Federal Aviation Administration October 8, 2020 – Federal Register Recent Federal Regulation Documents

Proposed Flight Standardization Board Report, The Boeing Company 737, Revision 17 and The Boeing Company 737 Airplane Flight Manual Airspeed Unreliable Non-Normal Checklist
Document Number: 2020-22381
Type: Notice
Date: 2020-10-08
Agency: Federal Aviation Administration, Department of Transportation
The FAA announces the availability of the draft Flight Standardization Board (FSB) Report, The Boeing Company 737, Revision 17 including an addendum describing potential refinements to The Boeing Company 737 Airplane Flight Manual (AFM) Airspeed Unreliable Non-Normal Checklist, which applies to The Boeing Company Model 737-8 and 737- 9 (737 MAX) airplanes. The FAA invites public comment.
Agency Information Collection Activities: Requests for Comments; Clearance of a New Approval of Information Collection: Survey of Industry's Response to Safety Alert for Operators (SAFO) 17007
Document Number: 2020-22352
Type: Notice
Date: 2020-10-08
Agency: Federal Aviation Administration, Department of Transportation
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 collection involves survey responses from U.S. operator (Part 121 and Part 135) employees who lead departments responsible for Operations and Standards, Training, and Safety to understand how industry has addressed recommendations from SAFO 17007 and to inform future guidance on manual flight skill proficiency in future en-route and terminal environments. This information collection is necessary, as no other information sources have been identified that would provide the required information. Operator policies and procedures are not publicly shared; therefore, this is the only reliable method to gather anonymous information from a representative industry sample.
Agency Information Collection Activities: Requests for Comments; Clearance of a New Approval of Information Collection: Airman Knowledge Test Registration Collection
Document Number: 2020-22292
Type: Notice
Date: 2020-10-08
Agency: Federal Aviation Administration, Department of Transportation
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 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 October 22, 2019. The information collected is necessary to ensure compliance and proper registration of an individual for the necessary knowledge test for the certification or rating pursued by the individual.
Agency Information Collection Activities: Requests for Comments; Clearance of a New Approval of Information Collection: FAA Organization Designation Authorization (ODA) Survey
Document Number: 2020-22274
Type: Notice
Date: 2020-10-08
Agency: Federal Aviation Administration, Department of Transportation
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 February 4, 2020. The collection involves a survey of Organization Designation Authorization (ODA) holders and ODA program applicants to document and assess FAA certification and oversight activities. The information to be collected is necessary because it is required of the FAA per Section 213 of the FAA Reauthorization Act of 2018.
Airworthiness Directives; General Electric Company Turbofan Engines
Document Number: 2020-22267
Type: Rule
Date: 2020-10-08
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new airworthiness directive (AD) for all General Electric Company GE90-110B1 and GE90-115B model turbofan engines. This AD was prompted by an in-service occurrence of loss of engine thrust control resulting in uncommanded high thrust. This AD prohibits dispatch of an airplane if certain status messages are displayed on the engine indicating and crew alerting system (EICAS) and if certain conditions are present per the manufacturer's service information. As a terminating action, this AD requires revision of the existing FAA-approved minimum equipment list (MEL) by incorporating into the MEL the dispatch restrictions listed in this AD. The FAA is issuing this AD to address the unsafe condition on these products.
Airworthiness Directives; Airbus Helicopters
Document Number: 2020-22259
Type: Rule
Date: 2020-10-08
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new airworthiness directive (AD) for certain Airbus Helicopters Model SA-365N, SA-365N1, AS-365N2, AS 365 N3, EC 155B, EC155B1, AS350B3, AS355F, AS355F1, AS355F2, AS355N, AS355NP, EC130B4, and EC130T2 helicopters. This AD requires inspecting the main rotor (M/R) servo actuators, and depending on the inspection results, replacing the affected part, applying a slippage mark, and reporting information. This AD was prompted by an incident of a sudden, strong nose-up attitude followed by intensive vibrations and increased loads on the flight controls during a cruise flight. The actions of this AD are intended to address an unsafe condition on these products.
Airworthiness Directives; Airbus SAS Airplanes
Document Number: 2020-22243
Type: Rule
Date: 2020-10-08
Agency: Federal Aviation Administration, Department of Transportation
The FAA is superseding Airworthiness Directive (AD) 2018-17- 05, which applied to all Airbus SAS Model A350-941 and -1041 airplanes. AD 2018-17-05 required a check of the insulation resistance of the direct drive solenoid valve (DDSOV) of each affected electro-hydrostatic actuator (EHA) and applicable corrective actions. Since the FAA issued AD 2018-17-05, it was determined that certain EHA part numbers can be modified and re- identified as specified in a European Union Aviation Safety Agency (EASA) AD, which could inadvertently remove certain part numbers from the applicability in other EHA-related ADs including AD 2018-17-05. This AD was prompted by reports of EHA units that were returned to the manufacturer with degraded insulation resistance in the DDSOV; investigation results revealed that moisture ingress, due to incorrect sealing application, had caused this degradation. This AD was also prompted by a report of a technical issue detected on EHAs installed on inboard ailerons and elevators, causing potential erroneous monitoring of those actuators. This AD requires a check of the insulation resistance of the DDSOV of each affected EHA and applicable corrective actions, and modification or replacement of certain EHAs; as specified in two EASA ADs, which are incorporated by reference. The FAA is issuing this AD to address the unsafe condition on these products.
Airworthiness Directives; Airbus Helicopters
Document Number: 2020-22241
Type: Rule
Date: 2020-10-08
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new airworthiness directive (AD) for certain Airbus Helicopters Model AS-365N2, AS 365N3, EC 155B, EC155B1, and SA-365N1 helicopters. This AD requires modifying the main gearbox (MGB) tail rotor (T/R) drive flange installation. This AD was prompted by several reported occurrences of loss of tightening torque of the Shur-Lok nut, which serves as a retainer of the T/R drive flange. The actions of this AD are intended to address an unsafe condition on these products.
Airworthiness Directives; Airbus SAS Airplanes
Document Number: 2020-22235
Type: Rule
Date: 2020-10-08
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new airworthiness directive (AD) for certain Airbus SAS Model A330-202, -203, -223, -223F, -243, -243F, - 302, -303, -323, -343, and -941 airplanes; and Model A340-313, -541, and -642 airplanes. This AD was prompted by the results of laboratory tests on non-rechargeable lithium batteries installed in emergency locator transmitters (ELTs), which highlighted a lack of protection against currents of 28 volts DC or 115 volts AC that could lead to thermal runaway and a battery fire. This AD requires modifying a certain ELT by installing a diode between the ELT and the terminal block, 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.
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