SAE International Datasheets for Standards and Technical Documents
Standards and technical documents includes standards, codes, regulation, handbooks, manuals, comprehensive guides and other formal publications. Standards, codes, and regulation establish uniform specifications, procedures or technical criteria.
Standards and Technical Documents: Learn more
| Product Name | Notes |
|---|---|
| Aerospace Recommended Practice (ARP) 1533 is a procedure for the analysis and evaluation of the measured composition of the exhaust gas from aircraft engines. Measurements of carbon monoxide, carbon dioxide,... | |
| ARP 1834 provides general guidance for the selection, approach to, and performance of various kinds of F/FA of digital systems and equipment. Its prime objective is to present several industry-acceptable,... | |
| ARP1834 provides general guidance for the selection, approach to, and performance of various kinds of F/FA of digital systems and equipment. Its prime objective is to present several industry-acceptable, cost-effective... | |
| Corrosion control is always of concern to the designer of electronic enclosures. The use of EMI gaskets to provide shielding often creates requirements that are in conflict with ideal corrosion... | |
| Details of a durable type and semi-permanently attached placard with prescribed text for the permissible fluids are included in the document. | |
| Engine test data reduction programs may range from programs which are limited to calculation of external performance, e.g. thrust, fuel flow, and airflow, to those which include an analysis of... | |
| Included in this document are requirements for conveyor systems, guides, stops, restraint hardware that are used on trucks, transporters, dollies, storage provisions, pallet build-up hoists, or other device-handling equipment. a)... | |
| Included in this document are requirements for conveyor systems, guides, stops, restraint hardware that are used on trucks, transporters, dollies, storage provisions, pallet build-up hoists, or other device-handling equipment. These... | |
| Perishable cargoes, e.g., dairy produce, fruit, vegetables, flowers, frozen foods, meat, fish, etc., require maintenance of specific temperature ranges during air related door-to-door transportation. | |
| Recommendations of this Aerospace Recommended Practice (ARP) are not intended to satisfy the more detailed and stringent requirements of aircraft design development. Also, they may not be directly applicable to... | |
| Recommendations presented in this document are intended primarily for the acquisition of far-field acoustical data. The test engine is to be appropriately configured and operated so that the acoustical signals... | |
| 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... | |
| SAE Aerospace Recommended Practice ARP1533 is a procedure for the analysis and evaluation of the measured composition of the exhaust gas from aircraft engines. Measurements of carbon monoxide, carbon dioxide,... | |
| Status programs are neither preliminary design nor specification programs (as covered by SAE Standard AS 681C) but represent an additional category: They are intended to provide the best estimate of... | |
| Systems shall be classified in terms of type, category and class. | |
| Technical Standard | |
| Test procedures are described for measuring noise at specific locations (passenger and cargo doors, and servicing positions) and for conducting general noise surveys around aircraft. Requirements are identified with respect... | |
| Test procedures are described for measuring noise at specific receiver locations (passenger and cargo doors, and servicing positions) and for conducting general noise surveys around aircraft. Procedures are also described... | |
| The backup ring is defined. The various types designed for use with O-rings in MIL-G-5514 packing glands, and MS 33566 and MS 21344 universal fitting installations, are described. | |
| The backup ring is defined. The various types designed for use with O-rings in MIL-G-5514 packing glands, and MS33566 and MS21344 universal fitting installations are described. Guidelines are included for... | |
| The dedicated aircraft addressed herein is to be an uncompromised all-freighter aircraft developed primarily for use in the civil transport industry. The requirements of this document are applicable but not... | |
| The dedicated aircraft addressed herein is to be an uncompromised all-freighter aircraft developed primarily for use in the civil transport industry. The requirements of thsi document are applicable but not... | |
| The external threaded fastener protrusion shall be defined as the external threads including the chamfer which extend through the top surface of the nut, see figure 1 . | |
| The intent of this ARP is to identify electrical connectors maintained by the AE-8C1 Committee, to provide their general application characteristics, associated configuration options, and recommendations for new design (see... | |
| The intent of this ARP is to identify selected electrical connectors, their general application characteristics, and associated configuration options recommended for new design, repair, and retrofit purposes (see 6.1 ). | |
| The pilot's seat is the basic link that supports and ties the pilot to the aircraft structure. It is essential that this function be accomplished in a manner that will... | |
| The primary measurement procedure recommended in this ARP includes the recording of sound pressure signals in the interior of an airplane during steady state cruise conditions with analysis after the... | |
| The purpose of this Aerospace Recommended Practice is to standardize test equipment and procedures for the measurement of smoke emission from aircraft gas turbine engines. The procedures included are for... | |
| The purpose of this document is to describe the recommendations of SAE Committee S-7 for a Flight Management Computer System (FMCS) capable of providing the functions and displays listed below... | |
| The purpose of this document is to establish minimum operational requirements that will ensure that perishable cargoes in insulated standard airborne containers can be kept in prime condition during the... | |
| The purpose of this procedure is to establish a technique for reliably and repeatedly measuring the RF shielding characteristics of EMI gasket materials and EMI gaskets against various joint surfaces. | |
| The purpose of this recommended practice is to establish a standard format for the presentation of helicopter mission data, which will provide data required to establish airframe and/or engine component... | |
| The purpose of this recommended practice is to provide aircraft industry with guidelines as to the pertinent information which should be contained in a user's manual for an environmental control... | |
| The purpose of this recommended practice is to provide recommendations concerning the procedure for wave soldering. | |
| The purpose of this recommended practice is to provide the missile hydraulic and pneumatic component designer with information learned, tested, and substantiated in the correction of problems and failures experienced... | |
| The purpose of this SAE Aerospace Recommended Practice (ARP) is to recommend general design and performance characteristics for hand-held Portable, Emergency Lighting Systems (note: the portable portion of this system... | |
| The purpose of this SAE Aerospace Recommended Practice (ARP) is to recommend general design and performance characteristics for portable, hand-held emergency lighting systems intended for use by crew members of... | |
| The purpose of this standard is to provide the missile hydraulic and pneumatic component designer with information learned, tested and substantiated in correction of problems and failures experienced with seals... | |
