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CURRENT
2012-05-29
Standard
AIR4979A
The primary objective of this document is to describe the systematic and random measurement uncertainties which may be expected when testing gas turbine engines in a range of different test facilities. The documentation covers a "traditional" method for estimating pretest uncertainties and a "new" method for computing and comparing posttest uncertainties. To determine these posttest uncertainties, data generated during the AGARD Uniform Engine Test Program (UETP) were analyzed and compared to the pretest estimates. The proposed procedure provides a mechanism for determining the expected accuracy of test results obtained from facilities which were not previously cross calibrated. Furthermore, the method can be used to assist in making cost-effective management decisions on the level of validation/cross calibration necessary when bringing a test facility on line.
CURRENT
2017-06-20
Standard
AIR4844C
The following terminology has been generated by the ATA/IATA/SAE Commercial Aircraft Composite Repair Committee (CACRC) and provides terminology for design, fabrication, and repair of composite and bonded metal structures.
CURRENT
2011-06-03
Standard
ARIR663-1
ARINC Report 663 focuses on the many aspects related to component technical data and documentation including a common understanding of levels one - three maintenance (test, repair, re-certification). This includes defining the extent and format of OEM documentation to be delivered to the airline customers to support both the decision and technical requirements to accomplish level three maintenance; establishing minimum data requirements to support the airlines' decision relative to the accomplishment of level three maintenance (test solution, type of repair process, projected MTBF, modification potential, unit cost, alternative repairs, etc.); and identifying the minimum technical data requirements to support level three maintenance in airline shops for future avionics components (test, documentation).
CURRENT
2017-06-26
Standard
ARIR675
The purpose of this document is to establish guidance for Aircraft Support Data Management (ASDM). This guidance is intended for operators (e.g., pilot-in-command, maintenance activities, renter-pilot, or air carrier certificate holder) of transport aircraft.
CURRENT
2002-08-30
Standard
ARIS424-16
THE CURRENT VERSION OF THIS DOCUMENT IS 424-21. THIS PREVIOUS VERSION IS AVAILABLE FOR YOUR CONVENIENCE. This standard provides a data base comprising standards used for the preparation of a navigation system data base. This data may be used with the operational flight software in a wide range of navigational equipment.
CURRENT
2004-08-31
Standard
ARIS424-17
THE CURRENT VERSION OF THIS DOCUMENT IS 424-21. THIS PREVIOUS VERSION IS AVAILABLE FOR YOUR CONVENIENCE. This standard provides a data base comprising standards used for the preparation of a navigation system data base. This data may be used with the operational flight software in a wide range of navigational equipment.
CURRENT
2005-11-23
Standard
ARIS424-18
THE CURRENT VERSION OF THIS DOCUMENT IS 424-21. THIS PREVIOUS VERSION IS AVAILABLE FOR YOUR CONVENIENCE. This standard provides a data base comprising standards used for the preparation of a navigation system data base. This data may be used with the operational flight software in a wide range of navigational equipment.
CURRENT
2009-07-14
Standard
ARIS647A-1
This specification is an international standard defining the content and format of electronic files which document Flight Data Recording systems. The FRED specification is an expansion of the Flight Recorder Configuration Standard (FRCS) and is intended to provide guidelines for software systems designers and developers of ground support equipment for flight data recorders. The FRED specification has been developed to facilitate the exchange of Flight Data Recorder (FDR) documentation between aircraft manufacturers, operators, and government agencies. This specification addresses the ARINC Specification 664: Part 7, Avionics Full Duplex Switched Ethernet in numerous sections.
CURRENT
2009-07-01
Standard
ARIS647A-1ERR1
This specification is an international standard defining the content and format of electronic files which document Flight Data Recording systems. The FRED specification is an expansion of the Flight Recorder Configuration Standard (FRCS) and is intended to provide guidelines for software systems designers and developers of ground support equipment for flight data recorders. The FRED specification has been developed to facilitate the exchange of Flight Data Recorder (FDR) documentation between aircraft manufacturers, operators, and government agencies. This specification addresses the ARINC Specification 664: Part 7, Avionics Full Duplex Switched Ethernet in numerous sections.
CURRENT
1981-09-10
Standard
ARIC729-1
This standard sets forth the characteristics of an ADDCS designed for installation in commercial transport aircraft. The ADDCS is intended to process, convert and multiplex analog and discrete signals in order to provide them in digital format described in ARINC 429.
CURRENT
1986-12-18
Standard
ARIR612
The purpose of this standard is to provide a source of definitions of terms and acronyms commonly used in the air transport maintenance community for test and evaluation with an emphasis on terms applicable to BITE.
