Federal Aviation Administration January 2020 – Federal Register Recent Federal Regulation Documents

The FAA proposes to supersede Airworthiness Directive (AD) 2005-23-09, which applies to all General Electric Company (GE) CF6- 80E1A1, -80E1A2, -80E1A3, -80E1A4, and -80E1A4/B model turbofan engines. AD 2005-23-09 requires initial and repetitive fluorescent- penetrant inspections (FPI) of certain areas of high-pressure compressor (HPC) cases, part number (P/N) 1509M97G07 and P/N 2083M69G03. Since the FAA issued AD 2005-23-09, GE performed an updated lifing analysis on the HPC case. As a result, GE found additional locations on the cases requiring FPI, revised the inspection interval for performing FPI of the existing location, and added an additional P/ N HPC case that requires inspection. This proposed AD would require an update of the Airworthiness Limitations Section (ALS) of GE Engine Manual GEK99376 and the operator's existing continuous airworthiness maintenance program (CAMP). The FAA is proposing this AD to address the unsafe condition on these products.

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 proposes to adopt a new airworthiness directive (AD) for certain The Boeing Company Model 727, 727C, 727-100, 727-100C, 727- 200, and 727-200F series airplanes. This proposed AD was prompted by reports of nuisance stick shaker activation while the airplane accelerated to cruise speed at the top of climb. This proposed AD was also prompted by an investigation of those reports that revealed that the angle of attack (AOA) (also known as angle of airflow) sensor vanes could not prevent the build-up of ice, causing the AOA sensor vanes to become immobilized, which resulted in nuisance stick shaker activation. This proposed AD would require a general visual inspection of the AOA sensors for certain AOA sensors, and replacement of affected AOA sensors. 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 ATRGIE Avions de Transport R[eacute]gional Model ATR42 airplanes and Model ATR72 airplanes. This proposed AD was prompted by reports of interference and chafing between a propeller brake hydraulic pipe and an electrical wire bundle bracket screw installed in the underwing box of the right-hand (RH) engine nacelle. This proposed AD would require a modification of the electrical wiring routing in the engine nacelles, a one-time detailed visual inspection (DVI) of the propeller brake hydraulic pipe and electrical wire bundle bracket screw head in the underwing box of the RH engine nacelle and, depending on findings, accomplishment of applicable corrective actions, as specified in a European Union Aviation Safety Agency (EASA) AD, which will be incorporated by reference. The FAA is proposing this AD to address the unsafe condition on these products.

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.

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 contact information along with the education and experience of a person seeking to be appointed as an FAA Designated Engineering Representative (DER). The information to be collected will be used to determine the eligibility and qualifications of the DER applicant.

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.

This rule amends, suspends, or removes Standard Instrument Approach Procedures (SIAPs) and associated Takeoff Minimums and Obstacle Departure Procedures 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 for the safe and efficient use of the navigable airspace and to promote safe flight operations under instrument flight rules at the affected airports.

In accordance with the Paperwork Reduction Act of 1995, FAA invites public comments about our intention to request Office of Management and Budget (OMB) approval to renew a previously approved information collection. The information collected is used by the FAA to register aircraft or record a security interest in a registered aircraft. The information required to register and prove ownership of an aircraft is required from any person wishing to register an aircraft.

This action modifies Class E airspace designated as an extension to a Class D or Class E surface area. This action also modifies Class E airspace extending upward from 700 feet above the surface. This action also removes a large area of Class E airspace extending upward from 700 feet above the surface east of the Walla Walla Regional Airport, Walla Walla, WA. Further, this action implements administrative corrections to the airport's Class D and Class E legal descriptions.

This action proposes to establish Class E airspace extending upward from 700 feet above the surface at Big Horn County Airport, Hardin, MT. The establishment of the Class E airspace will accommodate a new area navigation (RNAV) procedure and IFR departures at the airport. This action would ensure the safety and management of instrument flight rules (IFR) operations at the airport.

The FAA is adopting a new airworthiness directive (AD) for Airbus SAS Model A318 and A319 series airplanes; Model A320-211, -212, -214, -231, -232, and -233 airplanes; Model A321-111, -112, -131, -211, -212, -213, -231, and -232 airplanes; Model A330-200 and A330-200 Freighter series airplanes; Model A340-200 and -300 series airplanes; and Model A340-500 and -600 airplanes (except for airplanes equipped with flammability reduction means (FRM) approved by the FAA as compliant with the Fuel Tank Flammability Reduction (FTFR) rule). This AD was prompted by the FAA's analysis of the fuel system reviews on these models conducted by the manufacturer. This AD requires modifying the fuel quantity indicating system (FQIS) to prevent development of an ignition source inside the center fuel tank due to electrical fault conditions. This AD also provides alternative actions for cargo airplanes. This AD does not apply to airplanes equipped with FRM approved by the FAA. The FAA is 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 for a new information collection. The Federal Register Notice with a 60-day comment period soliciting comments on the following collection of information was published on November 1, 2019 (84 FR 58818). The collection involves submission of Employee Assault Prevention and Response Plans (EAPRP) for customer service agents of certificate holders conducting operations under Title 14 of the Code of Federal Regulations (CFR) part 121. The certificate holders will submit the information to be collected to the FAA for review and acceptance as required by Section 551 of Public Law 115-254, the FAA Reauthorization Act of 2018.

