Department of Transportation November 13, 2019 – Federal Register Recent Federal Regulation Documents
Results 1 - 9 of 9
Airworthiness Directives; The Boeing Company Airplanes
The FAA is superseding Airworthiness Directive (AD) 2019-20- 02, which applied to all The Boeing Company Model 737-600, -700, -700C, -800, -900, and -900ER series airplanes. AD 2019-20-02 required repetitive inspections for cracking of the left- and right-hand side outboard chords of frame fittings and failsafe straps at a certain station around two fasteners, and repair if any cracking is found. This AD also requires repetitive inspections for cracking of the left- and right-hand side outboard chords of frame fittings and failsafe straps at a certain station, but expands the inspection to the area around eight fasteners, and also requires repair if any cracking is found. This AD was prompted by a determination that the inspection area needs to be expanded. The FAA is issuing this AD to address the unsafe condition on these products.
Surface Transportation Project Delivery Program; Utah Department of Transportation Audit Report
The Moving Ahead for Progress in the 21st Century Act (MAP-21) established the Surface Transportation Project Delivery Program that allows a State to assume FHWA's environmental responsibilities for environmental review, consultation, and compliance under the National Environmental Policy Act (NEPA) for Federal highway projects. When a State assumes these Federal responsibilities, the State becomes solely responsible and liable for carrying out the responsibilities it has assumed, in lieu of FHWA. This program mandates annual audits during each of the first 4 years of State participation to ensure compliance with program requirements. This notice finalizes the findings of the second audit report for the Utah Department of Transportation (UDOT).
Surface Transportation Project Delivery Program; Ohio Department of Transportation Audit Report
The Moving Ahead for Progress in the 21st Century Act (MAP-21) established the Surface Transportation Project Delivery Program that allows a State to assume FHWA's environmental responsibilities for environmental review, consultation, and compliance under the National Environmental Policy Act (NEPA) for Federal highway projects. When a State assumes these Federal responsibilities, the State becomes solely responsible and liable for carrying out the responsibilities it has assumed, in lieu of FHWA. This program mandates annual audits during each of the first 4 years of State participation to ensure compliance with program requirements. This notice makes available the final report of Ohio Department of Transportation's (ODOT) third audit under the program.
Amendment of Class D and Class E Airspace, and Establishment of Class E Airspace; Spokane, WA
This action modifies Class D airspace, Class E surface area airspace, and establishes Class E airspace extending upward from 700 feet above the surface at Felts Field Airport, Spokane, WA. After a biennial review, the FAA found it necessary to amend existing airspace and establish new controlled airspace for the safety and management of Instrument Flight Rules (IFR) operations at this airport. This action makes a minor editorial change to the airspace designation and replaces the outdated term Airport/Facility Directory with the term Chart Supplement. The Class D and Class E surface areas are extended to the Spokane International Airport Class C surface area on the southwest and expanded 1.2 miles on the northeast. The Class E airspace extending upward from 700 feet above the surface is established to provide airspace for aircraft transitioning to and from Felts Field airport.
Airworthiness Directives; Aviointeriors S.p.A. Centaurus Passenger Seats
The FAA is adopting a new airworthiness directive (AD) for certain Aviointeriors S.p.A. (Aviointeriors) Centaurus passenger seats with a specific life vest pouch assembly installed. This AD was prompted by reports of life vest pouches that were installed incorrectly on certain seats. This AD requires inspection of the life vest pouch assembly and, depending on the results of the inspection, replacement of the life vest pouch assembly. The FAA is issuing this AD to address the unsafe condition on these products.
Airworthiness Directives; Airbus SAS Airplanes
The FAA is adopting a new airworthiness directive (AD) for certain Airbus SAS Model A318 and A319 series airplanes, Model A320- 211, -212, -214, -216, -231, -232, and -233 airplanes, and Model A321- 111, -112, -131, -211, -212, -213, -231, and -232 airplanes. This AD was prompted by a report that cracks were detected on frame (FR) 16 and FR 20 web holes and passenger door intercostal fitting holes at the door stop fitting locations. This AD requires repetitive rototest inspections of the holes at the door stop fittings for any cracking, and corrective actions if necessary, as specified in a European Aviation Safety Agency (EASA) AD, which is incorporated by reference. The FAA is issuing this AD to address the unsafe condition on these products.
Airworthiness Directives; Airbus SAS Airplanes
The FAA is superseding Airworthiness Directive (AD) 2012-22- 18, which applied to all Airbus SAS Model A330-243, -243F, -341, -342, and -343 airplanes. AD 2012-22-18 required repetitive inspections of the three inner acoustic panels of both engine air inlet (intake) cowls to detect disbonding, and corrective actions, if necessary. This AD continues to require all actions required by AD 2012-22-18, with a reduced initial compliance time and reduced repetitive inspection intervals. These actions are specified in a European Union Aviation Safety Agency (EASA) AD, which is incorporated by reference. This AD was prompted by additional reports of engine air inlet cowl collapse. The FAA is issuing this AD to address the unsafe condition on these products.
Airworthiness Directives; Bombardier, Inc., Airplanes
The FAA is adopting a new airworthiness directive (AD) for certain Bombardier, Inc., Model CL-600-1A11 (600), CL-600-2A12 (601), and CL-600-2B16 (601-3A and 601-3R Variants) airplanes. This AD was prompted by reports of the loss of all air data system information provided to the flightcrew, which was caused by icing at high altitudes. This AD requires revising the existing airplane flight manual (AFM) to provide the flightcrew with procedures for ``Unreliable Airspeed'' that stabilize the airplane's airspeed and attitude. The FAA is issuing this AD to address the unsafe condition on these products.
Airworthiness Directives; Airbus SAS Airplanes
The FAA is adopting a new airworthiness directive (AD) for all Airbus SAS Model A330-243, A330-243F, A330-341, A330-342, and A330-343 airplanes. This AD was prompted by reports of thrust reverser unit (TRU) beams found with evidence of thermally caused material degradation in the rearmost section of the TRU beam at certain latches. This AD requires an inspection for heat damage of each left-hand and right-hand TRU beam as specified in a European Union Aviation Safety Agency (EASA) AD, which is incorporated by reference. Depending on findings, this AD might also require inspections of the TRU beam latches, the TRU beam clevises, and the thrust reverser outer fixed structure rear area; corrective actions; and replacement of TRU beams. The FAA is issuing this AD to address the unsafe condition on these products.
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