Information Reports - SAE Mobilus

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IAQG-03282025-1 IAQG-03282025-1 (Current)04/02/2025
IAQG-03282025-1
IAQG-1 Standards Committee
test info reportjmsinforeport2172502/17/2025
test
Aviation Maintenance Committee
Test 01 on 15-01-2025AIR2025011501 (Current)01/28/2025
Test 01 on 15-01-2025
A-20C Interior Lighting
TightGV6677_202501 (Current)01/17/2025
Scoop
Agricultural Tractor Standards Committee (ATSC)
Test TitleGV44556 (Historical)01/09/2025
Test Scope
Agricultural Tractor Standards Committee (ATSC)
TitleAIRS12242024 (Current)12/24/2024
SS
A-20A Crew Station Lighting
Arinc Automation Document - Standard Information Report - PageCount 101 - 150KJH005 (Current)12/19/2024
Arinc Automation Document - Standard Information Report - PageCount 101 - 150
Flight Simulator Engineering and Maintenance Committee
Arinc Automation Document - Standard Information Report - PageCount 151 - 209 KJH006 (Current)12/19/2024
Arinc Automation Document - Standard Information Report - PageCount 151 - 209
Aviation Maintenance Committee
TightAIR12122024A (Current)12/12/2024
New Scoop
A-6 Aerospace Actuation, Control and Fluid Power Systems
TightAIR12122024 (Historical)12/12/2024
Scoop
A-6 Aerospace Actuation, Control and Fluid Power Systems
TTAIR12092024 (Current)12/09/2024
SS
A-6 Aerospace Actuation, Control and Fluid Power Systems
Demo Title 12/3/2024AIR12032024 (Current)12/03/2024
Demo Scope 12/3/2024
A-6 Aerospace Actuation, Control and Fluid Power Systems
Automation Title for Group Code D23PC-Auto-1715022264466 (Current)05/06/2024
Automation Abstract for Group Code D23
Automation Title for Group Code D23PC-Auto-1713447365379 (Current)04/18/2024
Automation Abstract for Group Code D23
Flight Simulator Engineering and Maintenance Committee
An eleventh one for CUR-1174PC11-CUR-1174 (Current)04/02/2024
Italic
Flight Simulator Engineering and Maintenance Committee
A sixth one for CUR-1174PC6-CUR-1174 (Current)03/26/2024
N/A
TEST - Designing for Long Life with ElastomersAIR1412E-CSP (Historical)02/23/2024
This document lists those guidelines recognized as being essential for consideration by the designer who is preparing to select an elastomer as part of an aerospace design.
Airlines Electronic Engineering Committee
LONG-TERM STORAGE RELIABILITY OF HIGH PRESSURE GAS CONTAINERS FOR PNEUMATIC ACTUATION SYSTEMSAIR4725 (Current)04/06/2023
This SAE Aerospace Information Report (AIR) provides design data reliability information relative to the long-term storage of gas containers or pressure vessels charged with nitrogen or helium at pressures ranging from 6000 to 12 000 psi. The gas containers are cylindrical, spherical, or toroidal in shape. Internal volumes range up to 1385 in3. Applications for this type cold gas actuation system include tactical missiles, guided projectiles, and smart bombs. A typical system is described.
A-6A2 Military Aircraft Committee
HANDBOOK OF HYDRAULIC METRIC CALCULATIONSAIR1657 (Current)04/05/2023
SI and other metric units related to aerospace hydraulics are summarized. Conversion of English units is provided as required. Fundamental fluid properties and physical laws governing fluid motion and pressure are described in SI units. Examples of application to typical aerospace hydraulic system components are worked out. Thermodynamic processes are excluded from the scope of this report.
A-6A2 Military Aircraft Committee
Cadmium Plate Cyclic Corrosion Test . AIR6130A (Current)01/25/2023
14-day material test to determine the cyclic effects of runway deicing compounds on cadmium plated parts.
null, null
682 Guidance for Air Transport Service Bulletins (TEST POPST CT and APPSEARCH)ARINC682 (Current)09/21/2022
This document provides industry guidance to supplement ATA standards and airframe requirements, addressing gaps and vague areas to move suppliers/vendors and airframers toward a common standard for format and wording in Vendor Service Bulletins (VSB) for Air Transport components. This document supplements the VSB guidance of iSpec 2200, providing clarity of requirements and resulting in a common standard wording and format of VSBs from all suppliers on all aircraft types. The guidance in this document is intended to be applied to VSBs created and released subsequent to the release of the guidance document and will not require the retroactive update of VSBs released prior to the creation and release of the guidance.
