Federal Aviation Administration November 4, 2016 – Federal Register Recent Federal Regulation Documents

Notice of Cancellation of Environmental Impact Statement for the Norfolk International Airport, Norfolk, Virginia
Document Number: 2016-26631
Type: Notice
Date: 2016-11-04
Agency: Federal Aviation Administration, Department of Transportation
The Federal Aviation Administration (FAA) announces that it has discontinued preparation of an Environmental Impact Statement (EIS) for the proposed construction of new Runway 5R/23L and associated development at Norfolk International Airport, Norfolk, Virginia. The FAA's discontinued preparation of the EIS is based upon the completion of the first phase of the EIS. Based on the results of the first phase (Scoping and Purpose & Need development), the FAA has determined that the fundamental purpose and need is not supported by the current or anticipated development needs of the Airport at this time.
Passenger Facility Charge (PFC) Program; Draft FAA Order 5500.1B
Document Number: 2016-26630
Type: Notice
Date: 2016-11-04
Agency: Federal Aviation Administration, Department of Transportation
FAA is rescinding the draft FAA Order 5500.1B, Passenger Facility Charge published on August 5, 2016, and withdrawing its request for public review and comment.
Airworthiness Directives; The Boeing Company Airplanes
Document Number: 2016-26629
Type: Rule
Date: 2016-11-04
Agency: Federal Aviation Administration, Department of Transportation
We are adopting a new airworthiness directive (AD) for all The Boeing Company Model MD-90-30 airplanes. This AD requires a detailed inspection of the forward and aft surfaces on the left and right sides at the cant station 1520 bulkhead for any crack in the upper cap and (cap) doubler, webs and doublers, stiffeners, and the lower tee cap between longerons 3 through 11, and repairs if necessary. This AD was prompted by a report of cracking in various structures in the fuselage cant station 1520 bulkhead. We are issuing this AD to detect and correct cracking in the bulkhead, which could result in reduced structural integrity of the airplane.
Establishment of Class E Airspace; Camden, AL
Document Number: 2016-26455
Type: Rule
Date: 2016-11-04
Agency: Federal Aviation Administration, Department of Transportation
This action establishes Class E airspace at Camden, AL to accommodate new Area Navigation (RNAV) Global Positioning System (GPS) Standard Instrument Approach Procedures (SIAPs) serving Camden Municipal Airport. Controlled airspace is necessary for the safety and management of instrument flight rules (IFR) operations at the airport.
Establishment of Class E Airspace; Murray, KY
Document Number: 2016-26449
Type: Rule
Date: 2016-11-04
Agency: Federal Aviation Administration, Department of Transportation
This action establishes Class E airspace at Murray, KY, to accommodate new Area Navigation (RNAV) Global Positioning System (GPS) Standard Instrument Approach Procedures (SIAPs) serving Murray Calloway County Hospital Heliport. Controlled airspace is necessary for the safety and management of instrument flight rules (IFR) operations at the heliport.
Proposed Establishment of Class E Airspace, Thermopolis, WY
Document Number: 2016-26440
Type: Proposed Rule
Date: 2016-11-04
Agency: Federal Aviation Administration, Department of Transportation
This action proposes to establish Class E airspace extending upward from 700 feet above the surface at Hot Springs County Airport, Thermopolis, WY, to support the development of Instrument Flight Rules (IFR) operations under standard instrument approach and departure procedures at the airport, for the safety and management of aircraft within the National Airspace System.
Amendment of Class D and Class E Airspace; Eugene, OR, and Corvallis, OR
Document Number: 2016-26439
Type: Rule
Date: 2016-11-04
Agency: Federal Aviation Administration, Department of Transportation
This action amends Class E airspace designated as an extension, and Class E airspace extending upward from 700 feet above the surface at Mahlon Sweet Field Airport, Eugene, OR, to accommodate airspace redesign for the safety and management of Instrument Flight Rules (IFR) operations at the airport. Corvallis Municipal Airport is removed from the Mahlon Sweet Field Airport regulatory text by creating a stand-alone airspace designation for the airport. Additionally, this action updates the airport reference points for these airports in Class D and E airspace, as well as removes the Notice to Airmen (NOTAM) requirement noted in Class E surface area airspace.