| The recommendations listed in Section 3 shall apply to all regularly assigned flight crew member's seats located on the flight deck. | |
| The recommended practice establishes the requirements for lubricating oil filters for general aviation reciprocating engine applications with lubricating oil systems normally operating in a pressure range of 345 - 689... | |
| The requirements of this document are applicable to ground handling and transport systems equipment which is designated to accommodate main deck unitized cargo in the form of intermodal containers and... | |
| The requirements of this SAE Aerospace Recommended Practice (ARP) are applicable to ground handling and transport systems equipment which is designated to accommodate main deck unitized cargo in the form... | |
| The scope of this recommended practice covers specialized internal combustion engine powered equipment used in the support of aircraft operations. The equipment may be self-propelled, truck mounted, trailer mounted, skid... | |
| The scope of this SAE Recommended Practice covers specialized internal combustion engine powered equipment used in support of aircraft operations. The equipment may be self-propelled, truck mounted, trailer mounted, skid... | |
| The symbols specified in this ARP are applicable to all aircraft cargo handling systems for underfloor as well as for maindeck systems. Utilizing the symbols the conveyance, guidance, restraint, power... | |
| The symbols specified in this SAE Aerospace Recommended Practice (ARP) are applicable to all aircraft cargo handling systems for lower deck as well as for upper deck systems. Utilizing the... | |
| The test procedure applies to the refueling manifold system connecting the receiver aircraft fuel tanks to the refueling source fuel pump(s) for both ground and aerial refueling. The test procedure... | |
| The Test Procedure of ARP 1525 is Embodied in ASTM F519, Hydrogen Embrittlement Testing of Aerospace Materials. The requirements of the latest issue of ASTM F519 shall be fulfilled whenever... | |
| The tests are static in nature to minimize complexity and cost of required testing facilities. As far as practical, applied static loads should take into account the combined static and... | |
| The turbine-engine inlet flow distortion methodology addressed in this document applies only to the effects of inlet total-pressure distortion. Practices employed to quantify these effects are developing and therefore, periodic... | |
| The turbine-engine inlet flow distortion methodology addressed in this document applies only to the effects of inlet total-pressure distortion. Practices employed to quantify these effects continue to develop and, therefore,... | |
| These formulae shall be used to determine drop dimensions for simple bend tube fittings utilizing flare and flareless end connection designs from 0° to 90° used in aircraft and aerospace... | |
| These recommendations apply to the user's manual for any computer program pertaining to aircraft ECS. This includes computer programs for: a Cabin air conditioning and pressurization performance. b Avionics equipment... | |
| These recommendations are to aid the air transport industry in providing standard passenger safety information cards for use on commercial passenger carrying aircraft. | |
| These recommendations are to aid the international air transport industry by identifying a standard, minimum amount of safety instructions and procedures that should be provided in the PSIS. Aircraft operators... | |
| These recommendations are to aid the international air transport industry by identifying a standard, minimum amount of safety instructions that shall be given in passenger safety information briefing cards and,... | |
| These recommendations are to aid the international air transport industry by identifying a standard, minimum amount of safety instructions that shall be provided in passenger safety information briefing materials (generally... | |
| These recommendations are written to cover the subject of obtaining filter patch test samples from aerospace hydraulic equipment of the categories shown below. The same procedure shall apply regardless of... | |
| These recommendations cover the basic criteria for the design of aircraft cabin pressurization control systems as follows: (1) To ensure aircraft safety. (2) Physiology and limits which govern maximum permissible... | |
| This Aerospace Recommended Practice (ARP) covers a brief discussion of the icing problem in aircraft fuel systems and different means that have been used to test for icing. Fuel preparation... | |
| This Aerospace Recommended Practice (ARP) describes a class of digital computer programs for use by organizations other than the engine supplier for reduction of engine test data relating to the... | |
| This Aerospace Recommended Practice (ARP) describes a manufacturing method for processing unidirectional graphite fiber/epoxy resin impregnated sheet and tape into multi-ply broadgoods and tape produced on an automated cross-plying machine. | |
| This Aerospace Recommended Practice (ARP) describes a standard method and means for measuring or calibrating the "Spectrum Amplitude" output of an impulse generator. | |
| This Aerospace Recommended Practice (ARP) describes techniques for nondestructive test (NDT) evaluation of the quality of electron beam (EB) welded joints in titanium-base alloys with depths of section at the... | |
| This Aerospace Recommended Practice (ARP) describes techniques recommended for use in producing electron beam welded joints in materials commonly employed in the aerospace industry. The guidelines described herein are oriented... | |
| This Aerospace Recommended Practice (ARP) describes the continuous sampling and analysis of gaseous emissions from aircraft gas turbine engines and is intended to standardize the emission test procedures 2x and... | |
| This Aerospace Recommended Practice (ARP) describes the processing system and techniques for the surface preparation and priming of aluminum alloy parts for structural adhesive bonding to achieve optimum bondline durability,... | |
| This Aerospace Recommended Practice (ARP) establishes a method of testing, and criteria for comparative evaluation of the abrasion resistance of chafe guard, and also establishes standard test equipment to be... | |
| This Aerospace Recommended Practice (ARP) establishes criteria for the design and performance of aircraft life raft devices to ensure their rapid and effective use as a flotation device in a... | |
| This Aerospace Recommended Practice (ARP) establishes criteria for the design and performance of aircraft life raft devices which will ensure their rapid and effective use as a flotation device in... | |
| This Aerospace Recommended Practice (ARP) establishes the requirements and the procedures for impulse testing of actuators, valves and pressure containers for use in aerospace hydraulic systems. It also refers to... | |
| This Aerospace Recommended Practice (ARP) establishes uniform requirements for color coding of elastomeric cushions on clamps used in aerospace tubing systems, wire bundle retention, and similar applications. | |
| This Aerospace Recommended Practice (ARP) identifies "type" and "degree" of change to brake, wheel, or component thereof, and recommends substantiation procedures to confirm that performance capability of an existing aircraft... | |
| This Aerospace Recommended Practice (ARP) is a general overview of typical airborne engine vibration monitoring (EVM) systems applicable to fixed or rotary wing aircraft applications, with an emphasis on system... | |