842-3 Guidance for Usage of Digital CertificatesARINC842-3 (Current)07/01/2022
The purpose of this document is to provide operational guidance for key life-cycle management, which refers to the phases through which digital certificates and associated cryptographic keys progress, from creation through usage to retirement. Additionally, this document provides implementation guidance for online certificate provisioning of aircraft systems. The scope includes both the onboard part (aircraft system) as well as the ground part (PKI provider and Ground Infrastructure). Consideration of both onboard and ground provides the benefit of security considerations being included in the process flow and chain of custody. Specifically, the management to and from the aircraft is defined within a workflow. The guidance is based on open international standards that are adapted to the aviation environment, recognizing that a typical commercial airplane has a long lifespan, its operational environment is highly complex and regulated, and multiple stakeholders operate ground-based
Airlines Electronic Engineering Committee
Aerospace Fluid System Standards, Metric, National and InternationalAIR2000F (Current)03/25/2022
The purpose of this aerospace information report is to provide a listing of national and international metric standards for use in aerospace fluid systems with their equivalent SAE inch, International ISO, and European AECMA standards.
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Aerospace Fluid System Standards, Metric, National and InternationalAIR2000F-TEST-REC (Historical)03/25/2022
The purpose of this aerospace information report is to provide a listing of national and international metric standards for use in aerospace fluid systems with their equivalent SAE inch, International ISO, and European AECMA standards.
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
679 Aircraft Server, Communications, and Interface StandardARINC679 (Current)11/10/2021
ARINC Report 679 defines the functional characteristics of an airborne server that will support Electronic Flight Bags (EFBs) and similar peripherals used in the flight deck, cabin, and maintenance applications. The document defines how EFBs will efficiently, effectively, safely, and securely connect to the airborne server in a way that offer expanded capabilities to aircraft operators. The airborne server has two main functions, first to provide specific services to connected systems, and second to provide centralized security for the EFB and its data. This document is a functional airborne server definition. It does not define the physical characteristics of the server.
Airlines Electronic Engineering Committee
Calculations and Background Information Used to Specify the Dimensions in AS6235AIR7358 (Current)11/09/2021
This SAE Aerospace Information Report (AIR) contains a description of the design approach, the calculations, some comparisons to alternate SAE Aerospace Recommended Practice (ARP) documents, and the background information used to generate the standard face seal gland dimensions specified in AS6235. NOTE: This AIR should be read in conjunction with AS6235. In some instances, the information contained within AS6235 is repeated for clarity.
A-6C2 Seals Committee
Calculations and Background Information Used to Specify the Dimensions in AS6235AIR7358-TEST-REC (Historical)11/09/2021
This SAE Aerospace Information Report (AIR) contains a description of the design approach, the calculations, some comparisons to alternate SAE Aerospace Recommended Practice (ARP) documents, and the background information used to generate the standard face seal gland dimensions specified in AS6235. NOTE: This AIR should be read in conjunction with AS6235. In some instances, the information contained within AS6235 is repeated for clarity.
A-6C2 Seals Committee
Aircraft Turbine Fuel Contamination History and Endurance Test RequirementsAIR4023C (Current)11/01/2021
This document discusses the history and development of endurance requirements, provides an analysis of test contaminant material and includes a discussion of future requirements.
AE-5B Aircraft and Engine Fuel and Lubricant Sys Components
Rollover Testing MethodsJ2926_202110 (Current)10/29/2021
The scope of this document is to provide an overview of the techniques found in the published literature for rollover testing and rollover crashworthiness evaluation at the vehicle and component levels. It is not a comprehensive literature review, but rather illustrates the techniques that are in use or have been used to evaluate rollover crashworthiness-related issues.
