Federal Aviation Administration 2019 – Federal Register Recent Federal Regulation Documents

The FAA proposes to adopt a new airworthiness directive (AD) for various transport airplanes. This proposed AD was prompted by reports of smoke and fumes in the flight deck. This proposed AD would require modification of certain universal serial bus (USB) receptacles located in the flight deck. The FAA is proposing this AD to address the unsafe condition on these products.

The FAA proposes to adopt a new airworthiness directive (AD) for all The Boeing Company Model MD-90-30 airplanes. This proposed AD was prompted by reports indicating that certain center wing stringers and skins have been identified to potentially be susceptible to cracking. This proposed AD would require repetitive eddy current, low frequency (ETLF) inspections of the left and right side fastener holes for any crack; repetitive eddy current, high frequency (ETHF) inspections of the lower skin for any crack; and repair if any crack is found. The FAA is proposing this AD to address the unsafe condition on these products.

The FAA proposes to adopt a new airworthiness directive (AD) for certain The Boeing Company Model 757-200, -200CB, and -300 series airplanes. This proposed AD was prompted by reports of cracks in the fuselage frame web at body station (STA) 1640. This proposed AD would require, depending on configuration, a general visual inspection for any previous repair, such as any reinforcing repair or local frame replacement repair, repetitive open hole high frequency eddy current (HFEC) inspections for any crack of the fuselage frame web fastener holes, on the left and right side of the airplane, and applicable on- condition actions. The FAA is proposing this AD to address the unsafe condition on these products.

The FAA is superseding Airworthiness Directive (AD) 2017-16- 10, which applied to all The Boeing Company Model 777 airplanes. AD 2017-16-10 required repetitive inspections of the left and right side underwing longerons for any crack, and related investigative and corrective actions if necessary. This AD retains the requirements of AD 2017-16-10, reduces certain compliance times for certain airplanes, and removes airplanes from the applicability. This AD was prompted by reports of cracks on the underwing longerons. The FAA is issuing this AD to address the unsafe condition on these products.

The FAA proposes to adopt a new airworthiness directive (AD) for all The Boeing Company Model 737 series airplanes, except for Model 737-100, 200, -200C, -300, -400, and -500 series airplanes. This proposed AD was prompted by reports of separation of the lower aft wing-to-body fairing panel 194E (``fairing panel 194E'') during flight, due to worn or damaged nutplates on the support structure. This proposed AD would require repetitive inspections of fairing panel 194E, wheel well panel 193D, and support structure for discrepancies, and related investigative and corrective actions if necessary. This proposed AD would also require rework of the panels and support structure, which would terminate the repetitive inspections. The FAA is proposing this AD to address the unsafe condition on these products.

This action proposes to modify Class D airspace at Acadiana Regional Airport, New Iberia, LA. The FAA is proposing this action as the result of the decommissioning of the ACADI non-directional radio beacon, (NDB). This would enhance the safety and management of standard instrument approach procedure for instrument flight rules (IFR), operations at this airport.

This action proposes to establish Class E airspace extending upward from 700 feet above the surface at Hunt Field, Lander, WY, to accommodate new area navigation (RNAV) procedures at the airport. This action would ensure the safety and management of instrument flight rules (IFR) operations within the National Airspace System.

We propose to supersede Airworthiness Directive (AD) 2012-22- 18, which applies to all Airbus SAS Model A330-243, -243F, -341, -342, and -343 airplanes. AD 2012-22-18 requires repetitive inspections of the three inner acoustic panels of both engine air intake cowls to detect disbonding, and corrective actions if necessary. Since we issued AD 2012-22-18, we have received additional reports of engine air inlet cowl collapse. This proposed AD would retain the requirements of AD 2012-22-18 with a reduced compliance time and reduced repetitive inspection intervals. This proposed AD would also provide for an optional modification that is terminating action for the repetitive inspections. These actions are specified in a European Aviation Safety Agency (EASA) AD, which will be incorporated by reference. We are proposing this AD to address the unsafe condition on these products.

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 Federal Register Notice with a 60-day comment period soliciting comments on the following collection of information was published on March 14, 2019. The collection involves the B4UFLY smartphone app that provides situational awareness of flight restrictionsincluding locations of airports, restricted airspace, special use airspace, and temporary flight restrictionsbased on a user's current or planned flight location. In order to maintain NAS safety in proximity to airports, authorization is now required from recreational Unmanned Aircraft System (UAS) pilots to operate in controlled airspace The data collected will assist the FAA with determining the best processes to authorize recreational UAS pilots and inform air traffic control personnel of a UAS pilot's intended flight in order to assess whether the UAS may disrupt or endanger manned air traffic.