| This Aerospace Recommended Practice (ARP) is intended to specify the environmental conditions necessary to permit the operating crew of large civil transport aircraft to perform their required duties and functions... | |
| This Aerospace Recommended Practice (ARP) is therefore intended to document the process of landing gear system development. Some of the steps covered are mandatory and others are elective, or dependent... | |
| This Aerospace Recommended Practice (ARP) is to establish criteria for design and installation of combination evacuation slide/raft devices for use both as ground and water escape devices in the event... | |
| This Aerospace Recommended Practice (ARP) is to provide a recommended minimum laboratory roll performance for main landing gear aircraft wheel without tire. | |
| This Aerospace Recommended Practice (ARP) outlines a recommended test procedure, data collection and preparation method for indoor noise tests of a bare turboshaft engine suitable for helicopter installations. It should... | |
| This Aerospace Recommended Practice (ARP) outlines the basic general design requirements for ground support equipment used in the civil air transport industry. It is intended to assist the airlines in... | |
| This Aerospace Recommended Practice (ARP) provides criteria for operational characteristics to be considered in the design of individual, inflatable life preservers intended for air transport safety. | |
| This Aerospace Recommended Practice (ARP) standardizes test equipment and procedures for the measurement of smoke emission from aircraft gas turbine engines. The procedures included are for determining and reporting the... | |
| This Aerospace Recommended Practice covers general requirements for preservation, packaging, and packing of hose assemblies. | |
| This Aerospace Recommended Practice covers the calibration and verification of automatic liquid-borne particle counter for the determination of the concentration by number and size distribution of particles in aerospace liquids. | |
| This aerospace recommended practice describes procedures for establishing a calibration curve for use with an automatic liquidborne particle counter (APC) and verifying the sizing and counting accuracy of the instrument. | |
| This Aerospace Recommended Practice establishes flexure test procedures to determine and classify the fatigue strengths of reconnectable or permanent hydraulic tube joints. The procedure is intended for conducting flexure tests... | |
| This Aerospace Recommended Practice includes the following areas: basis for system requirements; selection of materials coupled with hazards and safety; configuration of design; system operation; and evalua tion testing. | |
| This Aerospace Recommended Practice includes the following areas: basis for system requirements; selection of materials coupled with hazards and safety; configuration of design; system operation; and evaluation testing. | |
| This aerospace recommended practice provides a framework and suggested procedures or values for requirements for the design, performance, and test of hydraulically powered servoactuators for use in aircraft flight control... | |
| This Aerospace Recommended Practice provides technical and application information needed by the designers of aircraft electric systems and support equipment for the selection of overcurrent protective devices. It provides definitions... | |
| This Aerospace Recommended Practice recommends general criteria for the development and installation of an aircraft emergency signal system to permit any crew member (flight or cabin) to inform all other... | |
| This Aerospace Recommended Practice sets forth the guidelines for the use of non-black O-ring seals. Black is the preferred color for polymer types other than Silicone and Fluorosilicone. When a... | |
| This ARP applies to airline trailer equipment with four wheel running gear pulled and steered through an integral towbar; and which is used on airport ramps and other airport areas... | |
| This ARP applies to all types and models of civil aircraft for landing gear structure and mechanism excepting wheels, tires and brakes. All axles, wheel forks, axle beams, links, arms,... | |
| This ARP covers a procedure to be used in the determination of 0.05 to 0.3 ppm of chlorine in oxygen from any type of generator used for emergency or other... | |
| This ARP covers a procedure to be used in the determination of 0.05 to 0.3 PPM of chlorine in oxygen generated from any type of generator used for emergency or... | |
| 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,... | |
| This ARP covers procedures or methods to be used for fabricating, handling, testing, and installation of oxygen lines in an aircraft oxygen system. | |
| This ARP covers techniques for both paved and unpaved airfields. | |
| This ARP covers the basic criteria for the design of cabin pressure control systems (CPCS) for general aviation, commercial and military pressurized aircraft. | |
| This ARP covers the recommended requirements for the lighting and characteristics of instruments; information plates and displays; emergency, cautionary, advisory and status displays; circuit breaker and toggle switch positions; and... | |
| This ARP defines a recommended placard for readily identifying equipment with aircraft phosphate ester fluid to be used in the aircraft hydraulic systems to assure compatibility between the internal seals/materials... | |
| This ARP defines minimum requirements for horse stalls necessary to maintain a structurally safe operation and protect aircraft from corrosion created by waste spills. | |
| This ARP delineates requirements for system cleanliness, test gas supply system, test stand design, environmental chamber definition, instrumentation, dynamic test equipment and testing procedures. | |
| This ARP delineates two complementary filter element performance ratings and corresponding test procedures. It is intended for the noncleanable (disposable), fine fuel filter elements used in aviation gas turbine engine... | |
| This ARP describes methods for measuring the visual performance of direct view cathode ray tube displays used in aircraft flight decks and cockpits. Procedures may vary depending upon the type... | |
| This ARP describes procedure for determining the counting and sizing accuracy for an automatic liquid-borne particle counter (APC). This procedure is used in conjunction with a suspension of precisely sized... | |
| This ARP discusses design philosophy, system and equipment requirements, installation environment and design considerations for systems within the ATA 100 specification, Chapter 36, Pneumatic (reference 1). This ATA system/chapter covers... | |
| This ARP includes symbols for components and lines which are commonly used in the fuel and oil systems of airborne aerospace vehicles. | |
| This ARP is a system guide for Engine Monitoring System (EMS) definition and implementation. This keystone document addresses EMS benefits, capabilities and requirements. It includes EMS in-flight and ground applications... | |
| This ARP presents definitions of terminology used in conjunction with flight control systems. Terminology associated with fault-tolerant systems has been emphasized. No details of specific design approaches are given. Likewise,... | |
| This ARP presents definitions of terminology used in conjunction with redundant flight control systems. No details of specific redundant system design approaches are given. Likewise, no recommendations are included for... | |
| This ARP provides the definition of terms commonly used in aircraft environmental control system (ECS) design and analysis. Many of the terms may be used as guidelines for establishing standard... | |
| This ARP specifies both the nominal dimensions and the tolerances for a series of ball bearings with semifinished inside diameters which are suitable for supporting gas turbine rotating components in... | |