Impact and Rollover Test Procedures Standards Committee
Requirements for Using Robotic Hot Solder Dip to Replace the Finish on Electronic Piece PartsGEIASTD0006C-TEST-REC (Historical)10/26/2021
This standard defines the requirements for fully replacing undesirable surface finishes using robotic hot solder dip. Requirements for qualifying and testing the refinished piece parts are also included. This standard covers the replacement of pure tin and Pb-free tin alloy finishes with SnPb finishes with the intent of subsequent assembly with SnPb solder. This dipping is different from dipping to within some distance of the body for the purposes of solderability; solder dipping for purposes other than full replacement of pure tin and Pb-free tin alloy finishes are beyond the scope of this document. It covers process and testing requirements for robotic dipping process and does not cover semi-automatic or purely manual dipping processes. This standard does not apply to piece-part manufacturers who build piece parts with a hot solder dip finish. It applies to refinishing performed by a robotic hot solder dip service supplier or production facilities at the customer, whenever the intent
G-24 Pb-free Risk Management Committee for ADHP
Requirements for Using Robotic Hot Solder Dip to Replace the Finish on Electronic Piece PartsGEIASTD0006C (Current)10/26/2021
This standard defines the requirements for fully replacing undesirable surface finishes using robotic hot solder dip. Requirements for qualifying and testing the refinished piece parts are also included. This standard covers the replacement of pure tin and Pb-free tin alloy finishes with SnPb finishes with the intent of subsequent assembly with SnPb solder. This dipping is different from dipping to within some distance of the body for the purposes of solderability; solder dipping for purposes other than full replacement of pure tin and Pb-free tin alloy finishes are beyond the scope of this document. It covers process and testing requirements for robotic dipping process and does not cover semi-automatic or purely manual dipping processes. This standard does not apply to piece-part manufacturers who build piece parts with a hot solder dip finish. It applies to refinishing performed by a robotic hot solder dip service supplier or production facilities at the customer, whenever the intent
G-24 Pb-free Risk Management Committee for ADHP
NOx Tracking Parameter AccuracyJ3349_202110 (Historical)10/19/2021
This SAE Information Report provides SAE’s recommendations for meeting the requirements for REAL NOx accuracy demonstration and for the implementation of REAL NOx binning requirements as defined in OBD regulations 13 CCR 1971.1 and 13 CCR 1968.2.
Vehicle E E System Diagnostic Standards Committee
NOx Tracking Parameter AccuracyJ3349_202110-TEST-REC (Historical)10/19/2021
This SAE Information Report provides SAE’s recommendations for meeting the requirements for REAL NOx accuracy demonstration and for the implementation of REAL NOx binning requirements as defined in OBD regulations 13 CCR 1971.1 and 13 CCR 1968.2.
Vehicle E E System Diagnostic Standards Committee
Vision GlossaryJ264_202110 (Current)10/15/2021
The function of uniform terminology is to promote understandable and exact communication in the area of vision. A great deal of effort has been expended to make these definitions suit this purpose. It is recognized that this terminology, like other dictionaries, must be revised periodically to reflect current usage and changing needs. The Driver Vision Subcommittee of the Human Factors Engineering Committee, therefore, solicits suggestions for improvements and additions to be considered in future revisions.
Driver Vision Standards Committee
Overview and History of Aircraft Inerting SystemsAIR1903A (Current)10/08/2021
An airplane fuel tank inerting system provides an inert atmosphere in a fuel tank to minimize explosive ignition of fuel vapor. This SAE Aerospace Information Report (AIR) deals with the three methods of fuel tank inerting systems currently used in operational aircraft: (1) on-board inert gas generation systems (OBIGGS), (2) liquid/gaseous nitrogen systems, and (3) halon systems. The OBIGGS and nitrogen systems generally are designed to provide full-time fuel tank fire protection; the halon systems generally are designed to provide only on-demand or combat-specific protection. This document also addresses other design considerations that affect fuel tank flammability such as fuel tank pressure and other methods for reducing fuel tank flammability. This AIR does not treat the subject of explosion suppression foam (ESF) that has been used for fuel tank explosion protection on some military aircraft. ESF is also available for retrofit for commercial airplanes. The primary disadvantages of
AE-5D Fuel Tank Flammability Reduction Systems Committee
Elastomer Compatibility Considerations Relative to Elastomer SelectionAIR786C (Current)10/01/2021
This SAE Aerospace Information Report (AIR) contains data relative to the chemical nature of aerospace fluids and relates each to its empirical effect upon elastomeric components. Since the compatibilities of elastomers are determined by the compounding as well as the nature of the base polymer, the elastomers considered are limited to finished compounds for which material or performance specifications can be referenced.
