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 |
|---|---|
| No scope available. An Amendment corresponding to this standard is available at AS20659A_A1 | |
| No scope available. | |
| Pallet extensions provide support for items of cargo beyond either the short or the long sides of a pallet, allowing increased volume to be achieved. The extensions are designed to... | |
| Technical Standard | |
| The purpose of this SAE Aerospace Standard (AS) is to provide a description of the temper nomenclature system for aluminum alloys used in the aerospace industry by combining information from... | |
| The scope of this Aerospace Standard shall cover the methodology of defining and determining the "Internal Volumes" of both the main deck and lower deck aircraft cargo compartments. The minimum... | |
| The scope of this SAE Aerospace Standard (AS) shall cover the methodology of defining and determining the "internal volumes" of both the main deck and lower deck aircraft cargo compartments. | |
| This Aerospace Standard (AS) covers the requirements for polytetrafluoroethyl ene (PTFE) hose assemblies for use in aerospace hydraulic, fuel, and lubricating oil systems at temperatures between -67°F and 450°F for... | |
| This Aerospace Standard (AS) defines maximum free opening dimensions for airframe refueling ports on civil aircraft that require the exclusive use of aviation gasolines, and minimum free opening dimensions for... | |
| This Aerospace Standard (AS) defines the requirements for a polytetrafluoroethyl ene (PTFE) lined, para-aramid fiber reinforced, hose assembly suitable for use up to 4000 psi, and up to 275 °F,... | |
| This AS defines maximum free opening dimensions for airframe refueling ports on civil aircraft that require the exclusive use of aviation gasolines, and minimum free opening dimensions for airframe refueling... | |
| This document defines the requirements for a PTFE lined, aramid reinforced assembly suitable for use up to 275 °F and up to 4000 lbf/in 2x aircraft and missile hydraulic and... | |
| This document defines the requirements for a PTFE lined, aramid reinforced assembly suitable for use up to 275 °F and up to 4000 psi aircraft and missile hydraulic and pneumatic... | |
| This document establishes age limit and guidance for acceptance of hose and hose assemblies containing elastomeric materials for use in aircraft, space vehicles, missiles and component assemblies thereof at time... | |
| This document establishes age limits for acceptance of hose and hose assemblies containing elastomeric materials for use in aircraft, space vehicles, missiles and component assemblies thereof at time of delivery... | |
| This document establishes the requirements for aircraft, hydraulic couplings, self-sealing one side only, for use in Type II hydraulic systems (-65 to +275 °F temperature range) as defined by MIL-H-5440. | |
| This document establishes the temperature types and pressure classes that are commonly used in aerospace fluid systems. The temperature types and pressure classes are equivalent, but not identical, to the... | |
| This document is a design standard and is not to be used as a part number. The fitting end described within this standard is part of a non-reversible series described... | |
| This document is a design standard and is not to be used as a part number. This design standard describes the assembly and/or installation of a series of fitting ends... | |
| This document is a design standard and is not to be used as a part number. This standard describes a fitting end which is identical to the MS 33656 standard... | |
| This document is a design standard and is not to be used as a part number. This standard describes a standard flareless fitting end except that the thread and related... | |
| This drawing specifies parts AS19612, AS19613, AS19614, AS19615, AS19616, AS19617, AS19618, AS19619, AS19620, AS19621, AS19622, AS19623, AS19624, AS19625, AS19626, AS19627, AS19628, AS19629, AS19630, AS19631, AS19632, AS19634, AS19636, AS19638, AS19640, AS19642,... | |
| This drawing specifies parts AS20623, AS20624, AS20625, AS20626, AS20627, AS20628, AS20629, AS20630, and AS20631. To view suppliers qualified to manufacture this part, visit https://ts200.sae-it c.org/ . | |
| This list of terms, with accompanying photomicrographs where appropriate, is intended as a guide for use in the preparation of material specifications. | |
| This SAE Aerospace Standard (AS) defines the maximum allowable free opening dimensions for airframe fueling ports on civil aircraft that require the exclusive use of gasoline as an engine fuel,... | |
| This SAE Aerospace Standard (AS) defines the maximum allowable free opening dimensions for airframe fueling ports on civil aircraft that require the exclusive use of gasoline as an engine fuel... | |
| This SAE Aerospace Standard (AS) defines the requirements for a polytetrafluoroethyl ene (PTFE) lined, para-aramid fiber reinforced, hose assembly suitable for use up to 4000 psi, and up to 275... | |
| This SAE Aerospace Standard (AS) defines the requirements for polytetrafluoroethyl ene (PTFE) lined, metallic reinforced, hose assemblies suitable for use in aerospace hydraulic, fuel and lubricating oil systems at temperatures... | |
| This SAE Aerospace Standard (AS) defines the requirements for polytetrafluoroethyl ene (PTFE) lined, metallic reinforced, hose assemblies suitable for use in aerospace hydraulic, fuel, and lubricating oil systems at temperatures... | |
| This SAE Aerospace Standard (AS) establishes the characteristics and utilization of 270 V DC electric power at the utilization equipment interface and the constraints of the utilization equipment based on... | |
| This SAE Aerospace Standard (AS) establishes the dimensional and operational requirements for pallet extension devices. It provides support for items of cargo beyond either the short or the long sides... | |
