Department of Transportation March 3, 2017 – Federal Register Recent Federal Regulation Documents

Sunshine Act Meetings; Unified Carrier Registration Plan Board of Directors
Document Number: 2017-04317
Type: Notice
Date: 2017-03-03
Agency: Federal Motor Carrier Safety Administration, Department of Transportation
Railroad Cost of Capital-2016
Document Number: 2017-04133
Type: Notice
Date: 2017-03-03
Agency: Surface Transportation Board, Department of Transportation
The Board is instituting a proceeding to determine the railroad industry's cost of capital for 2016. The decision solicits comments on the following issues: The railroads' 2016 current cost of debt capital; the railroads' 2016 current cost of preferred equity capital (if any); the railroads' 2016 cost of common equity capital; and the 2016 capital structure mix of the railroad industry on a market value basis. Comments should focus on the various cost of capital components listed above using the same methodology followed in Railroad Cost of Capital2015, EP 558 (Sub-No. 19) (STB served Aug. 5, 2016).
Airworthiness Directives; Airbus Helicopters
Document Number: 2017-04116
Type: Proposed Rule
Date: 2017-03-03
Agency: Federal Aviation Administration, Department of Transportation
We propose to adopt a new airworthiness directive (AD) for Airbus Helicopters Model AS332C, AS332C1, AS332L, AS332L1, AS332L2, and EC225LP helicopters. This proposed AD would require inspecting the sliding cabin doors. This proposed AD is prompted by the failure of the sliding door's jettison mechanism due to corrosion. The proposed actions are intended to address the unsafe condition in these products.
Airworthiness Directives; Sikorsky Aircraft Corporation Helicopters
Document Number: 2017-04115
Type: Rule
Date: 2017-03-03
Agency: Federal Aviation Administration, Department of Transportation
We are publishing a new airworthiness directive (AD) for Sikorsky Aircraft Corporation (Sikorsky) Model S-92A helicopters. This AD requires inspecting certain bearings. This AD is prompted by reports of failed bearings with subsequent loss of tail rotor (TR) control. The actions of this AD are intended to address an unsafe condition on these helicopters.
Tariff of Tolls
Document Number: 2017-04069
Type: Rule
Date: 2017-03-03
Agency: Saint Lawrence Seaway Development Corporation, Department of Transportation
The Saint Lawrence Seaway Development Corporation (SLSDC) and the St. Lawrence Seaway Management Corporation (SLSMC) of Canada, under international agreement, jointly publish and presently administer the St. Lawrence Seaway Tariff of Tolls in their respective jurisdictions. The Tariff sets forth the level of tolls assessed on all commodities and vessels transiting the facilities operated by the SLSDC and the SLSMC. The SLSDC is revising its regulations to reflect the fees and charges levied by the SLSMC in Canada starting in the 2017 navigation season, which are effective only in Canada. An amendment to increase the minimum charge per lock for those vessels that are not pleasure craft or subject in Canada to tolls under items 1 and 2 of the Tariff for full or partial transit of the Seaway will apply in the U.S. (See SUPPLEMENTARY INFORMATION.) The Tariff of Tolls will become effective in Canada on March 20, 2017.
Seaway Regulations and Rules: Periodic Update, Various Categories
Document Number: 2017-04068
Type: Rule
Date: 2017-03-03
Agency: Saint Lawrence Seaway Development Corporation, Department of Transportation
The Saint Lawrence Seaway Development Corporation (SLSDC) and the St. Lawrence Seaway Management Corporation (SLSMC) of Canada, under international agreement, jointly publish and presently administer the St. Lawrence Seaway Regulations and Rules (Practices and Procedures in Canada) in their respective jurisdictions. Under agreement with the SLSMC, the SLSDC is amending the joint regulations by updating the Seaway Regulations and Rules in various categories. The changes update the following sections of the Regulations and Rules: Condition of Vessels; Seaway Navigation; Radio Communications; General; and, Vessels Transiting U.S. Waters. These amendments are necessary to take account of updated procedures and will enhance the safety of transits through the Seaway. Several of the amendments are merely editorial or for clarification of existing requirements. The joint regulations will become effective in Canada on March 20, 2017.
