Federal Aviation Administration April 10, 2014 – Federal Register Recent Federal Regulation Documents

Office of Commercial Space Transportation: Black Sky Training Safety Approval Performance Criteria
Document Number: 2014-08117
Type: Notice
Date: 2014-04-10
Agency: Federal Aviation Administration, Department of Transportation
This is notification of criteria used to evaluate the Black Sky Training, Inc. (BST) safety approval application. The FAA issued BST a safety approval, subject to the provisions of Title 51 U.S.C Subtitle V, ch. 509, and the orders, rules and regulations issued under it. Pursuant to Title 14 Code of Federal Regulations (14 CFR) Sec. 414.35, this Notice publishes the criteria that were used to evaluate the safety approval application.
Office of Commercial Space Transportation: Waypoint 2 Space Safety Approval Performance Criteria
Document Number: 2014-08116
Type: Notice
Date: 2014-04-10
Agency: Federal Aviation Administration, Department of Transportation
This is notification of criteria used to evaluate the Waypoint 2 Space, Inc. (W2S) safety approval application. The FAA issued W2S a safety approval, subject to the provisions of Title 51 U.S.C Subtitle V, ch. 509, and the orders, rules and regulations issued under it. Pursuant to Title 14 Code of Federal Regulations (14 CFR) Sec. 414.35, this Notice publishes the criteria that were used to evaluate the safety approval application.
Public Notice for Waiver of Aeronautical Land-Use Assurance
Document Number: 2014-08111
Type: Notice
Date: 2014-04-10
Agency: Federal Aviation Administration, Department of Transportation
The FAA is considering a proposal to change approximately 2.54 acres of airport land from aeronautical use to non-aeronautical use and to authorize the lease of airport property located at Cleveland Hopkins International, Cleveland, Ohio. The aforementioned land is not needed for aeronautical use. The property is located near the northwest corner of Brook Park Road and Rocky River Drive, north of the airport and outside the airport fence line. The property is currently vacant land not being used by the airport and is flat, weedy, and grassy. The property will be leased for the development of a gas/service station.
Airworthiness Directives; Airbus Airplanes
Document Number: 2014-08071
Type: Proposed Rule
Date: 2014-04-10
Agency: Federal Aviation Administration, Department of Transportation
We propose to adopt a new airworthiness directive (AD) for certain Airbus Model A318, A319, A320, and A321 series airplanes. This proposed AD was prompted by a report of a crack found in the fuselage during a fatigue test campaign. This proposed AD would require repetitive rototest inspections for cracking; corrective actions if necessary; and modification of the torsion box, which would terminate the repetitive inspections. We are proposing this AD to prevent cracking in the side box beam flange of the fuselage, which could affect the structural integrity of the airplane.
Airworthiness Directives; Pratt & Whitney Canada Corporation Turboprop Engines
Document Number: 2014-08009
Type: Proposed Rule
Date: 2014-04-10
Agency: Federal Aviation Administration, Department of Transportation
We propose to adopt a new airworthiness directive (AD) for certain serial number Pratt & Whitney Canada Corporation (P&WC) model PW150A turboprop engines. This proposed AD was prompted by reports of damage to a high-pressure fuel line, which could result in a high- pressure fuel leak into the engine nacelle. This proposed AD would require rerouting of the igniter cables and installation of new support brackets. We are proposing this AD to prevent high-pressure fuel leaks, which could cause engine fire and damage to the engine and the airplane.
Airworthiness Directives; Turbomeca S.A. Turboshaft Engines
Document Number: 2014-08008
Type: Rule
Date: 2014-04-10
Agency: Federal Aviation Administration, Department of Transportation
We are superseding airworthiness directive (AD) 2007-19-09R1 for all Turbomeca S.A. Arriel 2B1 turboshaft engines that do not have modification TU157 incorporated. AD 2007-19-09R1 required replacement of the hydromechanical metering unit (HMU) with a serviceable HMU. This AD requires HMU replacement; reduction of the compliance interval; and inclusion of the power turbine C2 cycle consumption rate when determining compliance times. This AD was prompted by reports of ruptures on HMU constant delta pressure valves that have less than 2,000 hours in service. We are issuing this AD to prevent failure of the HMU, which could lead to damage to the engine, and damage to the aircraft.