Browse SAE Mobilus

Browse 40,000+ industry standards and 150,000+ peer-reviewed publications spread across journal articles, technical papers, books, SAE Edge™ Research Reports and other content categories on our industry leading platform SAE Mobilus®

Items (196,126)
Find
Test Document 314TESTMARCH14 (Current)
scope
G-41 Reliability
Technical Standard
11012024-new-air110124-new-air (Current)
11012024-new-air
A-6 Aerospace Actuation, Control and Fluid Power Systems
Technical Standard
Valve Guide Information ReportJ1682_201712 (Current)12/20/2017
This SAE Information Report provides: a Types of valve guides and their nomenclature b Valve guide alloy designations and their chemistries c Valve guide alloy metallurgy d Typical mechanical and physical properties of guide alloys e Typical dimensional tolerances of valve guides and their counterbores f Recommended interference fits g Installation procedures h Application considerations
Metals Technical Committee
Information Report
Lighting, Aircraft Exterior, Night Vision Imaging System (NVIS) CompatibleARP4392 (Current)05/20/2016
This SAE Aerospace Recommended Practice (ARP) describes the recommended performance levels for equipment located on the aircraft exterior which produces radiant energy which will provide desired information when viewed with NVIS goggles. These performance intensities, normally stated in candelas for visible light, are modified to consider the goggle spectral response range. Where necessary, location of the equipment on the airplane is specified. The spectral emission characteristics may or may not include visible light. Whether or not visible energy is emitted, this document will refer to these items of equipment as "lights".
A-20B Exterior Lighting Committee
Recommended Practice
IGNITER, SPARK, AERONAUTICAL ENGINE (LOW TENSION)AS803 (Current)05/01/1991
This specification establishes the qualification and acceptance limits for aeronautical engine low tension spark igniters.
E-30 Propulsion Ignition Systems Committee
Technical Standard
Automated Manufacture of Continuous Multi-Ply Carbon Fiber/Epoxy Resin Impregnated BroadgoodsARP1674A (Current)08/14/2014
This document describes a manufacturing method for processing unidirectional carbon fiber/epoxy resin impregnated sheet and tape into multi-ply broadgoods and tape produced on an automated cross-plying machine. Broadgoods or tape of two or more ply configurations may be processed, where ply orientations of 0°, 45°, 90°, and 135° (as examples) may be automatically layed in a programmed sequence. In all configurations, the 0° ply direction is parallel to the length of the broadgoods roll or sheet, or tape.
AMS P17 Polymer Matrix Composites Committee
Recommended Practice
Hose Assemblies, Installed, Visual Inspection Guide ForARP1658B (Current)10/07/2014
This SAE Aerospace Recommended Practice (ARP) covers visible surface defects on aerospace hose assemblies which have been installed and are functioning within a working environment at the time of visual inspection.
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Recommended Practice
Application of Direct Pressure to Resin in Curing of Epoxy and Addition Type PolyimidesARP1927 (Current)08/14/2014
This recommended practice describes the materials, related equipment, and particular processing techniques utilized in process science curing of composite hardware where pressure is imparted specifically to the resin of curing composites. Included as Appendix "A" to this ARP is a discussion of the particular techniques developed for a processing science philosophy which has consistently produced void and porosity-free, large area, thick composite structures.