| This ARP specifies the methods, equipment, and materials to be used in the installation, mounting, and testing of receptacle connectors used in pressure differential applications requiring an effective connector seal. | |
| This ARP specifies the minimum design and test recommendations for aircraft tubeless tire and wheel overpressurization release devices to protect from possible explosive failure of the contained air chamber due... | |
| This document covers military aircraft wheel and brake equipment. | |
| This document covers military aircraft wheel and hydraulically actuated brake equipment. | |
| This document covers the recommended basics to be considered when assembling cadmium plated steel studs with rolled threads into cast, or forged, aluminum or magnesium parts. | |
| This document covers the recommended criteria and performance requirements for the design and installation of an aircraft emergency arresting hook intended for use with emergency runway arresting systems. Design criteria... | |
| This document defines design, performance, and test criteria for self-sealing breakaway valves for use in crash-resistant aircraft fuel systems. | |
| This document describes a hand-applied, non-tank, phosphoric acid anodizing process for surface preparation of aluminum alloys for structural adhesive bonding to achieve optimum bondline durability. | |
| This document describes a hand-applied, nontank, phosphoric acid anodizing process for surface preparation of aluminum alloys required to achieve optimum bondline durability for structural adhesive bonding. | |
| 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... | |
| This document describes a method for determining the specific gravity of tubing, fabricated from polytetrafluoroethyl ene, after a controlled heating and cooling cycle. The specific gravity obtained by this method... | |
| This document describes a procedure for determining depth of decarburization and carburization in heat treated carbon and low-alloy steel parts other than case hardened parts. It is not applicable to... | |
| This document describes an inspection procedure for detecting, by use of a radiographic opaque tracer and fluoroscopy methods, flaws which have been produced as the result of cutting, machining, or... | |
| This document describes an inspection procedure for detecting, by use of a radiographic opaque tracer and fluoroscopy or radiography methods, flaws which have been produced as the result of cutting,... | |
| This document describes techniques recommended for use in producing electron beam welded joints in materials commonly employed in the aerospace industry. | |
| This document describes the materials, equipment, and processing techniques used in fabricating high-strength or high-modulus carbon-fiber-reinfor ced polysulfone laminates for structural applications for service up to 120°C (250°F). | |
| This document describes the materials, equipment, and processing techniques used in fabricating high-strength or high-modulus graphite-fiber-reinf orced polysulfone laminates for structural applications for service up to 120°C (250°F). | |
| This document describes the materials, equipment, and processing techniques utilized in the fabrication of polyimide printed wiring boards. Included are recommendations for both double-sided and multi-layer boards. | |
| This document describes the materials, equipment, and processing techniques utilized in the fabrication of polyimide printed wiring boards. Included are recommendations for both double-sided and multilayer boards. | |
| This document establishes a test procedure for determining the propensity of aircraft turbine engine cleaning and maintenance materials for causing stress-corrosion cracking of titanium alloy parts. The evaluation is conducted... | |
| This document establishes general gland design criteria for static and dynamic O-ring seal applications used in fluid systems and at fluid pressures common to the aerospace industry. Detailed discussion of... | |
| This document establishes standard gland design criteria and dimensions for dynamic radial O-ring seal applications and provides recommendations for modifying these glands in special applications. There are no provisions in... | |
| This document establishes standard gland design criteria and dimensions for static axial O-ring seal applications without anti-extrusion devices specifically for engines and engine control systems operating at a maximum pressure... | |
| This document establishes standard gland design criteria and dimensions for static axial O-ring seal applications without anti-extrusion devices. | |
| This document establishes standard gland dimensions for static radial O-ring seal applications and provides recommendations for modifying these glands in special applications. No provisions are made in this document for... | |
| This document establishes the minimum requirements for the electrical bonding and grounding of electric, avionic, armament, communication, and electronic equipment installations for aeronautical and aerospace applications. The bonding and grounding... | |
| This document establishes the requirements for the sequencing of processes relating to parts fabricated from 300M or 4340 modified steel heat treated to, or to be heat treated to, 270,000... | |
| This document outlines the functional and design requirements for a battery-powered electric tow tractor in the handling of baggage or cargo trailers in airline service. | |
| This document provides a recommended practice for determining decarburization and carburization in heat treated carbon and low-alloy steel parts other than case hardened parts. It is not applicable to raw... | |
| This document provides a standard reference list of code designations to be applied to the various sleeves used on TFE hose assemblies when preparing related "AS" specifications and part numbers... | |
| This document provides a standard reference list of code designations to be applied to the various sleeves used on TFE hose assemblies when preparing related "AS" specifications and part numbers. | |
| This document provides recommended guidelines for a comprehensive program to determine the useful life of chemical oxygen generators where useful life is defined as the sum of shelf and service... | |
| This document provides recommended practices for the design, development, and verification testing of aircraft nosewheel steering (NWS) systems. | |
| This document provides recommended practices for the design, development, and verification testing of NWS systems. | |
| This document recommends and sets forth a set of symbols representing the components making up aircraft fuel and oil systems. The intended result is uniformity in system schematics so that... | |
| This document recommends general designs, tolerances, limits of application and suitable tooling, fixtures and accessories for mounting and driving jet engine rotors on horizontal and vertical balancing machines. | |
| This document recommends general gland design criteria for static and dynamic O-ring seal applications specifically for engines and engine control systems. | |
| This document recommends provisions for crew safety and survival which are intended to apply to cargo aircraft and equipment. This ARP applies specifically to cargo aircraft regardless of means of... | |
| This document recommends standard gland design criteria and dimensions for dynamic radial O-ring seal applications specifically for engine and engine control systems operating at pressures up to a maximum of... | |
| This document recommends standard gland dimensions for static radial O-ring seal applications specifically for engine and engine control systems and provides recommendations for modifying these glands in special applications. | |
