulation Documents

This notice contains a summary of a petition seeking relief from specified requirements of Title 14 of the Code of Federal Regulations. The purpose of this notice is to improve the public's awareness of, and participation in, the FAA's exemption process. 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.

This notice contains a summary of a petition seeking relief from specified requirements of Title 14 of the Code of Federal Regulations. The purpose of this notice is to improve the public's awareness of, and participation in, the FAA's exemption process. 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.

These special conditions are issued for the Gulfstream Aerospace Corporation (Gulfstream) GVI airplane. This airplane will have a novel or unusual design feature when compared to the state of technology envisioned in the airworthiness standards for transport- category airplanes. This design feature is non-rechargeable lithium 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.

We propose to adopt a new airworthiness directive (AD) for certain Airbus Helicopters Deutschland GmbH (Airbus Helicopters) Model MBB-BK 117 C-2 helicopters. This proposed AD would require inspecting each terminal lug and replacing any lug that has discoloration, corrosion, incorrect crimping, or incorrect installation. This proposed AD is prompted by the discovery that terminal lugs with incorrect crimping may have been installed on these helicopters. The proposed actions are intended to detect incorrectly installed or crimped terminal lugs and prevent contact resistance and reduced gastightness between the wire and terminal lug, subsequent loss of electrical power, and an electrical fire.

We are adopting a new airworthiness directive (AD) for The Boeing Company Model 787-8 and 787-9 airplanes powered by General Electric (GE) GEnx-1B engines. This AD requires revising the airplane flight manual (AFM) to provide the flight crew a revised fan ice removal procedure and a new associated mandatory flight crew briefing to reduce the likelihood of engine damage due to fan ice shedding. This AD also removes certain dispatch relief. For airplanes with certain engines, this AD also requires reworking or replacing at least one engine. This AD was prompted by a recent engine fan blade rub event that caused an in-flight non-restartable power loss. We are issuing this AD to prevent susceptibility to heavy fan blade rubs, which could result in engine damage and a possible in-flight non-restartable power loss of one or both engines.

This action establishes Class E airspace extending upward from 700 feet above the surface at Danville Municipal Airport, Danville, AR, to accommodate new Standard Instrument Approach Procedures (SIAPs) for the safety and management of Instrument flight Rules (IFR) operations at the airport.

This rule amends, suspends, or removes Standard Instrument Approach Procedures (SIAPs) and associated Takeoff Minimums and Obstacle Departure Procedures for operations at certain airports. These regulatory actions are needed because of the adoption of new or revised criteria, or because of changes occurring in the National Airspace System, such as the commissioning of new navigational facilities, adding new obstacles, or changing air traffic requirements. These changes are designed to provide for the safe and efficient use of the navigable airspace and to promote safe flight operations under instrument flight rules at the affected airports.

This rule amends, suspends, or removes Standard Instrument Approach Procedures (SIAPs) and associated Takeoff Minimums and Obstacle Departure Procedures for operations at certain airports. These regulatory actions are needed because of the adoption of new or revised criteria, or because of changes occurring in the National Airspace System, such as the commissioning of new navigational facilities, adding new obstacles, or changing air traffic requirements. These changes are designed to provide for the safe and efficient use of the navigable airspace and to promote safe flight operations under instrument flight rules at the affected airports.

We are superseding Airworthiness Directive (AD) 2012-17-13, which applied to certain The Boeing Company Model 707 airplanes, and Model 720 and 720B series airplanes. For certain airplanes, AD 2012-17- 13 required using redefined flight cycle counts; determining the type of material of the horizontal stabilizer, rear spar, and upper and lower chords on the inboard and outboard ends of the rear spar; repetitively inspecting for cracking of the horizontal stabilizer components; and repairing or replacing the chord, or modifying chord segments made of 7079 aluminum, if necessary. For all airplanes, AD 2012-17-13 required inspecting certain structurally significant items, and repairing discrepancies if necessary. This new AD adds a requirement to replace all chord segments made of 7079 aluminum with new, improved chord segments made of 7075 aluminum. This AD was prompted by a determination that all chord segments made of 7079 aluminum must be replaced with new, improved chord segments made of 7075 aluminum. We are issuing this AD to detect and correct stress corrosion and potential early fatigue cracking in the horizontal stabilizer, which could result in reduced structural integrity of the horizontal stabilizer.

These special conditions are issued for the Gulfstream Aerospace Corporation (Gulfstream) Model GVII-G500 airplane. This airplane will have a novel or unusual design feature when compared to the state of technology envisioned in the airworthiness standards for transport category airplanes. This design feature is electronic flight controls that affect maneuvering. 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.

The FHWA has forwarded the information collection request described in this notice to the Office of Management and Budget (OMB) for approval of a new information collection. We published a Federal Register Notice with a 60-day public comment period on this information collection on June 23, 2015. We are required to publish this notice in the Federal Register by the Paperwork Reduction Act of 1995.

The Department of Transportation is directing all interested persons to show cause why it should not issue an order finding Delux Public Charter, LLC fit, willing, and able, and awarding it commuter air carrier authorization.

The FAA is issuing this notice to advise owners of small unmanned aircraft systems (sUAS) used for purposes other than as model aircraft under the authority of an exemption issued by the FAA that they may register their sUAS using the web-based aircraft registration system. It also provides specific information pertaining to any exemptions that include conditions relating to the registration of small UAS.

