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.
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Technical Standard
The purpose of this standard is set forth the desired location, arrangement and general requirements of aircraft circuit breakers and fuses. The recommendations of this standard apply to all civil...
The recommendations of this standard apply to all civil type multi-engine transport aircraft.
This design standard provides information on the use of self-locking shank nuts, thread sizes .164-36 thru .375-24, together with details of flange hole and abutment shoulder for their installation.
This design standard provides information on the use of self-locking shank nuts, thread sizes .1640-36 through .3750-24, together with details of flange hole and abutment shoulder for their installation.
This design standard provides information on the use of self-locking shank nuts, thread sizes .1640-36 thru .3750-24, together with details of flange hole and abutment shoulder for their installation.
This document covers the general requirements for hydraulic aircraft jacks. It can be applied to tripod, unipod, and axle jacks that may be used on open ramp areas as well...
This document covers the general requirements for hydraulic jacks as used on commercial aircraft. It can be applied to tripod, unipod, and axle jacks which may be used on open...
This document establishes standard gland dimensions for low pressure static radial O-ring seal applications and provides recommendations for modifying these glands in special applications. No provisions are made in this...
This document establishes techniques for validating that an aircraft station complies with the interface requirements delineated in MIL-STD-1760.
This document establishes techniques for validating that an Aircraft Station Interface (ASI) complies with the interface requirements delineated in MIL-STD-1760 Revision E.
This document establishes techniques for validating that an Aircraft Station Interface (ASI) complies with the interface requirements delineated in MIL-STD-1760B Notice 3. For validation of aircraft designed to MIL-STD-1760A Notice...
This document establishes techniques for validating that an Aircraft Station Interface (ASI) complies with the interface requirements delineated in MIL-STD-1760C. For validation of aircraft designed to MIL-STD-1760A Notice 2 AS4764...
This document is a guideline for format, structure and content for ground support equipment (GSE) technical manuals. This document focuses on requirements specific to the GSE industry and does not...
This document is a result of the desire for interoperability of modules on a Pi-Bus. This standard is a stand alone document that used the Very High Speed Integrated Circuit...
This document shall serve as a guide for format, style, and method of presentation for all material included in manufacturers' publications for ground support equipment (GSE). These requirements shall be...
This drawing specifies parts AS48014, AS48015, AS48016, AS48017, AS48018, AS48019, AS48020, AS48021, AS48022, AS48023, AS48024, AS48025, AS48026, AS48027, AS48028, AS48029, AS48030, AS48031, AS48032, AS48034, AS48036, AS48038, AS48040, AS48042, AS48044, AS48046,...
This drawing specifies parts AS48116, AS48117, AS48118, AS48119, AS48120, AS48121, AS48122, AS48123, AS48124, AS48125, AS48126, AS48127, AS48128, AS48129, AS48130, AS48131, AS48132, AS48134, AS48136, AS48138, AS48140, AS48142, AS48144, AS48146, AS48148, AS48150,...
This drawing specifies parts AS48218, AS48219, AS48220, AS48221, AS48222, AS48223, AS48224, AS48225, AS48226, AS48227, AS48228, AS48229, AS48230, AS48231, AS48232, AS48234, AS48236, AS48238, AS48240, AS48242, AS48244, AS48246, AS48248, AS48250, AS48252, AS48254,...
This drawing specifies parts AS48320, AS48321, AS48322, AS48323, AS48324, AS48325, AS48326, AS48327, AS48328, AS48329, AS48330, AS48331, AS48332, AS48334, AS48336, AS48338, AS48340, AS48342, AS48344, AS48346, AS48348, AS48350, AS48352, AS48354, AS48356, AS48358,...
This drawing specifies parts AS48405, AS48406, AS48407, AS48408, AS48409, AS48410, AS48411, AS48412, AS48413, AS48414, AS48415, AS48416, AS48417, AS48418, AS48419, AS48420, AS48421, AS48422, AS48423, AS48424, AS48425, AS48426, AS48427, AS48428, AS48429, AS48430,...