Airworthiness Directives; Airbus Airplanes
Document Number: 2017-03972
Type: Rule
Date: 2017-03-03
Agency: Federal Aviation Administration, Department of Transportation
We are adopting a new airworthiness directive (AD) for certain Airbus Model A318-112 airplanes; Model A319-111, -112, -115, -132, and -133 airplanes; Model A320-214, -232, and -233 airplanes; and Model A321-211, -212, -213, -231, and -232 airplanes. This AD was prompted by a quality control review on the final assembly line, which determined that the wrong aluminum alloy was used to manufacture several structural parts. This AD requires a one-time eddy current conductivity measurement of certain cabin and cargo compartment structural parts to determine if an incorrect aluminum alloy was used, and replacement if necessary. We are issuing this AD to address the unsafe condition on these products.
Airworthiness Directives; The Boeing Company Airplanes
Document Number: 2017-03968
Type: Rule
Date: 2017-03-03
Agency: Federal Aviation Administration, Department of Transportation
We are adopting a new airworthiness directive (AD) for The Boeing Company Model 777-200 and -300 series airplanes equipped with Rolls-Royce Model Trent 800 engines. This AD was prompted by reports of damage to the upper bifurcation forward fire seal and seal deflector, and localized damage to the insulation blanket installed just aft of the fire seal. This AD requires installing serviceable thrust reverser (T/R) halves on the left and right engines. We are issuing this AD to address the unsafe condition on these products.
Airworthiness Directives; The Boeing Company Airplanes
Document Number: 2017-03964
Type: Rule
Date: 2017-03-03
Agency: Federal Aviation Administration, Department of Transportation
We are adopting a new airworthiness directive (AD) for all The Boeing Company Model 767-200 and -300 series airplanes. This AD was prompted by an evaluation by the design approval holder (DAH) indicating that the frame-to-floor-beam joints and frames common to shear ties at certain locations of fuselage structure are subject to widespread fatigue damage (WFD). This AD requires inspections for cracking of certain frame inner chords and webs common to the floor beam joint and at frames common to the shear ties at certain sections, and corrective action if necessary. We are issuing this AD to address the unsafe condition on these products.
Airworthiness Directives; Airbus Airplanes
Document Number: 2017-03951
Type: Rule
Date: 2017-03-03
Agency: Federal Aviation Administration, Department of Transportation
We are adopting a new airworthiness directive (AD) for all Airbus Model A300 series airplanes. This AD was prompted by an evaluation by the design approval holder (DAH) that indicates that a section of the wing and aft fuselage is subject to widespread fatigue damage (WFD). This AD requires an inspection to determine if certain modifications have been done. We are issuing this AD to address the unsafe condition on these products.
Airworthiness Directives; Pilatus Aircraft Ltd. Airplanes
Document Number: 2017-03719
Type: Rule
Date: 2017-03-03
Agency: Federal Aviation Administration, Department of Transportation
We are adopting a new airworthiness directive (AD) for Pilatus Aircraft Ltd. Models PC-6, PC-6-H1, PC-6-H2, PC-6/350, PC-6/350-H1, PC- 6/350-H2, PC-6/A, PC-6/A-H1, PC-6/A-H2, PC-6/B-H2, PC-6/B1-H2, PC-6/B2- H2, PC-6/B2-H4, PC-6/C-H2, and PC-6/C1-H2 airplanes. This AD results from mandatory continuing airworthiness information (MCAI) issued 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 certain combinations of the aileron counterweight and the attaching parts possibly resulting in reduced thread engagement and leading to disconnection of the aileron counterweight from the aileron. We are issuing this AD to require actions to address the unsafe condition on these products.
Airworthiness Directives; United Instruments, Inc. Series Altimeters
Document Number: 2017-03488
Type: Rule
Date: 2017-03-03
Agency: Federal Aviation Administration, Department of Transportation
We are adopting a new airworthiness directive (AD) for certain United Instruments, Inc. 5934 series altimeters that were manufactured between January 2015 and February 2016 and installed in airplanes and helicopters. This AD was prompted by reports of certain altimeters displaying higher than actual altitude due to a slow diaphragm leak, which would affect the accuracy of the altimeters. This AD requires replacing the affected altimeters. We are issuing this AD to correct the unsafe condition on these products.
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