A-6C2 Seals Committee
Elastomer Compatibility Considerations Relative to Elastomer SelectionAIR786C-TEST-REC (Historical)10/01/2021
This SAE Aerospace Information Report (AIR) contains data relative to the chemical nature of aerospace fluids and relates each to its empirical effect upon elastomeric components. Since the compatibilities of elastomers are determined by the compounding as well as the nature of the base polymer, the elastomers considered are limited to finished compounds for which material or performance specifications can be referenced.
A-6C2 Seals Committee
115/200 Volt, 400 Hz Aircraft External Electrical Power Connector Contact Maintenance ProceduresAIR4365B (Current)09/30/2021
This SAE Aerospace Information Report (AIR) describes procedures for use in the field to determine if 115/200 Volt, 400 Hz aircraft external electrical power connectors are excessively worn, which may result in the inability of the external power plug to be retained, intermittent electrical performance and arcing.
AGE-3 Aircraft Ground Support Equipment Committee
Aircraft Engine Life Cycle Cost GuideAIR1939A (Current)09/10/2021
AIR 1939 addresses communication of LCC data between equipment suppliers, aircraft engine producers, aircraft manufacturers, and users, as illustrated in Figure 1. The LCC data categories addressed include: research, development, test and evaluation (RDT&E); acquisition (initial procurement and investment); and operating and support (O&S) costs. While input and output formats are suggested, calculation procedures and cost methodology are specifically excluded since many LCC models preferred by the industry are company sensitive or proprietary (Figure 1). The relationship of LCC input data to program phase is described. Ground rules and assumptions are addressed. A glossary of LCC terms is provided. The LCC impact of propulsion systems on other aircraft systems is considered. This document was specifically developed for military propulsion system cost analysis. However, it is believed that a functional relationship exists between military and commercial Life Cycle Cost analysis and that
LCLS Life Cycle Logistics Supportability
Oxygen Considerations for High Elevation Airport Operations (HEAO)AIR6829 (Current)08/26/2021
This document covers information concerning the use of oxygen when flying into and out of high elevation airports for both pressurized and non-pressurized aircraft. Oxygen requirements for pressurized aircraft operating at high altitudes have for decades emphasized the potential failures that could lead to a loss of cabin pressurization coupled with the potential severe hypoxic hazard that decompressions represent. This document is intended to address the case where the relationship between cabin and ambient pressures are complicated by operations at high terrestrial altitudes. Operators who fly into these high-altitude airports should address the issues related to this environment because it carries the potential for insidious hypoxia and other conditions which can affect safety. It provides information to consider in developing operational procedures to address hypoxia concerns consistent with regulatory mandates. In some sections, procedures are discussed that may mitigate the
A-10 Aircraft Oxygen Equipment Committee
Oxygen Considerations for High Elevation Airport Operations (HEAO)AIR6829-TEST-REC (Historical)08/26/2021
This document covers information concerning the use of oxygen when flying into and out of high elevation airports for both pressurized and non-pressurized aircraft. Oxygen requirements for pressurized aircraft operating at high altitudes have for decades emphasized the potential failures that could lead to a loss of cabin pressurization coupled with the potential severe hypoxic hazard that decompressions represent. This document is intended to address the case where the relationship between cabin and ambient pressures are complicated by operations at high terrestrial altitudes. Operators who fly into these high-altitude airports should address the issues related to this environment because it carries the potential for insidious hypoxia and other conditions which can affect safety. It provides information to consider in developing operational procedures to address hypoxia concerns consistent with regulatory mandates. In some sections, procedures are discussed that may mitigate the
A-10 Aircraft Oxygen Equipment Committee
Basic Aircraft Oxygen Systems DesignAIR825/14 (Current)08/11/2021
This slash document collects general reference material related to gaseous oxygen system flow requirements and sizing calculations. This document will assist oxygen system equipment designers and operators to establish systems and equipment requirements. The document consists of charts, tables, system schematics, system requirements, and sample calculations for system sizing.
A-10 Aircraft Oxygen Equipment Committee
Introduction to Oxygen Equipment for AircraftAIR825/1 (Current)08/11/2021
The purpose of this document is to give the reader an overview of the document package which makes up AIR825, Introduction to Oxygen Equipment for Aircraft, and a basic overview (see Section 4) of the operational concerns driven by human physiology during altitude exposure.
