Department of Transportation July 15, 2016 – Federal Register Recent Federal Regulation Documents
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Notice of Opportunity for Public Comment on Non-Rulemaking Action To Change Land Use From Aeronautical to Non-Aeronautical at Jackson-Medgar Wiley Evers International Airport, Jackson, Mississippi
Under the provisions of title 49, U.S.C. 47153(c), notice is being given that the FAA is considering a request from the Jackson Municipal Airport Authority to waive the requirement that a 130 acre parcel of surplus property, located on Jackson-Medgar Wiley Evers International Airport, be used for aeronautical purposes.
Special Conditions: Cirrus Design Corporation, Model SF50; Whole Airplane Parachute Recovery System
These special conditions are issued for the Cirrus Design Corporation (Cirrus), model SF50 airplane. This airplane will have a novel or unusual design feature(s) associated with a whole airplane parachute recovery 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.
Proposed Agency Information Collection Activities; Comment Request
Under the Paperwork Reduction Act of 1995 (PRA), this notice announces FRA is forwarding the renewal of the information collection requirements (ICR) abstracted below to the Office of Management and Budget (OMB) for review and comment. The ICR describes the nature of the information collection and its expected burden. On February 25, 2016, OMB approved Form FRA F 1680.167 for 180 days under emergency clearance procedures. FRA seeks regular clearance of this form for the maximum period (3 years) to comply with Fixing America's Surface Transportation Act (FAST Act) requirements. The Federal Register notice with a 60-day comment period soliciting comments on the following collection of information was published on March 24, 2016.
Application of Rectrix Aviation, Inc. for Commuter Authority
The Department of Transportation is directing all interested persons to show cause why it should not issue an order tentatively finding Rectrix Aviation, Inc., fit, willing, and able to provide scheduled passenger service as a commuter air carrier using small aircraft pursuant to Part 135 of the Federal Aviation Regulations.
Applications of 21 Air, LLC for Certificate Authority
The Department of Transportation is directing all interested persons to show cause why it should not issue orders finding 21 Air, LLC, fit, willing, and able, and awarding it certificates of public convenience and necessity authorizing it to engage in interstate and foreign charter air transportation of property and mail.
Airworthiness Directives; Sikorsky Aircraft Corporation Helicopters
We propose to adopt a new airworthiness directive (AD) for Sikorsky Aircraft Corporation (Sikorsky) Model S-92A helicopters. This proposed AD would require inspecting the main transmission forward (fwd) and aft frame assembly and adjacent skins for a crack and loose fasteners and establishing life limits for certain frame assemblies. This proposed AD is prompted by fatigue analysis indicating stress concentrations as well as the discovery of a crack in the station (STA) 362 frame and skin on a Model S-92A helicopter. The proposed actions are intended to detect a crack in a frame assembly and prevent failure of a frame and subsequent loss of control of the helicopter.
Airworthiness Directives; Bombardier, Inc. Airplanes
We propose to supersede Airworthiness Directive (AD) 2013-02- 08, for all Bombardier, Inc. Model CL-600-2B19 (Regional Jet Series 100 & 440) airplanes. AD 2013-02-08 currently requires inspecting the trunnions and upper and lower pins of the horizontal stabilizer trim actuator (HSTA), and replacement or re-identification if necessary; and revising the maintenance program to include safe life limits and inspection requirements for the HSTA. Since we issued AD 2013-02-08, we determined that not all affected attachment pins and trunnions were included in the required inspections. In addition, for certain airplanes on which the replacement in AD 2013-02-08 was done, incorrect attachment hardware may have been used. This proposed AD would require measuring the diameter of certain bolts and attach holes, and, as applicable, measuring the diameter of the attach holes in the trunnions and pins, doing detailed visual inspections of the trunnions, pins, and spacers, doing corrective actions, and re-identifying trunnions and pins. This proposed AD also requires revising the maintenance or inspection program. This proposed AD also removes certain airplanes from the applicability. We are proposing this AD to prevent failure of the attachment pins and trunnions of the HSTA. This condition could result in separation of the horizontal stabilizer, and consequent loss of control of the airplane.
