Federal Aviation Administration September 12, 2022 – Federal Register Recent Federal Regulation Documents
Results 1 - 5 of 5
Enforcement Policy Regarding Production Requirements for Standard Remote Identification Unmanned Aircraft
For noncompliance with the remote identification production requirements applicable to unmanned aircraft, which occurs on or before December 16, 2022, the FAA will consider all circumstances, in particular, the delay in the FAA's acceptance of a means of compliance, when exercising its discretion whether to take enforcement action.
Noise Certification Standards: Matternet Model M2 Aircraft
The Federal Aviation Administration (FAA) is promulgating noise certification standards that apply only to the Matternet Model M2 quadcopter unmanned aircraft (UA) because no generally applicable noise standards were available for this aircraft at the time the aircraft was presented for certification. Therefore, to complete the Matternet Model M2's type certification process for noise, the FAA adopts the standards in this rule for the Matternet Model M2.
Amendment of Class D and Class E Airspace and Revocation of Class E Airspace; La Crosse, WI
This action amends the Class D and Class E airspace and revokes Class E airspace at La Crosse, WI. This action due to an airspace review conducted as part of the decommissioning of the La Crosse very high frequency (VHF) omnidirectional range (VOR) as part of the VOR Minimal Operational Network (MON) Program.
Airworthiness Directives; MHI RJ Aviation ULC (Type Certificate Previously Held by Bombardier, Inc.) Airplanes
The FAA proposes to adopt a new airworthiness directive (AD) for all MHI RJ Aviation ULC Model CL-600-2C10 (Regional Jet Series 700, 701 & 702) airplanes, Model CL-600-2C11 (Regional Jet Series 550) 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 proposed AD was prompted by a report that the pressure switch gauge assembly for the cargo bay fire extinguisher container has the potential to display an incorrect pressure under certain environmental conditions. This proposed AD would require replacing affected high rate of discharge (HRD) and low rate of discharge (LRD) pressure switch gauge assemblies for the cargo bay fire extinguisher container. The FAA is proposing this AD to address the unsafe condition on these products.
Airworthiness Directives; Airbus SAS Airplanes
The FAA proposes to adopt a new airworthiness directive (AD) for all Airbus SAS Model A321-251N, A321-251NX, A321-252N, A321-252NX, A321-253N, and A321-253NX airplanes. This proposed AD was prompted by a stress analysis on the engine structure that indicated that the fail- safe lug may not be able to sustain, during one inspection interval as currently specified in an airworthiness limitations item, the loads deriving from the engagement of the secondary load path within that inspection interval for the aft engine mount system. This proposed AD would require repetitive detailed inspections of the aft engine mount and secondary load path clearance fail-safe pin and replacement of the engine if necessary, as specified in a European Union Aviation Safety Agency (EASA) AD, which is proposed for incorporation by reference. The FAA is proposing this AD to address the unsafe condition on these products.
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