Search
Advanced Search
of the following are true

Results

Items (208,190)
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 ARP describes recommended sampling conditions, instrumentation, and procedures for the measurement of nonvolatile particle number and mass concentrations from the exhaust of aircraft gas turbine engines. Procedures are included to estimate sampling system loss performance. This ARP is not intended for in-flight testing, nor does it apply to engines operating in the afterburning mode. This ARP is intended as a guide toward standard practice and is subject to change to keep pace with experience and technical advances
E-31P Particulate Matter 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 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 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 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 semi-fluid lubricant suitable for use in aircraft gearboxes and transmissions
AMS M Aerospace Greases Committee
This specification covers a solvent-dispersed, corrosion-inhibiting compound packaged in aerosol cans
AMS B Finishes Processes and Fluids Committee
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 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 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 interior aircraft cabin coatings, which when tested under specified conditions exhibit low heat release and smoke release properties
AMS G8 Aerospace Organic Coatings 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 SAE Aerospace Recommended Practice (ARP) recommends design and test criteria for reusable shipping and storage stands for aircraft engines. An optional hard cover (enclosure) is also specified
AGE-4 Packaging, Handling and Transportability 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 specification covers hard-pressed fiberboard in the form of flat panels
AMS P17 Polymer Matrix Composites Committee
This specification covers the requirements for adhesives in film form for bonding metal facings to metal cores and to metal components of sandwich panels which are intended for use in primary and secondary structural airframe parts that may be exposed to temperatures up to 500°F (260°C
AMS P17 Polymer Matrix Composites 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 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
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 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 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
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 specification covers one type of cushion tread (semi-pneumatic) wheels for use on mobile ground support equipment
AGE-3 Aircraft Ground Support Equipment Committee
The purpose of this SAE Aerospace Recommended Practice (ARP) is to provide the aerospace industry with recommendations concerning the minimization of stress corrosion cracking in wrought heat-treatable carbon and low alloy steels and in austenitic, precipitation hardenable, and martensitic corrosion-resistant steels and alloys. The detailed recommendations are based on laboratory and field experience and reflect those design practices and fabrication procedures which should avoid in-service stress corrosion cracking
AMS E Carbon and Low Alloy Steels Committee
This document presents minimum criteria for the design and installation of LED passenger reading light assemblies in commercial aircraft. The use of “shall” in this specification expresses provisions that are binding. Non-mandatory provisions use the term “should
A-20C Interior Lighting
This Aerospace Standard covers two basic Stall Warning Systems, one measures air flow and pressure distribution on the airfoil and the other measures the angle of airflow with respect to an arbitrary reference line. Each type of system includes, as a minimum, a sensor and the means for activating a device which warns the pilot of an impending stall
A-4 Aircraft Instruments Committee
Recommendations presented in this document are intended primarily for the acquisition of far-field noise data. The test engine is to be appropriately configured and operated so that the sound pressure levels obtained are consistent with the specific objectives of the test. The principal output of the data reduction system is one-third octave band sound pressure levels. However, when appropriate, data may be recorded for purposes of broader or narrower bandwidth analysis
A-21 Aircraft Noise Measurement Aviation Emission Modeling
This specification covers aramid fibers in the form of woven cloth
AMS P17 Polymer Matrix Composites Committee
This specification covers a corrosion-inhibiting, water soluble, modified epoxy primer in liquid form
AMS P17 Polymer Matrix Composites Committee
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
Items per page:
1 – 50 of 208190