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Stage: Final Publications
Regulatory Agency Final Publications
FAA AC_00-46F Aviation Safety Reporting Program
This advisory circular (AC)
provides guidance for the submission of reports under the Federal Aviation
Administration (FAA) Aviation Safety Reporting Program (ASRP). The ASRP is a
cooperative safety reporting program that invites pilots, controllers, flight attendants
(F/A), maintenance personnel, dispatchers, and other users of the National Airspace
System (NAS), or any other person, to report to the National Aeronautics and Space
Administration (NASA) actual or potential discrepancies and deficiencies in aviation
safety. NASA serves as a third party to receive and process Aviation Safety Reports.
Examples of operations covered by the program include departure, en route, approach,
and landing operations and procedures; air traffic control (ATC) procedures and
equipment; crew and ATC communications; aircraft cabin operations; aircraft movement
on the airport; near midair collisions (NMAC); aircraft maintenance and recordkeeping;
airport conditions or services; and unmanned aircraft operations. The effectiveness of this
program in improving safety depends on the free, unrestricted flow of information from
the users of the NAS. Based on information obtained from this program, the FAA will
take corrective action as necessary to remedy defects or deficiencies in the NAS. The
reports may also provide data for improving the current system and planning for a future
system.
FAA AC_00-46F
Commercial Operation of Certain Categories of Aeroplanes without an ETOPS Approval
This regulatory amendment and the associated updates to the AMC & GM to Regulation No 965/2012 and to AMC-20, harmonise EASA regulations with U.S. Federal Aviation Administration (FAA) and Transport Canada Civil Aviation (TCCA) regulation for conducting non-ETOPS operations, including updating certain requirements for operations between 120-180 minutes from an airport by large business jets (see, CAT.OP.MPA.140). Aeroplanes with an MCTOM above 45 360 kg were previously subject to 60 minute ETOPS.
Note: RMT.0695 was worked as a Stakeholder-Led Rulemaking Task (SLRT) with participation by Bombardier, Gulfstream, and Pratt & Whitney Canada with additional technical input from Airbus.
EASA In Flight Recorder Equipage Requirements for Certain Turbine-Engined Aeroplanes and Helicopters
The regulatory update and new amended AMC & GM establishes flight recorder equipage requirements for certain turbine-engined aeroplanes and helicopters with an MCTOM of 2 250 kg or more and aeroplanes with an MOPCS of more than nine, if first issued a new individual Certificate of Airworthiness on or after 5 September 2022 (see, CAT.IDE.A.191 and CAT.IDE.H.191, Lightweight flight recorder).
Runway Surface Condition Reporting and In-Flight Assessment of Landing Performance
This regulatory amendment and associated means of compliance and guidance material provide compliance with ICAO Annex 6, Part I requirements for a globally harmonised reporting format for runway surface conditions, airworthiness standards, and performance data.
The compliance date for the new standards for aeroplane landing performance calculation was deferred last year from 5 November 2020 until 12 August 2021 in response to the pandemic (see, Regulation (EU) 2020/1187).
ED Decision 2021/006/R
ED Decision 2021/005/R
Joint Industry Letter about FCC Ligado Order – One Year Later
GAMA21-14 Joint Industry Letter about Ligado Order Anniversary One Year Later – Congress and White House
FAA GA Survey Overview HERE
EUROCONTROL European Air Traffic Management Computer Emergency Response Team – 2021 Report on Cyber in Aviation
EASA SC E-19 EHPS Issue 1 Final (Apr 2021)
2021_GA Survey Results & Use_Webinar Materials – 7 Apr. 2021
EASA CM proposed_cm-prop-001 Proposed Certification Memorandum providing guidance for compliance with CS-E 515 (a) for Engine Critical Parts
The purpose of this Certification Memorandum is to provide specific guidance for applicants when
demonstrating compliance with CS-E 515 (a) for Engine Critical Parts. This CM provides guidance concerning
the recognition of non-hazardous features (an area, a region, or a zone whose localised failure will not result
in a Hazardous Engine Effect) within an Engine Critical Part and how such features may be credited within
the Engineering Plan of CS-E 515 (a).