This drawing specifies parts AS48506, AS48507, AS48508, AS48509, AS48510, AS48511, AS48512, AS48513, AS48514, AS48515, AS48516, AS48517, AS48518, AS48519, AS48520, AS48521, AS48522, AS48523, AS48524, AS48525, AS48526, AS48527, AS48528, AS48529, AS48530, AS48531,...
This drawing specifies parts AS48607, AS48608, AS48609, AS48610, AS48611, AS48612, AS48613, AS48614, AS48615, AS48616, AS48617, AS48618, AS48619, AS48620, AS48621, AS48622, AS48623, AS48624, AS48625, AS48626, AS48627, AS48628, AS48629, AS48630, AS48631, AS48632,...
This drawing specifies parts AS48708, AS48709, AS48710, AS48711, AS48712, AS48713, AS48714, AS48715, AS48716, AS48717, AS48718, AS48719, AS48720, AS48721, AS48722, AS48723, AS48724, AS48725, AS48726, AS48727, AS48728, AS48729, AS48730, AS48731, AS48732, AS48734,...
This procurement specification covers bolts and screws made from a corrosion and heat resistant, age hardenable nickel base alloy of the type identified under the Unified Numbering System as UNS...
This procurement specification covers inserts made from A286 alloy of the type identified under the Unified Numbering System as UNS S66286, solid film lubricated with a piastic self locking device,...
This SAE Aerospace Standard (AS) covers batch qualification procedure for virgin and compounded polytetrafluoroethyl ene (PTFE) resins used for compression molding. AS9100 requires virgin and modified PTFE as a testing...
This SAE Aerospace Standard (AS) covers laboratory test methods required to evaluate nonflammable hydraulic fluids. The methods of testing and description of the equipment have been used typically for evaluating...
This SAE Aerospace Standard (AS) covers the general requirements for the design, manufacture, and test of Solid State Power Controllers (SSPCs) of both dc and ac ratings for use in...
This SAE Aerospace Standard (AS) covers variable speed, reversible 0.375 (3/8) in chuck battery powered drills, with removable, rechargeable battery pack, used for general maintenance and construction where a battery...
This SAE Aerospace Standard (AS) covers variable speed, reversible battery powered drills with removable, rechargeable battery pack and either 3/8 inch or \u00bd inch chuck used for general maintenance and...
This SAE Aerospace Standard (AS) covers water conditioning agents used to facilitate aqueous wet-method magnetic particle inspection.
This SAE Aerospace Standard (AS) establishes minimum requirements for eddy current inspection of circular holes in nonferrous, metallic, aircraft engine hardware with fasteners removed. The inspection is intended to be...
This SAE Aerospace Standard (AS) establishes minimum requirements for eddy current inspection of circular holes in nonferrous, metallic, low conductivity (less than 5% IACS) aircraft engine hardware with fasteners removed.
This SAE Aerospace Standard (AS) establishes the requirements for 37 degree flared tube fittings or machined internal cone fluid connection fittings for use with 37 degree external cone, spherical nose,...
This SAE Aerospace Standard (AS) establishes the requirements for 37 degree flared tube fittings or machined internal cone fluid connection fittings for use with 37 degree external cone, spherical nose...
This SAE Aerospace Standard (AS) establishes the requirements for 37° flared tube fittings or machined internal cone fluid connection fittings for use with 37° external cone, spherical nose and seal...
This SAE Aerospace Standard (AS) establishes the requirements for 37° flared tube or machined cone fluid connection fittings (see Section 6 ) for use in all types of fluid systems.
This SAE Aerospace Standard (AS) establishes the requirements for a grooved clamp coupling and flanges suitable for joining intermediate pressure and temperature ducting in aircraft pneumatic systems. The rigid coupling...
This SAE Aerospace Standard (AS) establishes the requirements for beaded fluid connection fittings (see Section 6 ) for use in all types of fluid systems.
This SAE Aerospace Standard (AS) establishes the requirements for fluid fittings that combine both 37 degree flared and pipe threaded connections for use in all types of fluid systems.
This SAE Aerospace Standard (AS) establishes the requirements for fluid fittings that combine both 37° flared and pipe threaded connections for use in all types of fluid systems.