We propose to supersede Airworthiness Directive (AD) 2000-03- 20 R1, which applies to all Airbus SAS Model A300 B4-601, B4-603, and B4-620, Model A300 B4-600R series, and Model A300 F4-605R airplanes. AD 2000-03-20 R1 requires repetitive ultrasonic inspections to detect cracks on the forward fittings in the radius of a certain frame, adjacent to the tension bolts in the center section of the wings, and various follow-on actions. Since we issued AD 2000-03-20 R1, we have determined that the existing compliance times must be reduced. This proposed AD would retain the requirements of AD 2000-03-20 R1, add new airplanes to the applicability, and introduce new compliance times for the required inspections as specified in a European Aviation Safety Agency (EASA) AD, which will be incorporated by reference. We are proposing this AD to address the unsafe condition on these products.

This action modifies VHF Omnidirectional Range (VOR) Federal airways V-18, V-102, and V-278 in the vicinity of Guthrie, TX. The FAA is taking this action due to the planned decommissioning of the Guthrie, TX, VOR/Tactical Air Navigation (VORTAC) navigation aid (NAVAID), which provides navigation guidance for portions of the affected air traffic service (ATS) routes. The Guthrie VORTAC is being decommissioned as part of the FAA's VOR Minimum Operational Network (MON) program.

We are adopting a new airworthiness directive (AD) for certain Aviat Aircraft Inc. Models A-1C-180 and A-1C-200 airplanes equipped with a Rapco part number RA1798-00-1 fuel vent check valve installed on either wing or both. This AD was prompted by a report that the fuel tank vent check valves are sticking in the closed position causing fuel starvation to the engine. This AD requires revision of the airplane flight manual (AFM) to add a pre-flight check of the fuel vent check valves for proper operation and replacing any inoperative fuel vent check valve with an airworthy part. We are issuing this AD to address the unsafe condition on these products.

The FAA is adopting a new airworthiness directive (AD) for all Rolls-Royce plc (RR) RB211-524G2-19, RB211-524G2-T-19, RB211-524G3-19, RB211-524G3-T-19, RB211-524H2-19, RB211-524H2-T-19, RB211-524H-36 and RB211-524H-T-36 engines. This AD requires removal of affected low- pressure compressor (LPC) shafts. This AD was prompted by unauthorized repairs to the affected LPC shafts that reduced their expected life. The FAA is issuing this AD to address the unsafe condition on these products.

We are superseding Airworthiness Directive (AD) 2018-25-12, which applied to certain Airbus SAS Model A350-941 airplanes. AD 2018- 25-12 required modifying the vertical tail plane (VTP) tension bolts connection by adding sealant and protective treatment to the head of the connection, at the barrel nut cavities, and in the surrounding area. Since we issued AD 2018-25-12, it was determined that the instructions for certain airplanes are unclear for proper accomplishment of the required modification. This AD, for certain airplanes, requires accomplishing a revised modification and, for certain other airplanes, retains the modification required by AD 2018- 25-12, as specified in an European Aviation Safety Agency (EASA) AD, which will be incorporated by reference. We are issuing this AD to address the unsafe condition on these products.

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 collection involves information demonstrating that a launch or reentry operation involving a human participant will meet the risk criteria and requirements to ensure public safety. The information to be collected is necessary for the FAA to assess crew qualification and training; for operators to inform space flight participants and crew members of the risks associated with launch and reentry activities; for the implementation of waiver of claims; and to ensure environmental control and life support systems and other systems adequately protect public health and safety.

This action proposes to amend Class E airspace extending upward from 700 feet above the surface at Wray Municipal Airport, Wray, CO, to accommodate new area navigation (RNAV) procedures at the airport. This action would ensure the safety and management of instrument flight rules (IFR) operations within the National Airspace System. Additionally, this action proposes to remove Class E airspace extending upward from 1,200 feet above the surface at Wray Municipal Airport, Wray, CO. This airspace is wholly contained within the Denver en route airspace area and duplication is not necessary.

This notice contains a summary of a petition seeking relief from specified requirements of Federal Aviation 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 adopting an airworthiness directive (AD) for certain The Boeing Company Model 737-700C, -800, and -900ER series airplanes. This AD requires a maintenance records check to determine if any main slat track assembly has been removed, an inspection of the main slat track assemblies for a suspect lot number or a lot number that cannot be determined, and applicable on-condition actions. This AD was prompted by a report that certain main slat track assemblies were manufactured incorrectly and are affected by hydrogen embrittlement. The FAA is issuing this AD to address the unsafe condition on these products.

