Search Results

Standard

Combination Tail and Floodlamp for Industrial Equipment

2003-05-15

CURRENT

J94_200305

This SAE Standard provides performance and general design requirements and related test procedures for a combination tail and floodlamp for use on industrial wheeled equipment that may be operated on public roads.

Standard

TOLERANCES, METRIC Aluminum Alloy Drawn Tubing

1994-09-01

MAM2203B

Standard

TOLERANCES, METRIC Aluminum Alloy Drawn Tubing

1994-04-01

MAM2203A

This specification covers established metric manufacturing tolerances applicable to aluminum alloy drawn tubing ordered to metric dimensions. These tolerances apply to all conditions, unless otherwise noted. The term "excl" applies only to the higher figure of the specified range.

Standard

TOLERANCES, METRIC Aluminum Alloy Drawn Tubing

2002-07-23

MAM2203

This specification covers established metric manufacturing tolerances applicable to aluminum alloy drawn tubing ordered to metric dimensions. These tolerances apply to all conditions, unless otherwise noted. The term "excl" applies only to the higher figure of the specified range.

Standard

CABIN CONNECTORS AND CABLES PART 2 SPECIFICATION OF CONNECTORS, CONTACTS, AND BACKSHELLS

2018-11-28

CURRENT

ARINC800P2-1

This specification describes the general connectors, contacts, and backshells in their shape and characteristic for cabin systems for commercial aircrafts. ARINC 600, ARINC 404, and ARINC 801 connector specifications are published as independent standards.

Standard

CABIN CONNECTORS AND CABLES PART 2 SPECIFICATION OF CONNECTORS, CONTACTS, AND BACKSHELLS

2021-09-09

CURRENT

ARINC800P2-2

This specification describes the general connectors, contacts, and backshells in their shape and characteristic for cabin systems for commercial aircrafts. ARINC 600, ARINC 404, and ARINC 801 connector specifications are published as independent standards.

Standard

Manufacturing Message Specification – Service Definition and Protocol

2016-06-28

CURRENT

EIA511

The Manufacturing Message Specification is an application layer Standard designed to support messaging communications to and from programmable devices in a Computer Integrated Manufacturing (CIM) environment. This environment is referred to in this Standard as the manufacturing environment. This Standard does not specify a complete set of services for remote programming of devices, although provision of such a set of services may be the subject of future standardization efforts.

Standard

CABIN CONNECTORS AND CABLES, PART 4, STANDARD TEST METHODOLOGY

2020-07-13

CURRENT

ARINC800P4-1

ARINC 800 is the first industry standard intended for characterization of aviation-grade high-speed (Gbps) Ethernet links. The test methods are based on realistic representation of cabin networks. The notional cabling architecture is based on IFE seat distribution using multiple intermediate disconnects. Sequential testing is supported by building up number of connectors in the link. Test guidelines for mixed intermediate cable lengths are provided.

Standard

Procedure for the Continuous Sampling and Measurement of Non-Volatile Particle Emissions from Aircraft Turbine Engines

2013-11-18

HISTORICAL

AIR6241

This SAE Aerospace Information Report (AIR) describes procedures, required continuous sampling conditions, and instrumentation for the measurement of non-volatile particle number and mass concentrations from the exhaust of aircraft gas turbine engines. Procedures are included to calculate sampling loss performance. This AIR is not intended for in-flight testing, nor does it apply to engine operating in the afterburning mode.

Standard

Farm Equipment Two Conductor Breakaway Connector Cable

1977-01-30

CURRENT

J724_197701

Standard

Training Program Guidelines for Deicing/Anti-Icing of Aircraft on Ground

2014-08-05

HISTORICAL

ARP5149BDA

This document establishes the minimum criteria for effective training of air carrier and contractor personnel to deice/anti-ice aircraft to ensure the safe operation of aircraft during ground icing conditions. Appendix D specifies guidelines for particular airplane models.

Standard

Validation Methods For MIL-STD-1760D Mission Stores

2014-09-29

CURRENT

AS42701

This document establishes techniques for validating that a mission store complies with the interface requirements contained in MIL-STD-1760 Revision D.

Standard

Megawatt Charging System for Electric Vehicles

2021-12-15

WIP

J3271

This document describes the megawatt-level DC charging system requirements for couplers/inlets, cables, cooling, communication and interoperability. The intended application is for commercial vehicles with larger battery packs requiring higher charging rates for moderate dwell time. A simplified analog safety signaling approach is used for connection-detection to guarantee de-energized state for unmated couplers with superimposed high speed data for EVSE-EV charging control and other value added services.

Standard

Constant Speed Aerodynamic Procedure for Heavy Vehicles

2017-09-25

WIP

J3156

Develop and document an aerodynamic constant speed procedure for heavy vehicles that can accurately calculate the aerodynamic performance through the typical expected yaw angles during operation at highway speeds.

Standard

Considerations for future more electric aircraft electric power systems

2011-05-06

WIP

AIR6198

This activity is focused on more electric and all electric type power systems for air vehicles. The scope of which includes source, distribution and user contributions to electrical power quality, failure modes, coordination, system reliabilty and robustness, impacts of being flight critical and the gaps which exist in present standards and guidance documents.

Standard

Recommendations and Background Material for Battery Package Testing

2020-11-04

WIP

AIR6840

AS 6413 and slash sheets /1 & /2 hold the main information for testing of battery packaging. This document holds further information and expansion of philosophy, clarification etc. surrounding the testing and industry needs.

Standard

FZG Test Review

2017-02-28

WIP

AIR6919

Over the past several years the FZG A/8.3/90 test method has been used to evaluate current qualified aviation lubricants. The results of the effort have been summarized in this document as a historical reference to document the findings made from the committee.

Standard

Digital Avionics Fiber Optic Transmitters, Receivers and Transceivers for Aerospace Applications

2022-04-05

WIP

AIR7057

This information report is useful for personnel involved in the design, manufacturing, and/or use of digital fiber optic transmitters, receivers, and transceivers for aerospace applications

Standard

Fiber Optics and Applied Photonics Definitions

2020-01-30

WIP

AIR7366

A single depository for fiber optic and applied photonic definitions.

Standard

Engine Control Systems Interdependencies

2021-01-08

WIP

AIR6993

This SAE Aerospace Information Report (AIR) provides technical information regarding Engine Control Systems Interdependencies strategies and/or functions. This concerns aircraft with multiple power sources: at least two engines, whatever the nature of the power source is (electrical motor or gas turbine engine). Within this document the aircraft stands for fixed-wing aircraft as well as rotorcraft. The term EECS or FADEC is used for the engine electronic control system, whereas the term EEC is used for the electronic unit itself. The scope includes civilian aircraft powered by turbofan, turboprop, turboshaft and electrical engines equipped with electronic engine controls. Military aircraft is taken into consideration, however restricted topics that change the operational behaviors are not discussed.