This SAE Aerospace Standard (AS) establishes the requirements for fluid fittings that combine both beaded hose connections and 37 degree flared connections for use in all types of fluid systems.
This SAE Aerospace Standard (AS) establishes the requirements for fluid fittings that combine both beaded hose connections and 37° flared connections for use in all types of fluid systems.
This SAE Aerospace Standard (AS) establishes the requirements for fluid fittings that combine both beaded hose connections and pipe threaded connections for use in all types of fluid systems.
This SAE Aerospace Standard (AS) establishes the requirements for fluid fittings that combine both flanged fitting ends and beaded hose connections for use in all types of fluid systems.
This SAE Aerospace Standard (AS) establishes the requirements for fluid fittings that combine both flareless and pipe threaded connections for use in all types of fluid systems.
This SAE Aerospace Standard (AS) establishes the requirements for fluid fittings that combine both straight thread boss or flanged connections and 37 degree flared connections for use in all types...
This SAE Aerospace Standard (AS) establishes the requirements for fluid fittings that combine both straight thread boss or flanged connections and 37° flared connections for use in all types of...
This SAE Aerospace Standard (AS) establishes the requirements for fluid fittings that combine both straight thread port or flanged connections and 24° cone flareless connections for use in all types...
This SAE Aerospace Standard (AS) establishes the requirements for fluid fittings that combine both straight thread port or flanged connections, and 24 degree cone flareless connections for use in all...
This SAE Aerospace Standard (AS) establishes the requirements for pipe threaded fluid connection fittings (see Section 6 ) for use in all types of fluid systems.
This SAE Aerospace Standard (AS) establishes the requirements for straight threaded boss or flanged fluid connection fittings (see Section 6 ) for use in all types of fluid systems.
This SAE Aerospace Standard (AS) establishes the standard installation procedures and torque values for the AS short flareless hydraulic tube fittings in sizes -20 and -24, and parts listed in...
This SAE Aerospace Standard (AS) offers gland details for a 0.364 cross section gland (nominal 3/8 in) with proposed gland lengths for compression type seals with two backup rings over...
This SAE Aerospace Standard (AS) offers gland details for a 0.364 inch (9.246 mm) cross-section gland (nominal 3/8 inch) with proposed gland lengths for compression-type seals with two backup rings...
This SAE Aerospace Standard (AS) provides standardized gland (groove) design criteria and dimensions for elastomeric seal glands for static and dynamic applications. The glands have been specifically designed for applications...
This SAE Aerospace Standard (AS) provides standardized gland (groove) design criteria and dimensions for O-ring seal glands for static and dynamic applications, and other seals.
This SAE Aerospace Standard (AS) sets forth criteria for the selection and verification processes to be followed in providing tires that will be suitable for intended use on civil aircraft.
This SAE Aerospace Standard provides standardized gland (groove) design criteria and dimensions for elastomeric seal glands for static and dynamic applications. The glands have been specifically designed for applications using...
This specification covers minimum requirements for skid control equipment for use on all types and models of civil aircraft. It shall be the responsibility of the applicant (See Paragraph 5.1...
This specification establishes the procedure for installing hardened key types studs and inserts, eliminating the need for broaching key slots. It also defines the hole preparation necessary to install the...
This specification establishes the requirements for self-locking nuts, wrenching type (i.e., hexagon, double hexagon, and spline drive), made of a corrosion and heat resistant steel of the type identified under...
This standard covers minimum requirements for skid control equipment for use on all types and models of civil aircraft. It shall be the responsibility of the applicant to determine the...
This standard covers permanent marking intended to be easily and accurately read during the normal service life of the item and also covers temporary marking intended to provide legible identification...
This standard defines and controls marking methods on finished, semi-finished, and rough items.
This standard provides the following: a Definition of terms pertaining to marking. b Symbols for marking location. c Requirements and restrictions for permanent markings. d Types of marking methods. e...
This test method provides performance data on candidate insulation systems as a function of time and temperature. These data give engineering information on the wire insulation candidate relative to the...
To establish a specification for software input and output interfaces for condition monitoring and performance programs used to monitor equipment from multiple manufacturers. The purpose of standardizing these interfaces is...

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