Airworthiness Directives; Bombardier, Inc. Airplanes
We propose to adopt a new airworthiness directive (AD) for certain Bombardier, Inc. Model DHC-8-400 series airplanes. This proposed AD was prompted by a determination by the manufacturer that shims might not have been installed between certain longerons and longeron joint fittings. This proposed AD would require repetitive inspections of the external surface of the fuselage skin panel for loose or working fasteners, and corrective action if necessary; a detailed visual inspection of the longeron joint fittings for the existence of shims and, if necessary, repetitive inspections of the longeron and the longeron joint fittings for any cracking, and corrective action if necessary. This proposed AD would also provide terminating action for certain repetitive inspections. We are proposing this AD to detect and correct missing shims between the longerons and longeron joint fittings. Such missing shims could result in a gapping condition and lead to stress corrosion cracking of the longeron joint fittings, and could adversely affect the structural integrity of the wing-to-fuselage attachment joints.
Airworthiness Directives; Bombardier, Inc. Airplanes
We propose to adopt a new airworthiness directive (AD) for certain Bombardier, Inc. Model BD-700-1A10 and BD-700-1A11 airplanes. This proposed AD was prompted by a determination that the existing instruction in a certain task in the aircraft maintenance manual (AMM) will not accomplish the intent of a certification maintenance requirement (CMR). This CMR task tests the pitch feel (PF) and rudder travel limiter actuator (RTLA) back-up modules in the flight control unit (FCU) to detect dormant failures. This proposed AD would require doing an operational test of the FCU back-up modules, and repair if necessary. We are proposing this AD to detect and correct a dormant failure of both FCU back-up modules. This condition, in combination with other failures in the FCU, may result in the inability to maintain the minimum control requirements for the PF and RTLA, which could create hazardous flight control inputs during flight.
Airworthiness Directives; Rolls-Royce plc Turbofan Engines
We propose to adopt a new airworthiness directive (AD) for all Rolls-Royce plc (RR) RB211-Trent 875-17, RB211-Trent 877-17, RB211- Trent 884-17, RB211-Trent 884B-17, RB211-Trent 892-17, RB211-Trent 892B-17, and RB211-Trent 895-17 turbofan engines. This proposed AD was prompted by a report of cracking and material release from an engine upper bifurcation fairing. This proposed AD would require repetitive inspections of the engine upper bifurcation fairing and repairing or replacing any fairing that fails inspection. We are proposing this AD to prevent failure of the engine fire protection system, engine fire, and damage to the airplane.
Special Conditions: Gulfstream Aerospace Corporation Model GVII-G500 Airplanes; Isolation or Protection of Airplane Electrical-System Security From Unauthorized Internal Access
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 a digital systems architecture requiring isolation or protection from unauthorized internal access. 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.
Classified Information: Classification/Declassification/Access; Authority To Classify Information (RRR)
This final rule updates the regulations regarding classified information to reflect changes in organizational structure, update the legal authorities, incorporate new references, and refer historical researchers and former Presidential appointees to Executive Order 13526.
Deepwater Port License Application: Delfin LNG LLC, Delfin LNG Deepwater Port
The Maritime Administration (MARAD), in cooperation with the U.S. Coast Guard (USCG) and the Federal Energy Regulatory Commission (FERC), announces the availability of the Draft Environmental Impact Statement (DEIS) for the Delfin LNG deepwater port license application for the exportation of natural gas. Delfin LNG, LLC (Delfin LNG), is the applicant. A Notice of Application that summarized the original Delfin LNG license application was published in the Federal Register on July 16, 2015 (80 FR 42162). A Notice of Intent to Prepare an Environmental Impact Statement (EIS) and Notice of Public Meetings was published in the Federal Register on July 29, 2015 (80 FR 45270). A Notice of Receipt of Amended Application was published in the Federal Register on December 24, 2015 (80 FR 80455). This Notice of Availability (NOA) incorporates the aforementioned Notices by reference. The proposed Delfin LNG deepwater port would be located in Federal waters within the Outer Continental Shelf (OCS) approximately 37.4 to 40.8 nautical miles off the coast of Cameron Parish, Louisiana. The proposed Delfin LNG deepwater port incorporates onshore components, which are subject to FERC jurisdiction. These facilities are described in the section of this Notice titled ``FERC Application.'' Publication of this notice begins a 45-day comment period, requests public participation in the environmental impact review process, provides information on how to participate in the process and announces informational open houses and public meetings in Cameron, Louisiana and Beaumont, Texas.
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