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This specification covers an irradiated, thermally-stabilized, modified polyolefin plastic in the form of a thin-wall, heat-shrinkable tubing with a low recovery temperature
This specification covers epoxy-resin-impregnated glass fabric laminates in the form of sheet clad on one or both sides with electrolytically-deposited copper foil
This specification covers a non-crosslinked polyvinyl chloride plastic in the form of flexible, thinwall, heat-shrinkable tubing with a low recovery temperature
This specification covers the requirements for equipment, materials and procedures to be used in anodic treatments for magnesium base alloys for the purpose of increasing their corrosion resistance or producing surfaces suitable for the application of a protective organic finish
This specification covers flexible extruded, vinyl plastic tubing
This specification covers beryllium in the form of bars, rods, tubing, and machined shapes fabricated from vacuum hot pressed powder
This specification defines the procedures and requirements for joining metals and alloys using the electron-beam (EB) welding process
This specification defines the procedures and requirements for joining metals and alloys using the electron beam welding process
The GNSS sensor standard integrates Global Positioning System/Global Orbiting Navigation Satellite System (GLONASS) sensors. The sensor provides position information for display to pilots, and data to other navigation systems on the airplane
This specification, in conjunction with the general requirements for steel heat treatment covered in AMS2759, establishes the requirements and procedures for three classes of gas, vacuum, liquid, and low pressure (LPC) carburizing and related heat treatment of parts fabricated from carburizing grade steels. Parts made from steels other than those specified in the detail specifications may be heat treated in accordance with the applicable requirements using processing temperatures, times, and other parameters recommended by the material producer unless otherwise specified by the purchaser. This specification does not cover pack carburizing
This specification covers extruded polytetrafluoroethylene (PTFE) in the form of flexible tubing
The requirements for acquiring the sleeving described herein shall consist of this specification sheet and the issue of the following specification listed in that issue of the Department of Defense Index of Specifications and Standards (DODISS) specified in the solicitation: MIL-DTL-23053
This specification covers procedures for ultrasonic inspection of thin wall metal tubing of titanium, titanium alloy, and corrosion- and heat-resistant steels and alloys having nominal OD over 0.1875 inch (4.762 mm) with OD to wall thickness ratio of 8 or greater and wall thickness variation not exceeding ±10% of nominal
This procedure covers ultrasonic inspection of tubular, centrifugally-cast, corrosion-resistant steel cylinders
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
This document is intended to supplement the SAE J1939 documents by offering the SAE J1939 information in a form that can be sorted and search for easier use
This document provides general and specific design guidance for the development of software data loading equipment for all types of aircraft. The primary purpose of data load is to upload loadable software parts to airborne computers. A secondary function of data load is downloading data from airborne computers. Software data load functionality generally falls into the following categories: Portable Data Loader (PDL) for loading equipment on the ground or carried onto aircraft to perform onboard loading. Airborne Data Loader (ADL) for installation on aircraft to perform onboard loading. Data Load Function (DLF) is software that performs the data loading. This document defines data loaders designed to load avionics equipment over a high-speed interface using an Ethernet network protocol. This document defines media interfaces and protocol requirements specific to all data load functions, whether portable or airborne. This document also describes the desired capabilities of data loading
This specification covers manufacturing tolerances applicable to seamless and welded tubing of corrosion and heat-resistant steel. These tolerances apply to all conditions and are based on individual measurements, unless otherwise noted. Tubing may be specified by two dimensions only (OD and wall thickness, ID and wall thickness, or OD and ID
This specification establishes process controls for the repeatable production of preforms/parts using the laser directed energy deposition (L-DED-) process for additive manufacturing. Preforms are intended to be used to manufacture aerospace parts, but usage is not limited to such applications. Feedstock may be either wire (for L-DED-Wire) or powder (for L-DED-Powder
This specification covers pasted-mica electrical insulation for molded armature slot bases, commutator insulation, shells, heating elements, and other similar insulating purposes
This specification and its supplementary detail specifications cover a woven nylon cloth coated with polyether (EU) urethane
This specification covers electrical connections made with single, solid, round copper or copper alloy wire wrapped around copper alloy terminals without the use of solder
This specification covers a thermally-stabilized, irradiated, modified fluoropolymer in the form of very-thin-wall tubing
This specification covers an irradiated, thermally-stabilized, flame-resistant, modified silicone rubber in the form of heat shrinkable tubing
This specification covers an irradiated, thermally-stabilized, flame-resistant, modified-polyvinylidene-fluoride plastic in the form of extra-thin-wall tubing
Scope is unavailable
This specification covers an irradiated, thermally-stabilized, modified polyolefin plastic in the form of thin-wall, heat-shrinkable tubing with a low recovery temperature
This specification covers polytetrafluoroethylene-impregnated glass laminates in the form of sheet clad on one or both sides with electrolytically deposited copper foil
This specification covers extruded polytetrafluoroethylene (PTFE) in the form of flexible tubing
This specification covers procedures for ultrasonic immersion inspection of premium grade wrought titanium and titanium alloy forgings. Premium grade is a term used to describe titanium alloys used for critical rotating components in turbine engines. For details, see SAE AMS2380, the specification that covers the procedures for approval of products of premium-quality titanium alloys and the controls to be exercised in producing such products
This specification covers one type of high-contrast, fine-grain radiographic film in the form of cut sheets or rolls
This document defines an ILS/MLS/GLS multi-mode receiver that provides the flight path deviation guidance to the aircraft during the final approach and landing phase. The data sources may be Instrument Landing System (ILS), Microwave Landing System (MLS) or GNSS Landing System (GLS). Supplement 4 adds ILS look-alike data (ARINC 429) in support of GLS CAT II/III operation. It also defines Final Approach Segment Data Messages (FASDM) input labels to the MMR for new aircraft
This specification covers extruded polytetrafluoroethylene (PTFE) in the form of flexible tubing
This specification covers a crosslinked polyvinyl chloride plastic in the form of flexible, thin-wall, heat-shrinkable tubing
This specification covers pyrometric requirements for equipment used for the thermal processing of metallic materials. Specifically, it covers temperature sensors, instrumentation, thermal processing equipment, correction factors and instrument offsets, system accuracy tests, and temperature uniformity surveys. These are necessary to ensure that parts or raw materials are heat treated in accordance with the applicable specification(s
The complete requirements for procuring the product shall consist of this document and the latest issue of the basic specification, AMS2431
This document defines general practices for testing the physical layer of a fiber optic cable system. It is the intention of this document to outline proven practices for engineers and technicians engaged in testing and supporting fiber optic cable systems in aircraft
ARINC Specification 802 defines standard fiber optic cable meeting the operational and environmental requirements for the air transport industry. The purpose of this document is to avoid the proliferation of different designs of cables serving the same functions on different airplane models. ARINC Specification 802 comprises three sections. Section 1 provides a general description of the objectives, scope, the types of cable, and the applicable environmental categories. Section 2 addresses the desired physical properties of the fiber optic cables. Section 3 defines the qualification tests that may be used to ensure the cables meet the characteristics provided by this document. A glossary is provided in Appendix A
This standard provides guidance to those who develop avionics test programs and the source documentation on which they are based. This includes guidelines for all steps and phases within the TPS life cycle
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