| This SAE Aerospace Standard (AS) establishes the general requirements for the design, construction, acceptance, and qualification testing of flat cut-off pressure compensated, variable delivery hydraulic pumps used in military aircraft... | |
| This SAE Aerospace Standard (AS) establishes the requirements for 24 degree cone flareless fluid connection fittings and nuts, internally or externally swaged, preset, or welded sleeves for use in aircraft... | |
| This SAE Aerospace Standard (AS) establishes the requirements for 24° cone flareless fluid connection fittings and nuts, internally or externally swaged or welded sleeves or tube end adapters used only... | |
| This SAE Aerospace Standard (AS) establishes the requirements for 24° cone flareless fluid connection fittings and nuts, internally or externally swaged, preset, or welded sleeves for use in aircraft fluid... | |
| This SAE Aerospace Standard (AS) establishes the requirements for bite type sleeves for use with 24° cone flareless fluid connection fittings per AS18280. | |
| This SAE Aerospace Standard (AS) establishes the requirements for internally or externally swaged or welded sleeves or tube end adapters for use with 24° cone flareless fluid connection fittings per... | |
| This SAE Aerospace Standard (AS) establishes vibration and transmissibility test procedures which compare the relative strengths of various loop and saddle type support clamps. This procedure is intended for conducting... | |
| This SAE Aerospace Standard (AS) presents all appropriate boss dimensions from .125 inch to 2.0 inch tube sizes. | |
| This SAE Aerospace Standard (AS) provides for aircraft reciprocating engines formats for altitude graph sheets recommended for use when presenting engine performance data. | |
| This SAE Aerospace Standard establishes the requirements for a grooved clamp coupling, flanges, and seal suitable for joining high pressure and high temperature ducting in aircraft bleed air systems. The... | |
| This SAE Aerospace Standard establishes the requirements for a V-retainer coupling, flanges, and seal suitable for joining high pressure and high temperature ducting in aircraft bleed air systems. The rigid... | |
| This SAE Aerospace Standard establishes the requirements for a V-retainer coupling, flanges, and seal suitable for joining high-pressure and high-temperature ducting in aircraft bleed air systems. The rigid coupling joint... | |
| This specification and a detail pump specification establish the requirements for variable flow hydraulic pumps, for use in aircraft hydraulic systems conforming to and as defined in MIL-H-5440 and MIL-H-8891,... | |
| This specification covers the detail requirements for control transformer synchro, type 16CTB4b, 90 volt, 400 cycle. | |
| This specification covers the general requirements for the design and installation of fluid anti-icing, de-greasing, and washing systems installed in military aircraft. | |
| This specification covers the general requirements for the design, installation, and performance of thermal anti-icing equipment for the wings and empennage surfaces in aircraft. | |
| This specification covers the installation of aircraft interior lighting for military aircraft. | |
| This specification covers the installation of aircraft interior lighting. | |
| This specification covers the requirements for aircraft, hydraulic couplings, self sealing one side only, for use in Type II hydraulic systems (-65°F to +275° temperature range) as defined by MIL-H-5440. | |
| This specification covers the requirements for installation of fuel and oil lines in aircraft, except those lines furnished as part of the engine. | |
| This specification covers the requirements for self-sealing, quick-disconnect couplings for fuel and oil system components. | |
| This specification defines the requirements for a grooved clamp coupling and flanges suitable for joining intermediate pressure and temperature ducting in aircraft air systems. The rigid coupling joint assembly, hereafter... | |
| This specification defines the requirements for a grooved clamp coupling, flanges and seal suitable for joining high pressure and high temperature ducting in aircraft bleed air systems. The rigid coupling... | |
| This specification defines the requirements for a PTFE lined, non-metallic, aramid reinforced assembly suitable for use to 275°F and to 4000 lbf/in 2x (27 500 kPa) aircraft and missile hydraulic... | |
| This specification establishes the requirements for flareless tube connection fittings, nuts and sleeves for use in fluid systems (see 6.1 ). | |
| This specification relates to Synchros, 60 and 400 Hz. It is not complete in itself, but shall be used in conjunction with MIL-S-81963 in which the latter shall be recognized... | |
| This standard establishes the characteristics and utilization of 270-VDC electric power at the utilization equipment interface and the constraints on the utilization equipment. These characteristics shall be applicable for both... | |
| This supplement forms a part of AS1975, Hose Assembly, Polytetrafluoroethyl ene, Para-Aramid Reinforced, 3000/4000 psi, 275 °F, Standard Duty, Hydraulic, Aircraft Systems and shall be used to identify hose assembly... | |
| This supplement forms a part of the Aerospace Standard AS18280 Fittings, 24° Cone, Flareless, Fluid Connection, 3000 psi, and shall be used to identify fitting standards citing this procurement specification. | |
| This supplement forms a part of the Aerospace Standard AS1946, Hose Assembly, Polytetrafluoroethyl ene, Metallic Reinforced, up to 1500 psi and 450 ° F, Hydraulic and Pneumatic, and shall be... | |
| This supplement forms a part of the Aerospace Standard AS1946, Hose Assembly, Polytetrafluoroethyl ene, Metallic Reinforced, up to 1500 psi and 450 °F, Hydraulic and Pneumatic, and shall be used... |
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