AMS P17 Polymer Matrix Composites Committee
Recommended Practice
DESIGN OBJECTIVES FOR CRT DISPLAYS FOR PART 25 (TRANSPORT) AIRCRAFTARP1874 (Current)01/04/2008
This ARP covers CRT electronic display devices, both single color and multicolor, and is applicable to the following types of displays: Type I: Flight and Navigation Displays Type II: Engine, Systems and Warning Displays Type III: Control Displays
A-4ED Electronics Display Subcommittee
Recommended Practice
IAQG-03282025-1 IAQG-03282025-1 (Current)04/02/2025
IAQG-03282025-1
IAQG-1 Standards Committee
Information Report
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
Information Report
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
Information Report
Arinc Automation Document - - Characteristic - PageCount 45 – 100KJH004 (Current)12/19/2024
Arinc Automation Document - - Characteristic - PageCount 45 – 100
Aviation Maintenance Committee
Characteristic
Hose Assembly, Polytetrafluoroethylene, Metallic Braid Reinforced, 5080 psi (35,000 kPa), 400°F (204°C), Aircraft Hydraulic Systems (Supplement 1)..AS5960SUP1 (Current)09/24/2012
This supplement forms a part of the Aerospace Standard AS5960, Hose Assembly, Polytrafluoroethyloene, Metallic Braid Reinforced, 5080 psi (35,000 kPa), 400°F (204°C), Aircraft Hydraulic Systems, and shall be used to identify hose assembly standards citing this procurement specification.
null, null
Supplement
Loss Budget Specification for Fiber Optic Links . AS5750A (Current)02/22/2023
This document defines a quantified means of specifying a digital fiber optic link loss budget: Between end users and system integrators Between system integrators and subsystem suppliers Between subsystem suppliers and component vendors The standard specifies methods and the margin required for categories of links.
null, null
Technical Standard
AS6550 G.A. Flanged Half for 1 1/2" Re-Fuelling Coupling Self Sealing TypeAS6550-1 (Current)12/01/1955
No scope available.
Engine and Airframe Technical Standards Committee (TSC)
Technical Standard
AS6342 Cap Nut. (Rudder Bar)AS6342-1 (Current)11/19/1956
No scope available.
Engine and Airframe Technical Standards Committee (TSC)
Technical Standard
AS3296 Bolt - "Phillip's" Raised 120° C'SK HeadAS3296-7 (Current)07/01/1977
No scope available.
Engine and Airframe Technical Standards Committee (TSC)
Technical Standard
AS6337-6338 Pedal Pivot Bolt (Rudder Bar)AS6337-1 (Current)11/19/1956
No scope available.
Engine and Airframe Technical Standards Committee (TSC)
Technical Standard
AS8433 1/4 Bore Sediment Drain Valve, UnifiedAS8433-1 (Current)08/13/1968
No scope available.
Engine and Airframe Technical Standards Committee (TSC)
Technical Standard
AS46768 Nut, Self Locking, Miniature, Double Lug Floating Anchor, Cres. Steel, Silver Plated (125 000 lbf/in2) 425°CAS46768-1 (Current)08/01/1979
No scope available.
Engine and Airframe Technical Standards Committee (TSC)
Technical Standard
AS6339-6340 Assembly of Foot Pedal. (Rudder Bar)AS6339-1 (Current)11/19/1956
No scope available.
Engine and Airframe Technical Standards Committee (TSC)
Technical Standard
AS6711 Tee Union BodyAS6711-4 (Current)07/01/1975
No scope available.
Engine and Airframe Technical Standards Committee (TSC)
Technical Standard
485P2-5 Cabin Equipment Interfaces, Part 2, Physical Layer - In-Seat ProtocolARINC485P2-5 (Current)06/30/2020
ARINC Specification 485, Part 2 specifies the ARINC 485-control protocol used by the LRUs described in ARINC Specification 628 Part 2. This document defines a multi-drop bus. The point-to-point configuration is also supported. The point-to-point bus is treated simply as a multi-drop bus with only one drop. There is one master LRU and one or more slave LRUs present on the bus. However; multiple buses may be connected in parallel, where each parallel bus operates independently from each other.
Airlines Electronic Engineering Committee
Specification
579-2 Airborne VOR ReceiverARINC579-2 (Current)08/01/1989
This standard sets the basic requirements for a VOR receiver, whose function is to receive and process VOR signals in the frequency band 108.00 to 117.95 MHz. Provides traditional analog outputs and a digital output of omni bearing.