CURRENT
1998-01-04
Standard
ARIR613
In 1986 the airlines selected Ada as the high-order development language for avionics. ARINC 613 describes the Ada domain most suited for avionics software development. The standard provides valuable guidance to Ada compiler developers and Ada programmers.
CURRENT
2010-04-07
Standard
ARIR443
The purpose of this report is to illustrate to airfield and airport authorities the need for timely, accurate information regarding actual or planned changes to the physical airfield, recognize the changes in regulatory requirements in flight training, specifically visual database elements used in simulation, identify critical data elements for designing visual databases, and describe the elements and their uses in a simulated training environment. The list and descriptions of required visual database data elements will provide guidance to airfield and airport authorities and suppliers of data regarding minimum levels of data required to accurately create and maintain a visual representation of an airfield or other aircraft operating area. The report will also be used to provide information from airfield operators and managers concerning physical changes or additions to runways, taxiways, land-side gates, and the surrounding area.
CURRENT
2017-11-29
Standard
ARIR605
This guide has been written as an applications manual for writing avionics test specifications that conform to ARINC Specification 616. It provides advice for converting ATLAS test specifications into ATLAS test programs and implementing them on Automatic Test Equipment (ATE).This guide has been written as an applications manual for writing avionics test specifications that conform to ARINC Specification 616. It provides advice for converting ATLAS test specifications into ATLAS test programs and implementing them on Automatic Test Equipment (ATE).
CURRENT
2016-01-26
Standard
ARIR446
The intent of this standard is to provide guidance so the documentation provided with the Flight Simulation Training Device (FSTD) reflects and describes the delivered FSTD, including the description and definition of third party equipment and content. In the context of documentation guidance found in this report, the term FSTD is meant to include all levels of flight simulation devices. The documentation described herein is required for the operator to independently support the FSTD in the maintenance, operation, and update of the device throughout the lifetime of the device. This report describes a superset of a possible range of documentation involved in the initial delivery or an update of a FSTD. The deliverable documentation set for a particular FSTD may vary depending on the level of device (e.g., flat panel trainer versus a full flight simulator) as well as issues related to intellectual property, export compliance, technical requirements, and/or contractual agreements.
CURRENT
1984-11-05
Standard
ARIR419-3
This standard describes the technical characteristics of several digital transmission systems widely used in first-generation digital avionics. These digital transmission systems have been specified for inter-unit and inter-systems communications on board transport aircraft.
CURRENT
2016-07-06
Standard
ARIR422-1
This standard provides guidance to the maintenance community for identifying the modification status of avionics components and for preparing avionics service bulletins. This standard coordinates various methods used by airframe manufacturers and operators, for marking or identifying avionics that has been modified.
CURRENT
1961-06-01
Standard
ARIR407-1
The Synchro System Manual provides valuable information to designers and maintainers of avionics equipment that employ synchro devices. Synchro theory, synchro applications and signal definitions are included in this standard. Originally published in 1950, it is considered to be the classic guide for synchro devices. The Synchro System Manual provides valuable information to designers and maintainers of avionics equipment that employ synchro devices. Synchro theory, synchro applications and signal definitions are included in this standard. Originally published in 1950, it is considered to be the classic guide for synchro devices. The Synchro System Manual provides valuable information to designers and maintainers of avionics equipment that employ synchro devices. Synchro theory, synchro applications and signal definitions are included in this standard. Originally published in 1950, it is considered to be the classic guide for synchro devices.
CURRENT
2010-09-20
Standard
ARIR436-1
The purpose of ARINC Report 436 is to provide Flight Simulation Training Device (FSTD) users, suppliers and regulatory authorities a set of guidelines for Electronic Qualification Test Guide (eQTG) systems. This document is intended to be supplementary to existing regulatory authority requirements. This document is not designed to direct the use of certain technologies or platforms, but to outline the minimum requirements of an eQTG system. The choice of the technology used to meet these requirements is left to the system's designers and users.
CURRENT
2010-09-20
Standard
ARIR431
This is a final Report of the Avionics Maintenance Conference (AMC) Task Group 116 which was formed to discover the causes of "No Fault Found" in avionics equipment during test. This standard identifies sources of this problem and provides recommendations for its improvement.
HISTORICAL
2012-09-24
Standard
ARP5283A
The purpose of this specification is to provide airplane operators and tow vehicle manufacturers with: General design and operating requirements pertinent to test and evaluation of towbarless tow vehicles. Specific design requirements are provided in ARP4852 and ARP4853. Test and evaluation requirements. The results of these test evaluations will determine if the loads induced by the tow vehicle will exceed the design loads of the nose gear, or are within the aircraft manufacturer’s limits so that they do not affect the certified safe limit of the nose gear. The results of these test evaluations will also determine if a stability problem may occur during pushback and/or maintenance towing operations with the tested airplane/tow vehicle combination. This document specifies general test requirements and a test evaluation procedure for towbarless tow vehicles (TLTV) intended for pushback and maintenance towing only.