| This document sets forth minimum roll performance capability for main landing gear wheel to be rolled without tire. The recommended test requirements establish a laboratory demonstration level to equate satisfactory... | |
| This document specifies those requirements and procedures for periodic tests to insure maintenance of balance machine capabilities for balancing jet engine components. It will specify: (a) Requirements for tests (b)... | |
| This document specifies those requirements and procedures for periodic tests to insure maintenance of balancing machine capabilities for balancing jet engine components. It will specify: (a) Requirements for tests. (b)... | |
| This document will be limited in scope to power transfer units made up of two fixed displacement pumps/motors. | |
| This is a procedure for calculation of gaseous emissions data, specifically, emission index, fuel-air ratio, and combustion efficiency for aircraft turbine engines based on the measurement of carbon monoxide, carbon... | |
| This method covers the determination of the fracture toughness of metallic materials (K SR or K SB ) by testing slotted short-rod or short-bar specimens. | |
| This practice provides a method for evaluating microhardness and microstructure very close (0.002 inch (0.051 mm) or less) to the surface of a disk specimen. Specific accept/reject criteria for partial... | |
| This practice provides a method of evaluating microhardness and microstructure very close to the surface of a disk specimen. It is useful for process control in heat treatment of steel... | |
| This practice provides a method of evaluating microhardness and microstructure very close to the surface. It is useful for process control in heat treatment of steel parts to detect nitriding... | |
| This practice provides recommendations concerning the chemical milling of aluminum, magnesium, high temperature nickel alloys, titanium alloys, copper alloys, and specialty alloys. | |
| This procedure is intended to apply to fuel pumps. This procedure will be defined in terms of recommended test fluid, test setup, test conditions, and test method. This procedure may... | |
| This procedure is intended to apply to fuel pumps. | |
| This recommended practice covers a laboratory procedure for determining the cleaning efficiency of aircraft turbine engine gas path cleaners. Results are indicative of cleaning compound performance in the compressor sections... | |
| This recommended practice covers a test for detecting residual chlorides and bromides on electronic equipment. | |
| This recommended practice covers the determination of the amount of stock loss caused by use of chemical cleaning agents on aircraft turbine engine materials. | |
| This recommended practice covers two methods of analysis for rapid and accurate quantative determination of trace elements in alloys having a base of iron, nickel, or cobalt and used at... | |
| This recommended practice 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. | |
| This recommended practice defines a procedure for evaluating the corrosive effects of aircraft maintenance chemicals on aluminum alloys under conditions of intimate contact by visual comparison with control specimens. | |
| This recommended practice defines a procedure for evaluating the corrosive effects of aircraft maintenance chemicals on low-embrittling cadmium plate used on aircraft high-strength steels under conditions of total immersion by... | |
| This recommended practice defines a procedure for evaluating, by quantitative measurement of weight change, the corrosive effects of aircraft maintenance chemicals on low-embrittling cadmium plate used on aircraft high-strength steels... | |
| This recommended practice describes a two-pole electric connector for use in battery powered ground support equipment i.e. traction batteries. Alternatively, the connector can have two or more auxiliary contacts for... | |
| This recommended practice describes a two-pole electric connector for use in battery powered ground support equipment, i.e., traction batteries. Alternatively, the connector can have two or more auxiliary contacts for... | |
| This recommended practice describes an industrial battery charger, solid state type, hereafter called charger, for use in charging lead acid batteries in ground support equipment. | |
| This recommended practice describes an industrial battery, lead acid type, for use in electric powered ground support equipment. | |
| This recommended practice describes the materials and procedures for cleaning aluminum alloy detail parts and low-alloy steel parts (other than corrosion resistant steel) prior to structural adhesive bonding operations. | |
| This recommended practice describes the physical and chemical characterization techniques for identification of epoxy adhesive and prepreg resin systems in order to verify the chemical formulation, resin B-staging (See 8.1... | |
| This recommended practice describes the processing system and techniques for the surface preparation and priming of aluminum alloy parts for structural adhesive bonding to achieve optimum bondline durability, corrosion resistance,... | |
| This recommended practice establishes a flexure test procedure for determining the fatigue strength of bent hydraulic tubing. The procedure is intended for conducting flexure fatigue testing of hydraulic and pneumatic... | |
| This recommended practice establishes a test procedure for determining the propensity of aircraft turbine engine cleaning and maintenance materials for causing stress-corrosion cracking of titanium alloy parts. | |
| This recommended practice establishes flexure test procedures to determine and classify the fatigue strengths of reconnectable or permanent hydraulic tube joints. The procedure is intended for conducting flexure tests of... | |
| This recommended practice establishes the method for qualification testing of tube joints and fitting attachments, using the flexure test method described in ARP 1185. This qualification test method requires the... | |
| This recommended practice establishes the method for qualification testing of tube joints and fittings using the rotary or planar flexure test method described in ARP 1185. This qualification test method... | |
| This recommended practice establishes the procedures and requirements for cleaning titanium alloy parts prior to adhesive bonding operations. | |
| This recommended practice establishes the procedures and requirements for the cleaning of titanium alloy parts prior to adhesive bonding operations. | |
| This recommended practice establishes the requirements for lubricating oil filters for general aviation reciprocating engine applications with lubricating oil systems normally operating in a pressure range of 50 - 100... | |
| This recommended practice is applicable to all involute splines used in Aerospace Propulsion Units. | |
| This recommended practice lists the recommended across flats limits for hexagon bar stock drawing callouts. This recommendation is based on the comparison of existing hexagon tolerance standards and minimum wrench... | |
| This recommended practice lists wrenching surface sizes for fluid fittings which utilize unmachined hex bar dimensions or forged flat dimensions on the finished machine parts as wrenching surfaces. | |
| This Recommended Practice outlines the basic general design requirements for powered mobile ground support equipment used in the civil air transport industry. It is intended to assist the airlines in... | |
| This Recommended Practice outlines the electrical performance characteristics for a continuous duty, diesel or gasoline engine driven brushless alternator unit for supplying 400-Hertz electrical power to commercial transport aircraft. It... | |
