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SAE AIR5120 - ENGINE MONITORING SYSTEM RELIABILITY AND VALIDITY Organization: SAE
Date: 2016-11-01
Description: Purpose For Engine Monitoring Systems to meet their potential for improved safety and reduced operation and support costs, significant attention must be focused on their reliability and validity throughout the life cycle This AIR will provide program managers, designers, developers and customers a concise reference of the activities, approaches and considerations for the development and verification of a highly reliable engine monitoring system When applying the guidelines of this AIR it should be noted that engine monitoring systems physically or functionally integrated with the engine control system and/or performing functions that affect engine safety or are used to effect continued operation or return to service decisions shall be subject to the Type Investigation of the product in which they'll be incorporated and have to show compliance with the applicable airworthiness requirements as defined by the responsible Aviation Authority.
EUROCAE ED 75 - MINIMUM AVIATION SYSTEM PERFORMANCE STANDARDS: REQUIRED NAVIGATION PERFORMANCE FOR AREA NAVIGATION Organization: EUROCAE
Date: 2014-10-01
Description: This document contains Minimum Aviation System Performance Standards (MASPS) for area navigation systems operating in an RNP environment.
FAA-E-2835 - ENVIRONMENTAL REMOTE MONITORING SUBSYSTEM (ERMS) (RETROFIT FACILITIES ONLY) Organization: FAA
Date: 1989-04-14
Description: This specification establishes the Federal Aviation Administration's (FAA's) functional, performance, interface, development, and installation requirements for the retrofit of environmental remote monitoring subsystems (ERMS) at selected National Airspace System (NAS) facilities. Purpose.
ASTM - 15.11 - CONSUMER PRODUCTS; LIGHT SPORT AIRCRAFT; UNMANNED AIRCRAFT SYSTEMS; AIRCRAFT SYSTEMS; UNMANNED MARITIME VEHICLE SYSTEMS (UMVS); LANGUAGE SERVICES AND PRODUCTS; GENERAL AVIATION AIRCRAFT - TO PURCHASE CALL 1-800-854-7179 USA/CANADA OR 303-397-7956 WORLDWIDE Organization: ASTM
Date: 2016-11-01
Description: General Aviation Aircraft - Addresses issues related to design and construction, systems and performance, quality acceptance tests, and safety monitoring for general aviation aircraft that is less than 19,000 pounds and 12 passengers.
API/EI 1550 - HANDBOOK ON EQUIPMENT USED FOR THE MAINTENANCE AND DELIVERY OF CLEAN AVIATION FUEL - FIRST EDITION; NOW COPYRIGHTED BY EI * TO PURCHASE CALL 1-800-854-7179 USA/CANADA OR 303-397-7956 WORLDWIDE Organization: API
Date: 2007-10-01
Description: • Certain aspects of the design of other fuel cleanliness monitoring/control equipment that may be used in aviation fuel handling systems in the near future.
SAE/TP - 2010-01-1765 - SOH RECOGNITION OF LI-ION AVIATION BATTERIES VIA PASSIVE DIAGNOSTIC DEVICE Organization: SAE/TP
Date: 2010-11-02
Description: SOH includes information regarding battery energy, power and residual cycle life along with monitoring overall battery safety. This paper describes an SOH recognition technique for on-board Li-Ion aviation batteries and discusses a passive diagnostic device (PDD), that analyzes input data derived from normal system parameters such as battery current, voltage and ambient temperature.
SAE/TP - 2006-01-2444 - AN APPROXIMATE GRAPH MATCHING TECHNIQUE FOR INTEGRITY MONITORING IN INTEGRATED INTELLIGENT FLIGHT DECK APPLICATIONS Organization: SAE/TP
Date: 2006-08-29
Description: In order to improve safety of general aviation aircrafts, NASA is exploring the role of the Integrated Intelligent Flight Deck (IIFD) within the cockpit.
FAA - FO JO 1000.40 - AIR TRAFFIC ORGANIZATION TERMINAL SERVICES SAFETY MANAGEMENT SYSTEM Organization: FAA
Date: 2009-03-26
Description: The Federal Aviation Administration (FAA) assigns the highest priority to safety at all levels in the organization and continually strives to improve safety within the National Airspace System (NAS).
SAE AIR6212 - USE OF HEALTH MONITORING SYSTEMS TO DETECT AIRCRAFT EXPOSURE TO VOLCANIC EVENTS Organization: SAE
Date: 2016-12-01
Description: The document includes results of initiatives with the Federal Aviation Administration (FAA), the European Aviation Safety Agency (EASA), the International Civil Aviation Organization (ICAO), Transport Canada, various research organizations, Industry and other subject matter experts.