We propose to adopt a new airworthiness directive (AD) for certain Pratt & Whitney (PW) PW4164, PW4164-1D, PW4168, PW4168-1D, PW4168A, PW4168A-1D, and PW4170 turbofan engines. This proposed AD was prompted by several instances of fuel leaks on PW engines installed with the Talon IIB combustion chamber configuration. This proposed AD would require initial and repetitive inspections of the affected fuel nozzles and their replacement with parts eligible for installation. We are proposing this AD to prevent failure of the fuel nozzles, which could lead to engine fire and damage to the airplane.

The Fixing America's Surface Transportation (FAST) Act requires FMCSA to implement a ``Beyond Compliance'' program no later than 18 months after the enactment of the Act. Through this proposed program, the FMCSA Administrator must allow recognition, either through credit recognized by a new Beyond Compliance Behavior Analysis and Safety Improvement Category (BASIC), or an improved Safety Measurement System (SMS) percentile, for a motor carrier that: (1) Installs advanced safety equipment; (2) uses enhanced driver fitness measures; (3) adopts fleet safety management tools, technologies, and programs; or (4) satisfies other standards determined appropriate by the Administrator. The FAST Act also requires that the Agency provide the opportunity for notice and comment on a process for identifying and reviewing advanced safety equipment, enhanced driver fitness measures, fleet safety management tools, technologies, and programs, and other standards for use by motor carriers to receive recognition. This proposed program will not allow relief from regulatory requirements. This notice satisfies that requirement to seek comments on this program. Comments and data received in response to this notice will be used to further develop the Beyond Compliance program.

FMCSA announces its intent to establish the Household Goods (HHG) Consumer Protection Working Group (Working Group). The Fixing America's Surface Transportation (FAST) Act requires FMCSA to establish this Working Group to provide recommendations on how to better educate and protect HHG moving customers (consumers) during an interstate HHG move. FMCSA solicits applications and nominations of interested persons to serve on the Working Group. As required by the FAST Act, the Working Group must be composed of individuals with expertise in consumer affairs, educators with expertise in how people learn most effectively, and representatives of the interstate HHG moving industry. The FAST Act mandates that the Working Group make its recommendations and the U.S. Department of Transportation (DOT) publish them no later than December 4, 2016.

Notice is hereby given of the FAA's clarification of its policy regarding the acceptance of documents submitted to the FAA Aircraft Registry with digital signatures in support of aircraft registration under 14 CFR 47.13 and conveyances or security documents submitted to the FAA Aircraft Registry regarding claims and interests under 14 CFR 49.13.

We propose to supersede Airworthiness Directive (AD) 2011-10- 01, for all Dassault Aviation Model FALCON 7X airplanes. AD 2011-10-01 currently requires repetitive functional tests of the ram air turbine (RAT) heater and repair if necessary. Since we issued AD 2011-10-01, we received a revision of an airworthiness limitations items (ALI) document, which introduces new and more restrictive maintenance requirements and airworthiness limitations for airplane structures and systems. This proposed AD would require revising the maintenance or inspection program to incorporate new maintenance requirements and airworthiness limitations. We are proposing this AD to prevent reduced structural integrity and reduced control of these airplanes due to the failure of system components.

We propose to adopt a new airworthiness directive (AD) for all Dassault Aviation Model FALCON 900EX and FALCON 2000EX airplanes. This proposed AD was prompted by a review that identified a nonconformity between the torque value applied to the screw-nuts of aileron servo actuators, and the torque value specified by the type design. This proposed AD would require replacing certain aileron servo actuators with serviceable servo actuators. We are proposing this AD to prevent desynchronization between two servo actuator barrels, which could lead to reduced control of the airplane during roll maneuvers at low altitude.

We propose to supersede Airworthiness Directive (AD) 2010-10- 13, for all BAE SYSTEMS (Operations) Limited Model BAe 146 and Avro 146 series airplanes. AD 2010-10-13 currently requires repetitive inspections of the wing fixed leading edge and front spar structure for corrosion and cracking, and repair if necessary. Since we issued AD 2010-10-13, the Design Approval Holder (DAH) has issued revised inspection procedures that eliminate a previously approved inspection procedure. This proposed AD would require revised inspection procedures. We are proposing this AD to detect and correct corrosion and cracking of the wing fixed leading edge and front spar structure, which could result in reduced structural integrity of the wing.

The FAA hereby provides notice of intent to release approximately 0.07 acres of airport property at North Perry Airport, Hollywood, FL, from the conditions, reservations, and restrictions as contained in a Quitclaim Deed agreement between the FAA and Broward County, FL, dated October 11, 1957. The release of property will allow Broward County to dispose of the property for other than aeronautical purposes. The property is located at the intersection of Pembroke Road (State Road 824) and Airport Drive South, Hollywood, Florida. The parcel is currently designated as non-aeronautical land use. The property will be released of its federal obligations in order for the FDOT to use the property for installation and maintenance of a traffic signal device and associated highway improvements. The fair market value of these parcels has been determined to be $53,900.

In accordance with the requirements of section 3506(c)(2)(A) of the Paperwork Reduction Act of 1995, this notice announces the intention of the BTS to request the Office of Management and Budget's (OMB's) approval for an information collection related to the nation's ferry operations. The information collected will be used to produce a descriptive database of existing ferry operations. A summary report of survey findings will also be published by BTS on the BTS Web page.