These special conditions are issued for the Mitsubishi Aircraft Corporation (MITAC), Model MRJ-200 airplanes. These airplanes will have a novel or unusual design feature when compared to the state of technology envisioned in the airworthiness standards for transport category airplanes. These design features are electrical and electronic systems that perform critical functions, the loss of which could be catastrophic to the airplane. The applicable airworthiness regulations do not contain adequate or appropriate safety standards for this design features. 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.

This rule establishes, amends, suspends, or removes Standard Instrument Approach Procedures (SIAPs) and associated Takeoff Minimums and Obstacle Departure Procedures (ODPs) for operations at certain airports. These regulatory actions are needed because of the adoption of new or revised criteria, or because of changes occurring in the National Airspace System, such as the commissioning of new navigational facilities, adding new obstacles, or changing air traffic requirements. These changes are designed to provide safe and efficient use of the navigable airspace and to promote safe flight operations under instrument flight rules at the affected airports.

This action modifies VHF Omnidirectional Range (VOR) Federal airways V-8, V-92, V-214, and V-438 due to the planned decommissioning of the Grantsville, MD, VOR/DME navigation aid which provides navigation guidance for segments of the routes. The Grantsville VOR/DME is being decommissioned as part of the FAA's VOR Minimum Operational Network (MON) program.

We propose to supersede Airworthiness Directive (AD) 2005-17- 14, which applies to all Airbus SAS Model A300 series airplanes; Model A300 B4-600, B4-600R, and F4-600R series airplanes, and Model A300 C4- 605R Variant F airplanes (collectively called Model A300-600 series airplanes); and Model A310 series airplanes. AD 2005-17-14 requires repetitive tests to detect desynchronization of the rudder servo actuators, and adjustment or replacement of the spring rods of the rudder servo actuators, if necessary. AD 2005-17-14 also requires repetitive tests/inspections/analyses of the rudder servo actuators, and related investigative/corrective actions if necessary. Since we issued AD 2005-17-14, analyses of the inspection results indicated that the assumptions made to establish the survey campaign were not adequate, and a new investigation determined the existing inspection procedures and compliance times do not adequately address the unsafe condition. This proposed AD would retain some requirements of AD 2005- 17-14 and revise the inspection procedures and compliance times, as specified in an European Aviation Safety Agency (EASA) AD, which will be incorporated by reference. We are proposing this AD to address the unsafe condition on these products.

We are adopting a new airworthiness directive (AD) for certain Airbus Helicopters Deutschland GmbH (Airbus Helicopters) Model MBB-BK 117 D-2 helicopters. This AD requires replacing the rescue hoist cable cut pushbutton flip guard (flip guard). This AD was prompted by reports of unintended lifting of several flip guards. We are issuing this AD to address the unsafe condition on these products.

The FAA is considering a request from Tulsa Airports Improvement Trust to change approximately 507 acres located on the east side of the airport between North Mingo Road and Highway 169 from aeronautical use to non-aeronautical use and to authorize the conversion of the airport property. The proposal consists of three parcels of land which were originally acquired under the following grants: Federal Airport Aid Program (FAAP) Nos. 9-34-032-C132 in 1963 and 3-34-032-C514 in 1965 and Airport Development Aid Program (ADAP) No.6-40-99-15 in 1978. The land comprising these parcels is outside the forecasted need for aviation development and is no longer needed for indirect or direct aeronautical use. The Airport wishes to develop this land for compatible commercial, non-aeronautical use. The Airport will retain ownership of this land and ensure the protection of Part 77 surfaces and compatible land use. The income from the conversion of these parcels will benefit the aviation community by reinvestment in the airport. Approval does not constitute a commitment by the FAA to financially assist in the conversion of the subject airport property nor a determination of eligibility for grant-in-aid funding from the FAA. The disposition of proceeds from the conversion of the airport property will be in accordance with FAA's Policy and Procedures Concerning the Use of Airport Revenue, published in the Federal Register on February 16, 1999. In accordance with section 47107(h) of Title 49, United States Code, this notice is required to be published in the Federal Register 30 days before modifying the land-use assurance that requires the property to be used for an aeronautical purpose.

This action proposes special conditions for the Airbus Model A330-300 and Model A330-900 series airplanes. These airplanes, as modified by TTF Aerospace, LLC (TTF Aerospace), 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 a lower deck mobile crew rest (LD- MCR) installed in the aft cargo compartment of Model A330-300 and Model A330-900 series airplanes. The applicable airworthiness regulations do not contain adequate or appropriate safety standards for this design feature. These proposed 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.