CURRENT
2012-08-16
Standard
ARP5284B
To list the documentation required to ensure inspection, maintenance and calibration of the TLTV's aircraft NLG steering and tractive protection systems or alerting devices can be carried out in accordance with the requirements of this document and the referenced standards.
HISTORICAL
2005-02-16
Standard
ARP5533
This SAE Aerospace Recommended Practice (ARP) covers the requirements for a Stationary Runway Weather Information System (referred to as the system) to monitor the surface conditions of airfield operational areas to ensure safer ground operations of aircraft. The system provides (1) temperature and condition information of runway, taxiway, and ramp pavements and (2) atmospheric weather conditions that assist airport personnel to maintain safer and more efficient airport operations. The system can be either a wired system or a wireless system.
CURRENT
2015-09-07
Standard
ARP5533A
This SAE Aerospace Recommended Practice (ARP) covers the requirements for a Stationary Runway Weather Information System (referred to as the system) to monitor the surface conditions of airfield operational areas to ensure safer ground operations of aircraft. The system provides (1) temperature and condition information of runway, taxiway, and ramp pavements and (2) atmospheric weather conditions that assist airport personnel to maintain safer and more efficient airport operations. The system can be either a wired system or a wireless system.
CURRENT
2002-04-05
Standard
ARP5311
This SAE Aerospace Recommended Practice (ARP) defines all the relevant issues that affect the generation of an Interface Control Document for Mechanical Actuation Sub-Systems. It is intended to provide to all parties involved with the generation of Mechanical Actuation Sub-Systems, a definition of documentation, drawings, reports and design parameters required to assure a successful development of mechanical actuation sub-systems for Aerospace-Military and Commercial applications.
CURRENT
1996-11-01
Standard
ARP5089
This document provides background information on the design, application, repair and inspection of composite structures, including metal bonding, used on civil transport aircraft. The objective of this document is to assist inspectors to know where to expect composite and metal bonded parts on the aircraft, to understand the capabilities of current NDT methods and to aid interpretation of inspection results. This document does not contain inspection procedures. It is intended to be informative and should not be used singularly, that is, it does not override any instructions that may be issued within a manufacturer's or operator's published documentation.
CURRENT
2014-12-18
Standard
ARP210A
"Hot Day ", "Tropical Day ", "Standard Day ", "Polar Day " and "Cold Day " are part of the lexicon of the aircraft industry. These terms are generally understood to refer to specific, generally accepted characteristics of atmospheric temperature versus pressure altitude. There are also other, less well-known days, defined by their frequency of occurrence, such as "1% Hot Day ", "10% Cold Day ", or "Highest Recorded Day ". These temperature characteristics have their origins in multiple sources, including U.S. military specifications which are no longer in force.
CURRENT
2017-07-18
Standard
ARP4386D
This SAE Aerospace Recommended Practice (ARP) provides the technical terms and nomenclature, together with their definitions and abbreviations/acronyms that are used in aerospace fluid power, actuation and control systems. NOTE: ARP490 and ARP4493 are sources for definitions specifically for electrohydraulic servovalves.
CURRENT
2012-09-25
Standard
ARP4714A
This paper presents guidelines for development of a procedure for external software loading of an electronic engine control (EEC) for a commercial application, on-wing or in a qualified service shop. This paper makes the following assumptions: The EEC is designed to accept external software loading. The EEC is certified as part of an engine. The support equipment is qualified in accordance with procedures set forth by the engine (and aircraft, if necessary) certifying authority if the EEC cannot detect an integrity violation of the loaded program. The software to be loaded has been approved by the engine and aircraft certifying authorities. One or more configurations of EEC hardware has been identified for each version of software which is to be loaded in the EEC. It is appropriate to use these guidelines in the initial development phase, although the certification issues would not be applicable.
CURRENT
2002-04-01
Standard
AIR5784
There has been a recent upsurge in interest from the media concerning the quality of the environment within aircraft cabins and cockpits especially in the commercial world1-4. This has included (although by no means been limited to) the air quality, with particular reference to the alleged effects of contamination from the aircraft turbine lubricant. Possible exposure to ‘organophosphates’ (OPs) from the oil has raised special concerns from cabin crew. Such is the concern that government organisations around the world, including Australia, USA and UK, have set up committees to investigate the cabin air quality issue. Concern was also voiced in the aviation lubricants world at the way in which OP additives in turbine lubricants were being blamed in some reports for the symptoms being experienced by air crew and passengers. SAE Committee E-34 therefore decided that it should gather as much available information on the subject as possible.
Viewing 1 to 30 of 682

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