The FAA proposes to adopt a new airworthiness directive (AD) for certain The Boeing Company Model 787-8 and 787-9 airplanes. This proposed AD was prompted by reports that the cabin air compressor (CAC) outlet check valve failed due to fatigue of the aluminum flappers, and exposed the Y-duct to temperatures above its design limit. This proposed AD would require installing new inboard and outboard CAC outlet check valves on the left-side and right-side cabin air conditioning and temperature control system (CACTCS) packs. The FAA is proposing this AD to address the unsafe condition on these products.

This action amends the Class E airspace extending upward from 700 feet above the surface at Charles Cole Memorial Hospital Heliport, Coudersport, PA, and revokes the Class E airspace extending upward from 700 feet above the surface at Cherry Springs Airport, Galeton, PA. This action is due to an airspace review caused by the closure of the Cherry Spring Airport. The geographic coordinates of Charles Cole Memorial Hospital Heliport would also be updated to coincide with the FAA's aeronautical database. Airspace redesign is necessary for the safety and management of instrument flight rules (IFR) operations at Charles Cole Memorial Hospital Heliport.

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 for a new information collection. The Federal Register Notice with a 60-day comment period soliciting comments on the following collection of information was published on November 1, 2019. The collection involves submission of Fatigue Risk Management Plans (FRMP) for flight attendants of certificate holders operating under Title 14 of the Code of Federal Regulations. The certificate holders will submit the information to be collected to the FAA for review and acceptance as required by Section 335(b) of Public Law 115-254, the FAA Reauthorization Act of 2018.

The FAA is adopting a new airworthiness directive (AD) for certain Viking Air Limited Model CL-215-1A10 and CL-215-6B11 (CL-215T Variant) airplanes. This AD was prompted by reports of cracks on the wing lower skin under the drag angle at a certain wing station (WS). This AD requires a one-time inspection of the wing lower skin under the drag angle at a certain WS to determine if a certain repair or modification has been accomplished; repetitive visual inspections of certain fuselage structures; repetitive eddy current inspections of the front spar along a certain WS reference line, the drag angle, and all fastener holes; repetitive structural gap checks of a certain surface; and corrective actions if necessary. This AD also requires replacing certain rivets with certain fasteners, and corrective actions if necessary. The FAA is issuing this AD to address the unsafe condition on these products.

The FAA is adopting a new airworthiness directive (AD) for all Fokker Services B.V. Model F28 Mark 0100 airplanes. This AD was prompted by reports of smoke in the flight deck, in conjunction with the loss of electrical power. This AD requires replacement of affected generator power transfer contactors (GPTCs), essential bus transfer contactors (EBTCs), and auxiliary power transfer contactors (APTCs), as specified in a European Union Aviation Safety Agency (EASA) AD, which is incorporated by reference. The FAA is issuing this AD to address the unsafe condition on these products.

The FAA is adopting a new airworthiness directive (AD) for certain The Boeing Company Model 777-300ER and 777F series airplanes. This AD was prompted by an evaluation by the design approval holder (DAH) indicating that the fuselage stringers, stringer splices, and skin splice straps are subject to widespread fatigue damage (WFD). This AD requires repetitive detailed inspections of certain stringer splices and skin splice straps for any cracks, repetitive high frequency eddy current (HFEC) inspections of certain stringers and stringer splices for any cracks, and applicable on-condition actions. The FAA is issuing this AD to address the unsafe condition on these products.

The FAA is adopting a new airworthiness directive (AD) for all Bombardier, Inc., Model CL-600-2B19 (Regional Jet Series 100 & 440) airplanes, Model CL-600-2C10 (Regional Jet Series 700, 701 & 702) airplanes, Model CL-600-2D15 (Regional Jet Series 705) airplanes, Model CL-600-2D24 (Regional Jet Series 900) airplanes, and Model CL-600-2E25 (Regional Jet Series 1000) airplanes. This AD was prompted by a report that during Automatic Flight Control System (AFCS) ALTS CAP or (V) ALTS CAP mode, the flight guidance/autopilot does not account for engine failure while capturing an altitude. This AD requires revising the existing airplane flight manual (AFM) to include a limitation and an abnormal operating procedure for the AFCS. 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 Airbus Helicopters Model AS332C, AS332C1, AS332L, AS332L1, AS332L2, and EC225LP helicopters. This proposed AD would require, depending on helicopter configuration, installing skived polytetrafluoroethylene (PTFE) tape or removing skived PTFE tape and replacing the window seals. This proposed AD is prompted by a report of excessive friction between the window seal and the helicopter airframe. The actions of this proposed AD are intended to address an unsafe condition on these products.

The FAA proposes to supersede Airworthiness Directives (ADs) 2015-14-07, 2016-07-10, and 2016-24-09, which apply to The Boeing Company Model 787-8 and 787-9 airplanes. ADs 2015-14-07, 2016-07-10, and 2016-24-09 require actions related to certain flight control module (FCM) software. Since the FAA issued these ADs, the agency has received reports of unannunciated dual symmetric inboard slat skew and deficiencies in the FCM software. This proposed AD would also require installing flight control electronics (FCE) common block point 5 (CBP5) software, which would terminate the existing requirements. The FAA is proposing this AD to address the unsafe condition on these products.