| This Recommended Practice outlines the functional and design requirements for a battery powered, self propelled belt conveyor for handling baggage and cargo at aircraft bulk cargo holds. | |
| This Recommended Practice outlines the general requirements for a transportable self-contained, continuous duty, diesel engine driven brushless alternator unit for supplying 400-Hertz electrical power to high performance commercial transport aircraft. | |
| This recommended practice outlines the general requirements of a continuous duty, electric motor-driven brushless alternator unit for supplying 400 Hz electrical power to high performance commercial transport aircraft. This specification... | |
| This recommended practice provides general recommendations for welding structural assemblies for aerospace ground support equipment. | |
| This recommended practice provides recommendations concerning the chemical milling of aluminum, magnesium, and titanium alloys, and specialty alloys. | |
| This report describes a method of determining the dielectric integrity of a spark plug by subjecting the insulation in the plug to voltage stress. | |
| This report describes basic method for measurement of spark energy on all types of capacitance discharge exciters. Reference is made to other methods which may be used if limitations are... | |
| This report is applicable to any type of aerospace ground support vehicle, powered, or unpowered. | |
| This SAE Aerospace Recommended Practice (ARP) applies to airline trailer equipment with four wheel running gear pulled and steered through an integral tow bar, for use on airport ramps and... | |
| This SAE Aerospace Recommended Practice (ARP) applies to landing gear structures and mechanisms (excluding wheels, tires, and brakes and other landing gear systems) for all types and models of civil... | |
| This SAE Aerospace Recommended Practice (ARP) applies to landing gear structures and mechanisms (excluding wheels, tires, and brakes) for all types and models of civil and military aircraft applications. All... | |
| This SAE Aerospace Recommended Practice (ARP) applies to landing gear structures and mechanisms (excluding wheels, tires, and brakes) for all types and models of civil and military aircraft including all... | |
| This SAE Aerospace Recommended Practice (ARP) applies to survival kits to be carried with life rafts or slide/rafts on transport category airplanes flying extended over-water routes and equipped with approved... | |
| This SAE Aerospace Recommended Practice (ARP) covers a laboratory procedure for determining the cleaning efficiency of aircraft turbine engine gas path cleaners. Results are indicative of cleaning compound performance in... | |
| This SAE Aerospace Recommended Practice (ARP) covers procedures or methods to be used for fabricating, handling, testing, and installation of oxygen lines in an aircraft oxygen system. | |
| This SAE Aerospace Recommended Practice (ARP) covers the determination of the amount of stock loss caused by use of chemical cleaning agents on aircraft turbine engine materials. | |
| This SAE Aerospace Recommended Practice (ARP) covers the dimensions of an inside splined driver-wrench adapter, envelope of the housing-wrench reaction, the mechanical method of adapting the driver-wrench adapter to the... | |
| This SAE Aerospace Recommended Practice (ARP) covers the recommended criteria and performance requirements for the design and installation of land-based aircraft emergency and operational arresting hooks for use on runway... | |
| 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... | |
| This SAE Aerospace Recommended Practice (ARP) defines a method of numbering aircraft engine cylinders. | |
| This SAE Aerospace Recommended Practice (ARP) defines impulse test procedures that are recommended for hydraulic components. | |
| This SAE Aerospace Recommended Practice (ARP) defines minimum requirements for an aircraft transport ULD to transport horses properly and safely by air, to protect the horse(s) from injuries and to... | |
| This SAE Aerospace Recommended Practice (ARP) defines minimum requirements for an aircraft transport ULD to transport horses properly and safely by air, to protect the horse(s) from injuries, and to... | |
| This SAE Aerospace Recommended Practice (ARP) defines recommended planning and substantiation procedures and associated reviewing and approval processes to confirm that proposed changes do not compromise the demonstrated safety of... | |
| This SAE Aerospace Recommended Practice (ARP) defines recommended substantiation procedures and associated reviewing and approval processes to confirm that proposed changes do not compromise the demonstrated safety, performance, and airplane... | |
| This SAE Aerospace Recommended Practice (ARP) defines the measurement parameters that may be used by a pilot or operator to monitor the thermodynamic health of a turboshaft engine in a... | |
| This SAE Aerospace Recommended Practice (ARP) delineates the minimum operational requirements that will ensure that perishable cargoes in insulated standard airborne containers are kept in prime condition during the ground... | |
| This SAE Aerospace Recommended Practice (ARP) delineates two complementary filter element performance parameters: (1) dirt capacity, and (2) filtration efficiency, and corresponding test procedures. It is intended for non-cleanable (disposable),... | |
| This SAE Aerospace Recommended Practice (ARP) delineates two complementary filter element performance ratings: (1) dirt capacity, and (2) filtration efficiency, and corresponding test procedures. It is intended for non-cleanable (disposable),... | |
| This SAE Aerospace Recommended Practice (ARP) describes a class of digital computer programs for use by organizations other than the engine supplier for reduction of engine test data relating to... | |
| This SAE Aerospace Recommended Practice (ARP) describes a two-pole electric connector for use in battery powered ground support equipment, i.e., traction batteries. Alternatively, the connector can have two or more... | |
| This SAE Aerospace Recommended Practice (ARP) describes an industrial battery charger, solid state type, hereafter called charger, for use in charging lead acid batteries in ground support equipment. | |
| This SAE Aerospace Recommended Practice (ARP) describes an industrial battery, lead-acid type, for use in electric powered ground support equipment. | |
| This SAE Aerospace Recommended Practice (ARP) describes procedures for solution and solid graphite furnace atomic absorption spectrometric determination of lead, bismuth, selenium, tellurium, and thallium in nickel and cobalt high... | |
| This SAE Aerospace Recommended Practice (ARP) describes procedures for the determination of trace elements listed in AMS2280 for Nickel, Cobalt, and Iron-based high temperature alloys. | |
| This SAE Aerospace Recommended Practice (ARP) describes the continuous sampling and analysis of gaseous emissions from aircraft gas turbine engines. The measured gas species include carbon monoxide (CO), carbon dioxide... | |
| This SAE Aerospace Recommended Practice (ARP) describes three general types of Ground Support Equipment (GSE) battery chargers. The battery charger typically requiring up to 8 hours to recharge a 100%... | |
| This SAE Aerospace Recommended Practice (ARP) describes two general types of Ground Support Equipment (GSE) battery chargers. The conventional industrial battery charger typically requiring up to 8 hours to recharge... | |
| This SAE Aerospace Recommended Practice (ARP) discusses damage to aircraft fuselages caused by ground equipment contact at servicing and recommends methods to be incorporated or considered in ground equipment design... | |