Airlines Electronic Engineering Committee
Characteristic
AS6726 Pipe Couplings (Unified Adaptor), Steel Banjo Bolt with Union Head ConnectionAS6726-4 (Current)11/19/1957
No scope available.
Engine and Airframe Technical Standards Committee (TSC)
Technical Standard
AS6729 Double R.A. Cone Banjo Body (3/16" to 1/2") for use with Banjo Bolts. A.S. 6721-6AS6729-5 (Current)04/01/1968
No scope available.
Engine and Airframe Technical Standards Committee (TSC)
Technical Standard
566A-9 Mark 3 VHF Communications TransceiverARINC566A-9 (Current)01/01/1998
This standard defines the characteristics of a VHF Communications Transceiver unit capable of providing voice or data communications capability with the ground. Supplement 8 introduces 8.33 kHz channel spacing.
Airlines Electronic Engineering Committee
Characteristic
AS6526 Spider Assembly R.H.AS6526-1 (Current)12/01/1955
No scope available.
Engine and Airframe Technical Standards Committee (TSC)
Technical Standard
AS6523 Outer Handle Assembly - Double Handle LockAS6523-1 (Current)12/01/1955
No scope available.
Engine and Airframe Technical Standards Committee (TSC)
Technical Standard
AS6521 Main Body - Right HandAS6521-1 (Current)12/01/1955
No scope available.
Engine and Airframe Technical Standards Committee (TSC)
Technical Standard
VHF DIGITAL LINK (VDL) MODE 2 IMPLEMENTATION PROVISIONSARINC631-7 (Current)07/10/2017
This document describes the functions to be performed by airborne and ground components of the VDLM2 to successfully transfer messages from VHF ground networks to avionics systems on aircraft and vice versa where the data are encoded in a code and byte independent format. The compatibility of VDLM2 with OSI is established by defining a set of services and protocols that are in accordance with the OSI basic reference model. The compatibility with the ATN protocols is achieved by defining a set of interfaces between the VDLM2 subnetwork protocol specification and the Mobile Subnetwork Dependent Convergence Function (MSNDCF). The SNDCF is defined in the ICAO ATN SARPs.
Airlines Electronic Engineering Committee
Technical Standard
DATALINK GROUND SYSTEM STANDARD AND INTERFACE SPECIFICATION (DGSS/IS)ARINC620-8 (Current)12/21/2014
This standard sets forth the desired interface characteristics of the data link service provider to the data link user. Provides data link users the information needed to develop applications and to encourage uniformity and standardization (to the extent possible) among various data link service providers. Contains general and specific guidance concerning the interfaces between the data link service providers and both the airborne and ground user.
Airlines Electronic Engineering Committee
Technical Standard
AS6520 Main Body - Left HandAS6520-1 (Current)12/01/1955
No scope available.
Engine and Airframe Technical Standards Committee (TSC)
Technical Standard
AS8652 Self-Locking Nuts, Double Lug Anchor. C.R. Steel, 125,000 lbf/in2 250°CAS8652-4 (Current)11/01/1973
No scope available.
Engine and Airframe Technical Standards Committee (TSC)
Technical Standard
AS44409-412 Washer, Spring Tension, MetricAS44409-2 (Current)03/01/1991
No scope available.
Engine and Airframe Technical Standards Committee (TSC)
Technical Standard
AS46737 Tee Assy - Nipple End, Male Nut Union (Steel)AS46737-1 (Current)07/01/1980
No scope available.
Engine and Airframe Technical Standards Committee (TSC)
Technical Standard
AS5419AR Amendment Record for Drawing Standard No. AS5419AS5419AR-8 (Current)06/01/2012
No scope available.
Engine and Airframe Technical Standards Committee (TSC)
Supplement
AS5910-5991 Chain (1/2" Pitch) and Fittings Assembly Code. Non-Reversible ControlAS5910-4 (Current)01/11/1952
No scope available.
Engine and Airframe Technical Standards Committee (TSC)
Technical Standard
AS3369 Filler Cap Base. With VentAS3369-4 (Current)05/11/1951
No scope available.
