Federal Aviation Administration 2015 – Federal Register Recent Federal Regulation Documents

These special conditions are issued for the Dassault Model Falcon 5X 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 hydrophobic windshield coatings in lieu of windshield wipers. 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.

We propose to adopt a new airworthiness directive (AD) for all The Boeing Company Model 747-400F series airplanes. This proposed AD was prompted by an analysis of the production methods used to increase fatigue resistance of the upper closure fittings at the nose cargo door portal's C-3 frame, which indicated that cracking could start too early to be caught in a timely manner by the inspection or maintenance program. This proposed AD would require inspections of the upper closure fitting and connected strap and doubler at the nose cargo door portal for cracking, and related investigative and corrective actions if necessary. We are proposing this AD to detect and correct such cracking, which could result in sudden decompression and loss of the airplane's structural integrity.

We are adopting a new airworthiness directive (AD) for certain CFM International S.A. (CFM) CFM56-7B and CFM56-3 turbofan engines. This AD was prompted by a report of an uncommanded in-flight shutdown (IFSD) on a CFM CFM56-7B engine following rupture of the 73-tooth gearshaft located in the engine accessory gearbox (AGB). This AD requires AGB/transfer gearbox (TGB) magnetic chip detector (MCD) inspection of the affected gearshafts until removal. We are issuing this AD to prevent failure of certain engine AGB gearshafts, which could lead to failure of one or more engines, loss of thrust control, and damage to the airplane.

The FAA is issuing this notice to advise the public of the sixteenth NextGen Advisory Committee meeting.

We propose to supersede Airworthiness Directive (AD) 2012-12- 04, which applies to certain The Boeing Company Model 737-300, -400, and -500 series airplanes. AD 2012-12-04 currently requires repetitive external detailed inspections and nondestructive inspections to detect cracks in the fuselage skin along the chem-mill steps at stringers S-1 and S-2R, between station (STA) 400 and STA 460, and repair if necessary. Since we issued AD 2012-12-04, we have determined that, for certain airplanes, the skin pockets adjacent to the Air Traffic Control (ATC) antenna are susceptible to widespread fatigue damage. This proposed AD would require a preventive modification of the fuselage skin at crown stringers S-1 and S-2R. This proposed AD would reduce inspection thresholds and repetitive intervals for certain airplanes. We are proposing this AD to detect and correct fatigue cracking of the fuselage skin panels at the chem-mill steps, which could result in sudden fracture and failure of the fuselage skin panels, and consequent rapid decompression of the airplane.

The Farm Credit Administration (FCA) Board recently updated its Policy Statement on Equal Employment Opportunity and Diversity.

Notice is hereby given, pursuant to the Government in the Sunshine Act, of the regular meeting of the Farm Credit Administration Board (Board).

The Office of the Comptroller of the Currency (OCC), Board of Governors of the Federal Reserve System (Board), Federal Deposit Insurance Corporation (FDIC), the Farm Credit Administration (FCA), and the National Credit Union Administration (NCUA) (collectively, the Agencies) are amending their regulations regarding loans in areas having special flood hazards to implement certain provisions of the Homeowner Flood Insurance Affordability Act of 2014 (HFIAA), which amends some of the changes to the Flood Disaster Protection Act of 1973 mandated by the Biggert-Waters Flood Insurance Reform Act of 2012 (Biggert-Waters). Specifically, the final rule requires the escrow of flood insurance payments on residential improved real estate securing a loan, consistent with the changes set forth in HFIAA. The final rule also incorporates an exemption in HFIAA for certain detached structures from the mandatory flood insurance purchase requirement. Furthermore, the final rule implements the provisions of Biggert-Waters related to the force placement of flood insurance. Finally, the final rule integrates the OCC's flood insurance regulations for national banks and Federal savings associations. The Agencies plan to address the private flood insurance provisions in Biggert-Waters in a separate rulemaking.

