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ARINC 858 Part 2 provides aviation ground system gateway considerations necessary to transition to the Internet Protocol Suite (IPS). ARINC 858 Part 2 describes the principles of operation for an IPS gateway that enables ACARS application messages to be exchanged between an IPS aircraft and a ground ACARS host. ARINC 858 Part 2 also describes the principles of operation for an IPS gateway that enables OSI-based application messages to be exchanged between an IPS host and an OSI end system. This product was developed in coordination with ICAO WG-I, RTCA SC-223, and EUROCAE WG-108
Airlines Electronic Engineering Committee
This specification covers a prepolymer in the form of an epoxy cresol novolac (ECN) resin
AMS P17 Polymer Matrix Composites Committee
This specification establishes environmental criteria for designing Aerospace Ground Equipment (AGE) in support of space systems. The test levels in this specification have been elevated to compensate for absence of combined environments during test, and to allow for variations in equipment and operating conditions. Environmental requirements are summarized in Table 1
Aerospace Council
This specification covers tapes for masking during paint stripping operations (see 6.1
AMS G8 Aerospace Organic Coatings Committee
This specification covers a foaming-type, heat-curing, resin-base adhesive in the form of paste or sheet
AMS P17 Polymer Matrix Composites Committee
This specification and its supplementary detail specifications cover film adhesives compounded from modified epoxy resins in the form of ready-to-use sheet, supplied in rolls, either supported by mat or by woven monofilaments or unsupported
AMS P17 Polymer Matrix Composites Committee
This specification covers interior aircraft cabin coatings, which when tested under specified conditions exhibit low heat release and smoke release properties
AMS G8 Aerospace Organic Coatings Committee
This specification covers a corrosion-inhibiting, water soluble, modified epoxy primer in liquid form
AMS P17 Polymer Matrix Composites Committee
This ARP establishes the basic test and design requirements for separable metal seal boss fittings for use in aerospace fluid systems
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
This specification covers aramid fibers in the form of woven cloth
AMS P17 Polymer Matrix Composites Committee
This specification covers the requirements for nonperforated nylon paper base plastic honeycomb core material for aircraft structural applications, including exterior parts such as radio and radar antenna housings
AMS P17 Polymer Matrix Composites Committee
This specification covers lightweight, circular cross-sectional flexible airduct hose, fabricated from laminated fabric reinforced plastics, or laminated fabric reinforced synthetic rubbers, to be used in aircraft air-conditioning and anti-icing systems
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
This specification covers the general requirements for pneumatic control valves for use with the starters on aircraft gas turbine engines. This specification shall be used in conjunction with AS943, ARP949, and AIR1639
AE-6 Starting Systems and Auxiliary Power Committee
This Aerospace Recommended Practice (ARP) defines and establishes design, construction, and performance requirements for a flexible, reuseable, water-vaporproof cover for environmental protection of internal combustion engines, major components, and other military and commercial items (see 6.1
AGE-4 Packaging, Handling and Transportability Committee
Refrigerant containment is an important part of servicing mobile air-conditioning (A/C) systems. This procedure provides guidelines for technicians for servicing mobile A/C systems and operating refrigerant recycling equipment designed for HFC-134a (R-134a) (described in SAE J2210
Interior Climate Control Service Committee
This specification covers the requirements for one type of water repellent compound
Aerospace Council
This document establishes the requirements for a lightweight, nonkink, flexible elastomeric hose. This hose is typically used with air-operated aircraft ice-preventive systems
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
This specification covers one type of cushion tread (semi-pneumatic) wheels for use on mobile ground support equipment
AGE-3 Aircraft Ground Support Equipment Committee
This specification and its supplementary detail specifications cover two types of nylon tape and three types of nylon webbing
AMS P Polymeric Materials Committee
This specification covers the design and performance requirements for one type of sound aural protector
AGE-3 Aircraft Ground Support Equipment Committee
This specification covers nylon in the form of marquisette cloth
AMS P Polymeric Materials Committee
This report is intended to provide users and producers of metallic shot and grit1 with general information on methods of mechanically testing metal abrasives in the laboratory
Surface Enhancement Committee
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
This standard defines general requirements for spherical, radial-journal, conical, and thrust bearings which are of laminated elastomeric construction. These bearings are for use in an environment having a temperature spectrum of -65 to +160 °F while reacting steady state loads in addition to oscillating loads and motions. The operating temperature range of -65 to +160 °F reflects the current temperature range for existing parts, but allows for expansion in the future