| This SAE Aerospace Recommended Practice (ARP) discusses design philosophy, system and equipment requirements, installation environment and design considerations for military and commercial aircraft systems within the Air Transport Association (ATA)... | |
| This SAE Aerospace Recommended Practice (ARP) establishes a method of testing, and criteria for comparative evaluation of the abrasion resistance of chafe guard, and also establishes standard test equipment to... | |
| This SAE Aerospace Recommended Practice (ARP) establishes design guidance and photometric values for adequate cargo compartment and cargo access lighting systems for ground handling. The adoption of a standard set... | |
| This SAE Aerospace Recommended Practice (ARP) establishes design guidance for adequate and safe cargo compartment and cargo access lighting systems. The adoption of a standard set of illumination values, found... | |
| This SAE Aerospace Recommended Practice (ARP) establishes flexure test procedures to determine and classify the fatigue strengths of reconnectable or permanent hydraulic tube joints. The procedure is intended for conducting... | |
| This SAE Aerospace Recommended Practice (ARP) establishes recommendations with respect to personnel and aircraft safety for the design of lavatory compartments in commercial aircraft. Consideration should be given to the... | |
| This SAE Aerospace Recommended Practice (ARP) establishes requirements for the function, characteristics, and installation of an aircraft On Board Weight and Balance System (OBWBS) for use on civil transport aircraft. | |
| This SAE Aerospace Recommended Practice (ARP) establishes safety recommendations for lavatories in transport category airplanes. | |
| This SAE Aerospace Recommended Practice (ARP) establishes the criteria for the development and installation of an aircraft emergency signal system to permit any crew member to inform all other crew... | |
| This SAE Aerospace Recommended Practice (ARP) establishes the method for qualification testing of tube joints and fitting attachments, using the flexure test method described in ARP1185. This qualification test method... | |
| This SAE Aerospace Recommended Practice (ARP) establishes the minimum contents of and suggested supplements for survival kits for transport category airplanes flying over water areas during airline service. | |
| This SAE Aerospace Recommended Practice (ARP) establishes the minimum requirements and procedures for impulse testing of aerospace hydraulic actuators, valves, pressure containers, and similar fluid system components, except accumulators, for... | |
| This SAE Aerospace Recommended Practice (ARP) establishes the minimum requirements and procedures for impulse testing of aerospace hydraulic actuators, valves, pressure containers, and similar fluid system components, for use in... | |
| This SAE Aerospace Recommended Practice (ARP) establishes the requirements for lubricating oil filters for general aviation reciprocating engine applications with lubricating oil systems normally operating in a pressure range of... | |
| This SAE Aerospace Recommended Practice (ARP) establishes the requirements for the design, performance, and tests for hydraulically powered servoactuators for use in aircraft flight control systems. | |
| This SAE Aerospace Recommended Practice (ARP) establishes uniform requirements for color coding of elastomeric cushions on clamps used in aerospace tubing systems, wire bundle retention, and similar applications. | |
| This SAE Aerospace Recommended Practice (ARP) examines the whole construct of an Engine Health Management (EHM) system. This keystone document gives a top-level view and addresses EHM description, benefits, and... | |
| This SAE Aerospace Recommended Practice (ARP) identifies and defines a method of measuring those factors affecting installed power available for helicopter power plants. These factors are installation losses, accessory power... | |
| This SAE Aerospace Recommended Practice (ARP) identifies and defines a method of measuring those factors affecting installed power available for helicopter powerplants. These factors are installation losses, accessory power extraction,... | |
| This SAE Aerospace Recommended Practice (ARP) includes recommended ground flotation analysis methods for both paved and unpaved airfields with application to both commercial and military aircraft. | |
| This SAE Aerospace Recommended Practice (ARP) includes recommended ground flotation analysis methods for both paved and unpaved airfields. | |
| This SAE Aerospace Recommended Practice (ARP) is a system guide for Engine Monitoring System (EMS) definition and implementation. This keystone document addresses EMS benefits, capabilities, and requirements. It includes EMS... | |
| This SAE Aerospace Recommended Practice (ARP) is an application guide for hydraulic power transfer units and describes: The various types Typical design approaches Their operational characteristics and limitations Circuit recommendations... | |
| This SAE Aerospace Recommended Practice (ARP) is an application guide for hydraulic power transfer units, and describes the various types, typical design approaches, their operational characteristics and limitations, circuit recommendations,... | |
| This SAE Aerospace Recommended Practice (ARP) is applicable to any type of aerospace ground support vehicle, powered or unpowered. | |
| This SAE Aerospace Recommended Practice (ARP) is intended to document the process of landing gear system development. This document includes landing gear system development plans for commercial, military, fixed wing... | |
| This SAE Aerospace Recommended Practice (ARP) is intended to document the process of landing gear system development. This document includes landing gear system development plans for commercial/military, fixed wing, and... | |
| This SAE Aerospace Recommended Practice (ARP) is intended to recommend: a uniform criteria for determination of wind loads that aircraft ground support equipment can encounter and yet allow personnel to... | |
| This SAE Aerospace Recommended Practice (ARP) is to provide a recommended minimum laboratory roll performance for main landing gear aircraft wheels without tires installed and applies to both bolted and... | |
| This SAE Aerospace Recommended Practice (ARP) is to provide a recommended minimum laboratory roll performance for main landing gear aircraft wheels without tires installed and applies to both split wheel... | |
| This SAE Aerospace Recommended Practice (ARP) lists wrenching surface sizes and tolerances for fluid fittings which utilize machined or unmachined hex bar dimensions and machined or forged wrenching surfaces across... | |
| This SAE Aerospace Recommended Practice (ARP) outlines the basic general design requirements for ground support equipment used in the civil air transport industry. It is intended to assist in standardizing... | |
| This SAE Aerospace Recommended Practice (ARP) outlines the basic general design requirements for ground support equipment used in the civil air transport industry. It is intended to assist the airlines... | |
| This SAE Aerospace Recommended Practice (ARP) outlines the design and performance requirements for a battery-powered electric tow tractor for the handling of baggage or cargo trailers in airline service. The... | |
| This SAE Aerospace Recommended Practice (ARP) outlines the functional and design requirements for a b self-propelled belt conveyor for handling baggage and cargo at aircraft bulk cargo holds. Additional considerations... | |
| This SAE Aerospace Recommended Practice (ARP) outlines the functional and design requirements for a battery powered, self-propelled belt conveyor for handling baggage and cargo at aircraft bulk cargo holds. Additional... | |