The Federal Aviation Administration (FAA) announces its intent to host Public Workshops for the Draft Written Re-Evaluation of the O'Hare Modernization Environmental Impact Statement (Draft Re- Evaluation) for Chicago O'Hare International Airport, Chicago, Illinois. The Draft Re-Evaluation will identify the potential environmental impacts associated with the construction schedule modification that alters the timing for commissioning new Runway 10R/28L, new Runway 9C/ 27C, and the extension of Runway 9R/27L at O'Hare International Airport pursuant to the National Environmental Policy Act. The FAA will host Public Workshops on the Draft Re-Evaluation. The Public Workshops on the Draft Re-Evaluation will be held on the following dates: Monday, August 10, 2015, at White Eagle Banquets, 6839 North Milwaukee Avenue, Niles, Illinois 60714; Tuesday, August 11, 2015, at Taft High School, 6530 West Bryn Mawr Avenue, Chicago, Illinois 60631; Wednesday, August 12, 2015, at Monty's Elegant Banquets, 703 South York Road, Bensenville, Illinois 60106; Thursday, August 13, 2015, at Belvedere Events and Banquets, 1170 West Devon Avenue, Elk Grove Village, Illinois 60007. Each Public Workshop will start at 1 p.m. (Central Standard Time), and registration to participate in the Public Workshops will conclude by 9 p.m. (Central Standard Time). Representatives of FAA and its consultants will be available to provide information about the Draft Re-Evaluation. Spanish language translators will be available at the Public Workshops. If you need the assistance of a translator, other than Spanish, please call Ms. Amy Hanson at (847) 294-7354 by August 3, 2015. The Draft Re-Evaluation will be available for review on line at (https://www.faa.gov/airports/airport_development/omp/eis_re-e val/) and at libraries around O'Hare International Airport. The FAA will issue a separate notice at the time the Draft Re-Evaluation is available.

This notice contains a summary of a petition seeking relief from specified requirements of Title 14 of the Code of Federal Regulations. The purpose of this notice is to improve the public's awareness of, and participation in, the FAA's exemption process. Neither publication of this notice nor the inclusion or omission of information in the summary is intended to affect the legal status of the petition or its final disposition.

The FAA is issuing this notice to advise the public of the sixth meeting of the Special Committee 231.

This notice contains a summary of a petition seeking relief from specified requirements of Title 14, Code of Federal Regulations (14 CFR). The purpose of this notice is to improve the public's awareness of, and participation in, this aspect of the FAA's regulatory activities. Neither publication of this notice nor the inclusion or omission of information in the summary is intended to affect the legal status of the petition or its final disposition.

These special conditions are issued for the Pratt and Whitney Canada PW210A engine model. This engine will have a novel or unusual design featurean additional one engine inoperative (OEI) rating that combines the 30-second and 2-minute OEI ratings into a single rating. 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.

We propose to adopt a new airworthiness directive (AD) for all Airbus Model A318, A319, and A321 series airplanes. This proposed AD was prompted by reports of in-flight loss of fixed and hinged main landing gear (MLG) fairings, and reports of post-modification MLG fixed fairing assemblies that have wear and corrosion. This proposed AD would require, for certain airplanes, repetitive replacements of the fixed fairing upper and lower attachment studs of both the right-hand (RH) and left-hand (LH) MLG; and repetitive inspections for corrosion, wear, fatigue, cracking, and loose studs of each forward stud assembly of the fixed fairing door upper and lower forward attachment of both RH and LH MLG; and replacement if necessary. This proposed AD also provides an optional terminating modification for the repetitive replacements of the fixed fairing upper and lower attachment studs. We are proposing this AD to prevent in-flight detachment of an MLG fixed fairing and consequent damage to the airplane.

This notice summarizes the inadequacies of hook and loop fasteners as a means for securing automatic fixed (AF) and automatic potable (AP) ELTs, and avoids placing an undue burden on aircraft owners while acknowledging the voluntary efforts of ELT manufacturers to improve designs.

We are adopting a new airworthiness directive (AD) for Bell Helicopter Textron Canada (BHTC) Model 430 helicopters to require inspecting the tail rotor control tube assembly (control tube) and either repairing or replacing the control tube. This AD was prompted by two reports of failure of the control tube bonded clevis. The actions of this AD are intended to prevent failure of a control tube bonded clevis, which could lead to failure of the control tube and subsequent loss of helicopter control.

