Federal Aviation Administration November 24, 2015 – Federal Register Recent Federal Regulation Documents
Results 1 - 13 of 13
Agency Information Collection Activities: Requests for Comments; Clearance of Renewed Approval of Information Collection: B4UFLY Smartphone App
In accordance with the Paperwork Reduction Act of 1995, FAA invites public comments about our intention to request the Office of Management and Budget (OMB) approval to renew an information collection. The FAA's B4UFLY smartphone app will provide situational awareness of flight restrictionsincluding locations of airports, restricted airspace, special use airspaces, and temporary flight restrictionsbased on a user's current or planned flight location.
Agency Information Collection Activities: Requests for Comments; Clearance of Renewed Approval of Information Collection: Pilot Schools-FAR 141
In accordance with the Paperwork Reduction Act of 1995, FAA invites public comments about our intention to request the Office of Management and Budget (OMB) approval to renew an information collection. 49 U.S.C. 44707 empowers the Administrator of the Federal Aviation Administration (FAA) to provide for the examination and rating of civilian schools giving instruction in flying. This CFR prescribes the requirements for issuing pilot school certificates, provisional pilot school certificates and associated ratings to qualified applicants.
Agency Information Collection Activities: Requests for Comments; Clearance of Renewed Approval of Information Collection: Operating Requirements: Commuter and On-Demand Operation
In accordance with the Paperwork Reduction Act of 1995, FAA invites public comments about our intention to request the Office of Management and Budget (OMB) approval to renew an information collection. Title 49 U.S.C., section 44702 authorizes issuance of air carrier operating certificates. 14 CFR part 135 prescribes requirement for Air Carrier/Commercial Operators. The info collected shows compliance and applicant eligibility.
Approval of Noise Compatibility Program, Ted Stevens Anchorage International Airport and Lake Hood Seaplane Base, Anchorage, AK
The Federal Aviation Administration (FAA) announces its findings on the Noise Compatibility Program submitted by the Alaska Department of Transportation & Public Facilities (ADOT&PF) under the provisions of 49 U.S.C. (the Aviation Safety and Noise Abatement Act, hereinafter referred to as ``the Act'') and 14 CFR Part 150. These findings are made in recognition of the description of Federal and nonfederal responsibilities in Senate Report No. 96-52 (1980). On July 27, 2015, the FAA determined that the noise exposure maps (NEM) submitted by the ADOT&PF under Part 150 were in compliance with applicable requirements. On November 17, 2015, the FAA approved the Ted Stevens Anchorage International Airport (ANC) and Lake Hood Seaplane Base (LHD) noise compatibility program (NCP). Most of the recommendations of the program were approved.
Agency Information Collection Activities: Requests for Comments; Clearance of Renewed Approval of Information Collection: Dealer's Aircraft Registration Certificate Application
In accordance with the Paperwork Reduction Act of 1995, FAA invites public comments about our intention to request the Office of Management and Budget (OMB) approval to reinstate a previously discontinued information collection. AC Form 8050-5 is an application for a dealer's Aircraft Registration Certificate which, under 49 United States Code 1404, may be issued to a person engaged in manufacturing, distributing, or selling aircraft.
Proposed Establishment of Class E Airspace, South Naknek, AK
This action proposes to establish Class E airspace extending upward from 700 feet above the surface at South Naknek NR 2 Airport, South Naknek, AK, to accommodate new Area Navigation (RNAV) Global Positioning System (GPS) standard instrument approach procedures developed for the airport. The FAA is proposing this action to enhance the safety and management of Instrument Flight Rules (IFR) operations at the airport.
Proposed Establishment of Class E Airspace, South Bend, WA
This action proposes to establish Class E airspace at Willapa Harbor Heliport, South Bend, WA, to accommodate new standard instrument approach and departure procedures developed at the heliport. Controlled airspace is necessary for the safety and management of Instrument Flight Rules (IFR) operations at the heliport.
Airworthiness Directives; Turbomeca S.A. Turboshaft Engines
We propose to adopt a new airworthiness directive (AD) for certain Turbomeca S.A. Arriel 1E2 turboshaft engines. This proposed AD was prompted by reports of uncommanded in-flight shutdowns (IFSDs). This proposed AD would require removing the tachometer box on affected engines. We are proposing this AD to prevent failure of the tachometer box, which could lead to failure of the engine, IFSD, and loss of control of the helicopter.
Airworthiness Directives; Turbomeca S.A. Turboshaft Engines
We propose to adopt a new airworthiness directive (AD) for certain Turbomeca S.A. Arriel 2B, 2B1, 2C, 2C1, 2C2, 2D, 2E, 2S1, and 2S2 turboshaft engines. This proposed AD was prompted by a report of an uncommanded in-flight shutdown of an Arriel 2 engine caused by rupture of the 41-tooth gear, which forms part of the bevel gear in the engine accessory gearbox (AGB). This proposed AD would require inspection, and, depending on the results, removal of the engine AGB. We are proposing this AD to prevent failure of the engine AGB, which could lead to in-flight shutdown, damage to the engine, and damage to the aircraft.
Establishment of Class E Airspace; Newberry, MI
This action corrects an error in the legal description of a final rule published in the Federal Register of September 24, 2015, that establishes Class E airspace at the Newberry VHF Omni-Directional Range/Distance Measuring Equipment (VOR/DME), Newberry, MI. The legal description noted exclusionary language for Federal airways and Canadian airspace not required for this airspace.
Airworthiness Directives; Airbus Airplanes
We are adopting a new airworthiness directive (AD) for all Airbus Model A318, A319, A320, and A321 series airplanes. This AD was prompted by a determination that, in specific flight conditions, the allowable load limits on the vertical tail plane could be reached and possibly exceeded. Exceeding allowable load could result in detachment of the vertical tail plane. This AD requires modification of the pin programming flight warning computer (FWC) to activate the stop rudder input warning (SRIW) logic; and an inspection to determine the part numbers of the FWC and the flight augmentation computer (FAC), and replacement of the FWC and FAC if necessary. We are issuing this AD to prevent detachment of the vertical tail plane and consequent loss of control of the airplane.
Airworthiness Directives; ATR-GIE Avions de Transport Régional Airplanes
We are adopting a new airworthiness directive (AD) for all ATRGIE Avions de Transport R[eacute]gional Model ATR42 and ATR72 airplanes. This AD was prompted by new occurrences of certain cracked main landing gear (MLG) rear hinge pins. This AD requires identifying the serial number and part number of the MLG rear hinge pins, and replacing pins or the MLG if necessary. We are issuing this AD to detect and correct cracked rear hinge pins, which could lead to MLG structural failure, possibly resulting in collapse of the MLG and consequent injury to the occupants of the airplane.
Airworthiness Directives; Airbus Airplanes
We are superseding Airworthiness Directive (AD) 2008-22-20 for certain Airbus Model A330-200, A330-300, and A340-300 series airplanes. AD 2008-22-20 required repetitive high frequency eddy current (HFEC) inspections for cracking, repair if necessary, and modification of the upper shell structure of the fuselage. This new AD shortens certain compliance times. This AD was prompted by a determination from a fatigue and damage tolerance evaluation that the compliance times must be reduced. We are issuing this AD to prevent fatigue cracking of the upper shell structure of the fuselage, which could result in reduced structural integrity of the airplane.
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