| This SAE Aerospace Recommended Practice (ARP) outlines the functional and design requirements for a battery powered, self-propelled belt conveyor for handling baggage and cargo at aircraft bulk cargo holds. | |
| This SAE Aerospace Recommended Practice (ARP) presents a recommended part numbering scheme for fluid system component parts, which may require complex standard numbers. Standardizing on certain numbering systems provides for... | |
| This SAE Aerospace Recommended Practice (ARP) provides a guide for the preparation of a Helicopter Engine/Airframe Interface Document and Checklist. This document and checklist is intended to provide complete relevant... | |
| This SAE Aerospace Recommended Practice (ARP) provides a guide for the preparation of a helicopter engine/airframe interface document and checklist. This document and checklist should identify the information needed by... | |
| This SAE Aerospace Recommended Practice (ARP) provides a procedure for obtaining filter patch test samples from the following types of aerospace non-rotating hydraulic equipment: Mechanical/Hydraulic Units Electro/Hydraulic Units Pneumatic/Hydraulic Units... | |
| This SAE Aerospace Recommended Practice (ARP) provides a standard reference list of code designations to be applied to the various sleeves used on hose assemblies when preparing related "AS" specifications... | |
| This SAE Aerospace Recommended Practice (ARP) provides an overview of the various types of polytetrafluoroethyl ene (PTFE and TFE) back up rings for hydraulic and pneumatic fluid power applications, including... | |
| This SAE Aerospace Recommended Practice (ARP) provides an overview of the various types of polytetrafluoroethyl ene (PTFE) backup rings for hydraulic and pneumatic fluid power applications, including their advantages and... | |
| This SAE Aerospace Recommended Practice (ARP) provides guidance on the engine performance parameters that may be selected by airframe and engine manufacturers, and used by a pilot or operator, to... | |
| This SAE Aerospace Recommended Practice (ARP) provides recommended practices for cleaning aircraft oxygen equipment such as tubing, pieces parts (including regulator and valve parts), cylinders and ground-based equipment that may... | |
| This SAE Aerospace Recommended Practice (ARP) provides recommended practices for cleaning aircraft oxygen equipment such as tubing, pieces, parts (including regulator and valve parts), cylinders and ground-based equipment that may... | |
| This SAE Aerospace Recommended Practice (ARP) provides recommended practices for the cleaning of aircraft oxygen equipment, both metallic and non-metallic articles, such as oxygen lines (tubes, hoses, etc.), components (including... | |
| This SAE Aerospace Recommended Practice (ARP) provides technical and application information needed by the designers of aircraft electric systems and support equipment for the selection of overcurrent protective devices. It... | |
| This SAE Aerospace Recommended Practice (ARP) provides the definition of terms commonly used in aircraft environmental control system (ECS) design and analysis. Many of the terms may be used as... | |
| This SAE Aerospace Recommended Practice (ARP) specifies pictographic symbols for ground support equipment. They have been compiled for the benefit of those who deal with such equipment like airlines, airport... | |
| This SAE Aerospace Recommended Practice (ARP) specifies requirements for those portions of the aircraft Unit Load Device ground and terminal handling equipment that will have a direct bearing on the... | |
| This SAE Aerospace Recommended Practice (ARP) specifies the methods, equipment, and materials to be used in the installation, mounting, and testing of receptacle connectors used in pressure differential applications requiring... | |
| This SAE Aerospace Recommended Practice (ARP) specifies the minimum design and qualification test recommendations for aircraft wheel overpressurization release devices used with tubeless aircraft tires to protect from possible explosive... | |
| This SAE Aerospace Recommended Practice (ARP) specifies the minimum design and test recommendations for aircraft tubeless tire and wheel overpressurization release devices to protect from possible explosive failure of the... | |
| This SAE Aerospace Recommended Practice (ARP) specifies the minimum design and test recommendations for aircraft wheel overpressurization release devices used with tubeless aircraft tires to protect from possible explosive failure... | |
| This SAE Aerospace Recommended Practice (ARP) standardizes test equipment and procedures for the measurement of smoke emission from aircraft gas turbine engines. The procedures included are for determining and reporting... | |
| This SAE Aerospace Recommended Practice covers the recommended requirements for the lighting and characteristics of instruments; information plates and displays, emergency, cautionary, advisory and status displays; circuit breaker and toggle... | |
| This SAE Aerospace Recommended Practice defines a method for determining the weldability of weld filler metal in continuous coil or cut length form. It is applicable to all solid (non... | |
| This SAE Aerospace Recommended Practice describes the aluminum weldbonding process for fabrication of secondary aircraft structural assemblies possessing excellent strength, fatigue life, and environmental durability. | |
| This SAE Aerospace Recommended Practice recommends general criteria for the development and installation of an aircraft emergency signal system to permit any crew member (flight or cabin) to inform all... | |
| This specification covers the general requirements for conventional AC and/or DC current carrying filter networks for the reduction of electromagnetic interference. A conventional filter is defined herein as a component... | |
| This specification covers the requirements for aircraft, hydraulic, self sealing, quick disconnect couplings, for use in type II hydraulic systems (-65°F to +275°F temperature range) as defined by MIL-H-5440. | |
| This specification describes a method for determining the specific gravity of tubing, fabricated from polytetrafluoroethyl ene, after a controlled heating and cooling cycle. The specific gravity obtained by this method... | |
| This specification describes the materials, equipment, and procedures used in fabricating foam-in-place flight helmet liners. | |
| This specification establishes general design, performance, and test requirements for hydraulically powered servoactuators when used in aircraft flight control systems. | |
| This specification establishes the requirements for power operated hydraulic servoactuators when used in flight control systems. These servoactuators may be controlled by mechanical, hydraulic or electrical inputs or combinations thereof,... | |
| This specification has been declared Superseded by the Aerospace Materials Division SAE, as of January, 1993. | |
| This Technical Report has been declared "CANCELLED" as of November 2017. By this action, this document will remain listed in the respective index, if applicable. Cancelled Technical Reports are available... | |
| To provide a recommended practice covering the method criteria for defining 'wear limit' on involute splines. This recommended practice is applicable to all involute splines used in Aerospace Propulsion Units. | |
| Transient engine performance computer programs will be the primary source for time-dependent variations of engine performance. Steady-state engine performance computer programs will be the primary source for steady-state engine performance. |
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