A-10 Aircraft Oxygen Equipment Committee
COMMON TERMINOLOGY AND FUNCTIONS FOR SOFTWARE DISTRIBUTION AND LOADINGARINC645-1 (Current)08/11/2021
This document provides airlines, airframe manufacturers, aircraft equipment suppliers, and others with information that is specific to data, software, and ground tools used in aviation configuration and data management. As a starting point, this document provides guidance on: Which standard to use in specific situations The use of and how integrity checks should be applied Common terminology in airborne software management Since airplanes started using software controlled hardware, there has been a need to standardize processes and terminology. This document is the centroid to which other software standards are related.
Airlines Electronic Engineering Committee
Gaseous Oxygen and Oxygen Equipment, IntroductoryAIR825/3 (Current)08/11/2021
This Aerospace Information Report provides a general discussion on gaseous breathing oxygen and oxygen equipment for use on commercial aircraft. Other types of oxygen systems are mentioned to assist in this discussion. For detailed information on systems other than gaseous, reference the appropriate section of AIR825.
A-10 Aircraft Oxygen Equipment Committee
Convenient Location of Oxygen Masks for Both the Crew and Passengers of AircraftAIR1390A (Historical)08/10/2021
There are four basic conditions requiring the dispensing of oxygen through oxygen masks to aircraft occupants in turbine powered aircraft during flight. The following conditions are derived from the Federal Aviation Regulations (FAR) as listed in Section 2.
A-10 Aircraft Oxygen Equipment Committee
Electrical and Electronic Equipment Cooling in Commercial TransportsAIR64C-TEST-REC (Historical)08/10/2021
This document considers the cooling of equipment installed in equipment centers, which usually consist of rack-mounted equipment and panel mounted equipment in the flight deck. Instances where these two locations result in different requirements are identified. This document generally refers to the cooled equipment as E/E equipment, denoting that both electrical and electronic equipment is considered, or as an E/E equipment line-replaceable-unit (LRU). The majority of cooled equipment takes the form of LRUs. The primary focus of this document is E/E equipment which uses forced air cooling to keep the equipment within acceptable environmental limits. These limits ensure the equipment operates reliably and within acceptable tolerances. Cooling may be supplied internally or externally to the E/E equipment case. Some E/E equipment is cooled solely by natural convection, conduction, and radiation to the surrounding environment. This document discusses specification requirements, system
AC-9 Aircraft Environmental Systems Committee
Electrical and Electronic Equipment Cooling in Commercial TransportsAIR64C (Current)08/10/2021
This document considers the cooling of equipment installed in equipment centers, which usually consist of rack-mounted equipment and panel mounted equipment in the flight deck. Instances where these two locations result in different requirements are identified. This document generally refers to the cooled equipment as E/E equipment, denoting that both electrical and electronic equipment is considered, or as an E/E equipment line-replaceable-unit (LRU). The majority of cooled equipment takes the form of LRUs. The primary focus of this document is E/E equipment which uses forced air cooling to keep the equipment within acceptable environmental limits. These limits ensure the equipment operates reliably and within acceptable tolerances. Cooling may be supplied internally or externally to the E/E equipment case. Some E/E equipment is cooled solely by natural convection, conduction, and radiation to the surrounding environment. This document discusses specification requirements, system
AC-9 Aircraft Environmental Systems Committee
Guide for Installation of Electrical Wire and Cable on Aircraft Landing GearAIR4004A (Current)08/09/2021
Recent field experience has indicated significant problems with some types of wire and cables as routed on aircraft landing gear. This SAE Aerospace Information Report (AIR) is intended to identify environmental concerns the designer should consider, materials that appear to be most suitable for use in these areas, routing, clamping, and other protection techniques that are appropriate in these applications. In recent years aircraft certification regulatory agencies introduced new regulations regarding Electrical Wiring Interconnection Systems (EWIS) to further enhance safety of the associated systems and aircraft overall.
A-5B Gears, Struts and Couplings Committee
Crashworthy Landing Gear DesignAIR4566A (Current)08/09/2021
The intent of this SAE Aerospace Information Report (AIR) is to document the design requirements and approaches for the crashworthy design of aircraft landing gear. This document covers the field of commercial and military airplanes and helicopters. This summary of crashworthy landing gear design requirements and approaches may be used as a reference for future aircraft.
A-5B Gears, Struts and Couplings Committee
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