We are adopting a new airworthiness directive (AD) for certain Bombardier, Inc. Model DHC-8-400 series airplanes. This AD was prompted by a report of loose bolts that are intended to secure the translating door crank assembly to the outside handle shaft. This AD requires a detailed inspection for loose bolts on the aft translating door crank assembly, and removal and reinstallation of the bolts. We are issuing this AD to prevent loose bolts from falling out. If both bolts become loose or fall out after the door is closed and locked, the door cannot be opened from inside or outside, which could impede evacuation in the event of an emergency.

This notice contains a summary of a petition seeking relief from specified requirements of Title 14, Code of Federal Regulations (14 CFR). The purpose of this notice is to improve the public's awareness of, and participation in, this aspect of the FAA's regulatory activities. Neither publication of this notice nor the inclusion or omission of information in the summary is intended to affect the legal status of the petition or its final disposition.

In accordance with the National Environmental Policy Act of 1969, as amended (NEPA; 42 United States Code 4321 et seq.), Council on Environmental Quality NEPA implementing regulations (40 Code of Federal Regulations parts 1500 to 1508), and FAA Order 1050.1E, Change 1, Environmental Impacts: Policies and Procedures, the FAA is announcing the availability of the Final EA and FONSI/ROD for the Houston Spaceport.

We propose to adopt a new airworthiness directive (AD) for Piaggio Aero Industries S.p.A Model P-180 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 the need to restore the safe fatigue life of the bulkhead structure. We are issuing this proposed AD to require actions to address the unsafe condition on these products.

We propose to adopt a new airworthiness directive (AD) for all Airbus Model A318-111 and -112 airplanes; Model A319-111, -112, and - 115 airplanes; Model A320-214 airplanes; and Model A321-111, -112, - 211, -212, and -213 airplanes. This proposed AD was prompted by reports of cracked cadmium-plated lock nuts that attach the hinge to the fan cowl door. This proposed AD would require inspecting to determine the serial number of each engine fan cowl door, inspecting for cracking of the hinge lock nuts of any affected door, and replacing the lock nuts if necessary. We are proposing this AD to detect and correct cracking of the hinge lock nuts, which could result in separation of the hinge from the fan cowl door, in-flight loss of the door, and consequent damage to the airplane.

We propose to supersede Airworthiness Directive (AD) 2008-26- 07, which applies to all McDonnell Douglas Model DC-8-11, DC-8-12, DC- 8-21, DC-8-31, DC-8-32, DC-8-33, DC-8-41, DC-8-42, and DC-8-43 airplanes; Model DC-8-50 series airplanes; Model DC-8F-54 and DC-8F-55 airplanes; Model DC-8-60 series airplanes; Model DC-8-60F series airplanes; Model DC-8-70 series airplanes; and Model DC-8-70F series airplanes. AD 2008-26-07 currently requires repetitive inspections of the lower skin and stringers at certain stations, and corrective actions if necessary. This proposed AD is intended to complete certain mandated programs intended to support the airplane reaching its limit of validity (LOV) of the engineering data that support the established structural maintenance program. This proposed AD would also require an eddy current high frequency (ETHF) inspection for cracks of the fastener open holes common to the lower skins, stringers, and splice fittings at a certain station; installation of external doublers and fasteners and repetitive eddy current low frequency (ETLF) inspections around the fasteners for any crack; and corrective actions if necessary. We are proposing this AD to detect and correct cracks in the lower skins, stringers, and fastener holes of the splice fittings, which could result in the loss of structural integrity of the airplane.

The FAA is issuing this notice to advise the public of the sixty-sixth meeting of the Special Committee 135.

The FAA is issuing this notice to advise the public of the fifth meeting of the Special Committee 229.

The Federal Aviation Administration (FAA) proposes to rule and invites public comment on the application for a release of approximately 5,037 square feet of airport property at the Elko Municipal Airport (Airport), City of Elko, Nevada. The City of Elko proposes to release the airport land in order to acquire an equal 5,037 square feet parcel of privately-owned land. The land exchange was proposed after a 2011 deed survey disclosed that the airport perimeter fence encroached into private property abutting the airport. Relocation of the fence is not practical due to the cost associated with moving the fence and underground utilities. The parties concluded that the encroachment problem could be resolved with an equitable land exchange. Since the release land is not needed for airport purposes, the exchange will not negatively impact the airport or civil aviation.