Engine and Airframe Technical Standards Committee (TSC)
Technical Standard
AS2824 Drum AssemblyAS2824-6 (Current)09/23/1946
No scope available.
Engine and Airframe Technical Standards Committee (TSC)
Technical Standard
AS4913-4920 Protection Covers for Flanges and DrivesAS4913-1 (Current)12/04/2015
No scope available.
Engine and Airframe Technical Standards Committee (TSC)
Technical Standard
AS44404-406 Elastomeric Grommets (Various). For Aeronautical PurposesAS44404-3 (Current)09/01/1975
No scope available.
Engine and Airframe Technical Standards Committee (TSC)
Technical Standard
CABIN COMMUNICATION SYSTEMS (CCS)ARINC746-6 (Current)11/19/2010
This document provides general and specific design guidance for the development, installation, and desired operational capability of Cabin Communications Systems, including satellite communications, air-to-ground communications, and gatelink. Supplement 6 incorporates guidance for protection of personal information using methods consistent with the Payment Card Industry (PCI) Data Security Standard (DSS). The CCS characteristic provides encryption approaches for payment card information and suggestions for key management.
Airlines Electronic Engineering Committee
Characteristic
AS43013 Ring, Sealing, Toroidal (O-Ring - Inch Series) for General Aerospace UseAS43013-5 (Current)08/28/2012
This drawing specifies parts AS43013-001, AS43013-002, AS43013-003, AS43013-004, AS43013-005, AS43013-006, AS43013-007, AS43013-008, AS43013-009, AS43013-010, AS43013-011, AS43013-012, AS43013-013, AS43013-014, AS43013-015, AS43013-016, AS43013-017, AS43013-018, AS43013-019, AS43013-020, AS43013-021, AS43013-022, AS43013-023, AS43013-024, and AS43013-025. To view suppliers qualified to manufacture this part, visit https://ts200.sae-itc.org/.
Engine and Airframe Technical Standards Committee (TSC)
Technical Standard
AS43013-AR Amendment Record for Drawing Standard No. AS43013AS43013AR-5 (Current)08/28/2012
No scope available.
Engine and Airframe Technical Standards Committee (TSC)
Supplement
AS43003-AR Amendment Record for Drawing Standard No. AS43003AS43003AR-4 (Current)08/28/2012
No scope available.
Engine and Airframe Technical Standards Committee (TSC)
Supplement
AS43003 Ring, Sealing, Toroidal (O-Ring - Inch Series) for use with Tapped Port Bosses to SAE AS5202AS43003-4 (Current)08/28/2012
This drawing specifies parts 6AS43003-914, AS43003-901, AS43003-902, AS43003-903, AS43003-904, AS43003-905, AS43003-906, AS43003-907, AS43003-908, AS43003-909, AS43003-910, AS43003-911, AS43003-912, AS43003-914, AS43003-918, AS43003-920, AS43003-924, AS43003-928, and AS43003-932. To view suppliers qualified to manufacture this part, visit https://ts200.sae-itc.org/.
Engine and Airframe Technical Standards Committee (TSC)
Technical Standard
FULL-FORMAT PRINTERARINC744 (Current)12/30/1990
This standard sets forth the characteristics of a full-format printer capable of printing up to 132 characters of alphanumeric and/or semi-graphic data on 8.5 x 11 inch or A4 paper size. Participating equipment interface using ARINC 429 data buses. It is optionally capable of producing hard-copy graphics in the form of addressable dot plotting data.
Airlines Electronic Engineering Committee
Characteristic
AUTOMATIC DEPENDENT SURVEILLANCE (ADS)ARINC745-2 (Current)06/30/1993
This standard defines ADS system functions. It describes the ADS to ground-based application end-to-end operation. Includes a brief overview of the entire ADS system in order to aid the reader in understanding the ADS environment.
Airlines Electronic Engineering Committee
Characteristic
Items per page:
1 – 50 of 196126