SAE/TP - 2010-01-1770 - SYSTEM INTEGRATION OF A SAFE, HIGH POWER, LITHIUM ION MAIN BATTERY INTO A CIVIL AVIATION AIRCRAFT Organization: SAE/TP
Date: 2010-11-02
Description: Emergency discharge with failed electronics is enabled with the selection of a less volatile chemistry, the use of an analog Module Management System for cell balancing and protection, and the use of a microcontroller-based digital Central Monitoring System that reports health. System safety failure hazard assessment is considered Major, and the battery software is certified to the requirements of RTCA DO-178B, Design Assurance Level C.
SAE AIR5665 - (R) ARCHITECTURE FRAMEWORK FOR UNMANNED SYSTEMS Organization: SAE
Date: 2013-02-01
Description: As Unmanned Systems gain acceptance, the focus of the Framework has moved from individual systems to systems of systems. Finally, as the abilities of Unmanned Systems grow, it has been necessary to ensure that the capabilities described herein are supportive of more autonomous systems, while still enabling the teleoperated systems.
ICAO 9863 - AIRBORNE COLLISION AVOIDANCE SYSTEM (ACAS) MANUAL - SECOND EDITION; INCOPORATED CORRIGENDUM 1: 8/21/2012 AND CORRIGENDUM 2: 09/26/2012 Organization: ICAO
Date: 2012-01-01
Description: Scope and target audience This manual aims to describe all the important aspects of ACAS and the implications for: a) aviation regulators; b) aircraft operating agencies; c) flight crew; d) maintenance engineers; e) air navigation service providers (ANSPs); f) air traffic controllers; and g) persons conducting safety studies.
DS/EN 1846-3 - FIREFIGHTING AND RESCUE SERVICE VEHICLES - PART 3: PERMANENTLY INSTALLED EQUIPMENT - SAFETY AND PERFORMANCE Organization: DS
Date: 2013-08-02
Description: The permanently installed equipment covered by this Part of this European Standard is given below: - water installation; - liquid additive installation; - monitor; - equipment gantries; - demountable systems using a hydraulic hook arm.
SNV - SN EN 1846-3 - FIREFIGHTING AND RESCUE SERVICE VEHICLES - PART 3: PERMANENTLY INSTALLED EQUIPMENT - SAFETY AND PERFORMANCE Organization: SNV
Date: 2013-10-01
Description: The permanently installed equipment covered by this Part of this European Standard is given below: - water installation; - liquid additive installation; - monitor; - equipment gantries; - demountable systems using a hydraulic hook arm.
NBN - EN 1846-3 - FIREFIGHTING AND RESCUE SERVICE VEHICLES - PART 3: PERMANENTLY INSTALLED EQUIPMENT - SAFETY AND PERFORMANCE Organization: NBN
Date: 2013-09-20
Description: The permanently installed equipment covered by this Part of this European Standard is given below:- water installation;- liquid additive installation;- monitor;- equipment gantries;- demountable systems using a hydraulic hook arm.
NBN - EN 1846-3 - FIREFIGHTING AND RESCUE SERVICE VEHICLES - PART 3: PERMANENTLY INSTALLED EQUIPMENT - SAFETY AND PERFORMANCE Organization: NBN
Date: 2013-09-20
Description: The permanently installed equipment covered by this Part of this European Standard is given below:- water installation;- liquid additive installation;- monitor;- equipment gantries;- demountable systems using a hydraulic hook arm.
DIN EN 1846-3 - FIREFIGHTING AND RESCUE SERVICE VEHICLES - PART 3: PERMANENTLY INSTALLED EQUIPMENT - SAFETY AND PERFORMANCE Organization: DIN
Date: 2013-11-01
Description: The permanently installed equipment covered by this Part of this European Standard is given below: - water installation; - liquid additive installation; - monitor; - equipment gantries; - demountable systems using a hydraulic hook arm.
CEN - EN 1846-3 - FIREFIGHTING AND RESCUE SERVICE VEHICLES - PART 3: PERMANENTLY INSTALLED EQUIPMENT - SAFETY AND PERFORMANCE Organization: CEN
Date: 2013-07-01
Description: The permanently installed equipment covered by this Part of this European Standard is given below: - water installation; - liquid additive installation; - monitor; - equipment gantries; - demountable systems using a hydraulic hook arm.
ITU-R REPORT M.2204 - CHARACTERISTICS AND SPECTRUM CONSIDERATIONS FOR SENSE AND AVOID SYSTEMS USE ON UNMANNED AIRCRAFT SYSTEMS Organization: ITU-R
Date: 2010-11-01
Description: The second class involves sensor(s) or electronic system(s) monitoring the air space from the ground and is referred to as ground-based sense and avoid (GBS&A).
SAE ARP5120 - AIRCRAFT GAS TURBINE ENGINE HEALTH MANAGEMENT SYSTEM DEVELOPMENT AND INTEGRATION GUIDE Organization: SAE
Date: 2016-03-01
Description: When applying the guidelines of this ARP it should be noted that engine monitoring systems may be physically or functionally integrated with the engine control system and may also affect safety or be used to effect continued operation or return to service.

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