Amendment of Class E Airspace; Albany, OR
Document Number: 2016-26437
Type: Rule
Date: 2016-11-04
Agency: Federal Aviation Administration, Department of Transportation
This action amends Class E airspace at Albany Municipal Airport, Albany, OR. Advances in Global Positioning System (GPS) mapping accuracy and a reliance on precise geographic coordinates to define airport and airspace reference points have made this airspace redesign necessary for the safety and management of Instrument Flight Rules (IFR) operations.
Proposed Amendment of Class E Airspace, Monongahela, PA
Document Number: 2016-26436
Type: Proposed Rule
Date: 2016-11-04
Agency: Federal Aviation Administration, Department of Transportation
This action proposes to amend Class E airspace at Monongahela, PA, as the Allegheny VHF Omni-directional Range, (VOR), has been decommissioned, requiring airspace reconfiguration at Rostraver Airport. Controlled airspace is necessary for the safety and management of instrument flight rules (IFR) operations at the airport.
Airworthiness Directives; Pilatus Aircraft Ltd. Airplanes
Document Number: 2016-26431
Type: Rule
Date: 2016-11-04
Agency: Federal Aviation Administration, Department of Transportation
We are adopting a new airworthiness directive (AD) for all 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 the aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as wear and cracks on the stabilizer-trim attachment and structural components. We are issuing this AD to require actions to address the unsafe condition on these products.
Airworthiness Directives; Pilatus Aircraft Ltd. Airplanes
Document Number: 2016-26429
Type: Proposed Rule
Date: 2016-11-04
Agency: Federal Aviation Administration, Department of Transportation
We propose to adopt 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 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 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 proposed AD to require actions to address the unsafe condition on these products.
Airworthiness Directives; Turbomeca S.A. Turboshaft Engines
Document Number: 2016-26335
Type: Proposed Rule
Date: 2016-11-04
Agency: Federal Aviation Administration, Department of Transportation
We propose to adopt a new airworthiness directive (AD) for all Turbomeca S.A. Arriel 2B turboshaft engines. This proposed AD was prompted by a report of an uncommanded in-flight shutdown (IFSD) on a single-engine helicopter, caused by a low returning spring rate of the needle of the hydro-mechanical metering unit (HMU). This proposed AD would require removing any pre-modification (mod) TU 158 HMU and replacing with a part eligible for installation. We are proposing this AD to prevent failure of the HMU, failure of the engine, IFSD, and loss of the helicopter.
Airworthiness Directives; Saab AB, Saab Aeronautics (Formerly Known as Saab AB, Saab Aerosystems) Airplanes
Document Number: 2016-26327
Type: Rule
Date: 2016-11-04
Agency: Federal Aviation Administration, Department of Transportation
We are superseding Airworthiness Directive (AD) 2012-24-06 for certain Saab AB, Saab Aeronautics Model 340A (SAAB/SF340A) and SAAB 340B airplanes. AD 2012-24-06 required replacing the stall warning computer (SWC) with a new SWC that provides an artificial stall warning in icing conditions, and modifying the airplane for the replacement of the SWC. This new AD adds airplanes to the applicability, and adds requirements to replace the existing SWCs with new, improved SWCs, and to modify the airplane for the new replacement of the SWC. This new AD also reduces the compliance time for replacing the SWCs. This AD was prompted by a determination that airplanes with certain modifications were excluded from the applicability in AD 2012-24-06, and are affected by the identified unsafe condition; and that the SWC required by AD 2012-24-06 contained erroneous logic. We are issuing this AD to prevent natural stall events during operation in icing conditions, which could result in loss of control of the airplane.
Airworthiness Directives; The Boeing Company Airplanes
Document Number: 2016-25958
Type: Rule
Date: 2016-11-04
Agency: Federal Aviation Administration, Department of Transportation
We are superseding Airworthiness Directive (AD) 2006-20-11 for certain The Boeing Company Model 757-200, -200CB, and -200PF series airplanes. AD 2006-20-11 required initial and repetitive detailed or high frequency eddy current (HFEC) inspections for cracks around the rivets at the upper fastener row of the skin lap splice of the fuselage, and repair of any crack found. This new AD no longer allows the detailed inspections and instead requires repetitive external HFEC inspections for cracking of the skin lap splices of the fuselage, and repair if necessary. This AD was prompted by an evaluation done by the design approval holder (DAH) indicating that the fuselage skin lap splice is subject to widespread fatigue damage (WFD). We are issuing this AD to detect and correct fatigue cracking at certain skin lap splice locations of the fuselage, which could result in reduced structural integrity and rapid decompression of the airplane.