ACBG Plain Bearing Committee
This SAE Standard describes head position contours and procedures for locating the contours in a vehicle. Head position contours are useful in establishing accommodation requirements for head space and are required for several measures defined in SAE J1100. Separate contours are defined depending on occupant seat location and the desired percentage (95 and 99) of occupant accommodation. This document is primarily focused on application to Class A vehicles (see SAE J1100), which include most personal-use vehicles (passenger cars, sport utility vehicles, pick-up trucks). A procedure for use in Class B vehicles can be found in Appendix B
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The air cranking system components, which include the tank, valve, hose, and starter, must be carefully selected to provide the necessary speed to start an engine under the most severe climatic conditions for which the system is intended. Engine cranking loads increase with cold temperatures, therefore, the initial selection of these components, needs to consider low-temperature engine torque requirements. To insure an adequate air cranking system is obtained, it is important that proper test procedures are used for obtaining the cranking load requirements of the engine
Vehicle EE System Diagnostics Steering Committee
This SAE Recommended Practice identifies some basic and general conditions that should be considered when making electrical starter motor applications
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This SAE Metric Aerospace Standard (MA) provides minimum design, installation, and removal requirements for MA3520 and MA3521 thin wall inserts and is applicable when specified on engineering drawings or in procurement documents
E-25 General Standards for Aerospace and Propulsion Systems
This specification and its supplementary detail specifications cover various types of para-aramid fabric in the form of webbing
AMS P Polymeric Materials Committee
This specification covers general requirements for covers intended to protect the following aircraft parts: Cockpit Fuselage Canopy Engine Armament Propeller or Rotor Miscellaneous
AGE-2 Air Cargo
This document covers insulated, flexible air duct assemblies for portable ground support air conditioners and heaters
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
This document categorizes the different types of storage requirements, either on the aircraft or new unused or overhauled on the shelf, for aircraft landing gears/components. Recommendations and examples of proper landing gear storage are outlined. Reclamation recommendations are provided for aircraft landing gear returning from long-term storage
A-5 Aerospace Landing Gear Systems Committee
This specification covers hollow glass microspheres
AMS P Polymeric Materials Committee
This specification covers fluorocarbon (FKM) elastomeric coating materials for fiber-reinforced-resin composite structures in the form of two-component brushable or sprayable liquids
AMS G8 Aerospace Organic Coatings Committee
This specification covers the requirements for ozone resistant chlorosulfonated polyethylene rubber in sheet form and as molded or extruded parts
AMS CE Elastomers Committee
This SAE Aerospace Standard (AS) defines the requirements for a threaded flexible coupling assembly, which utilizes ferrules or machined tube end fittings to join tubing and components in aircraft fuel and fuel vent or other systems. This coupling assembly is designed for use from -65 to +200 °F and at 125 psig peak working pressure, and the coupling assembly may be used in other fluid systems when requirements are within the limits
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
This specification covers two grades of ethylene-propylene rubber having excellent resistance to ozone and hot water, but poor resistance to hydrocarbon oils or solvents
AMS CE Elastomers Committee
This specification covers semi-fluid lubricant suitable for use in aircraft gearboxes and transmissions
AMS M Aerospace Greases Committee
This specification covers methacrylate sheets, rods and tubes produced by casting or machining cast blanks. This specification does not apply to heat-formed and molded or extruded shapes, or shapes made by assembling two or more pieces
AMS P Polymeric Materials Committee
This SAE Aerospace Standard (AS) covers the requirements for threaded lubrication fittings, straights and elbows, to be used for admitting and retaining lubricants supplied by pressure lubricating equipment
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
This aerospace specification establishes the requirements for metric saddle or omega style clamps used for systems installation in aerospace equipment
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
This Aerospace Standard covers hose assemblies intended for use in aircraft high temperature fluid systems. The specified temperature range is -55°C (-67°F) to +204°C (400°F). Operating pressures are listed in Table I
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
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