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 |
|---|---|
| Amendment 1 of AS5756. | |
| Amendment 1 of AS5768/1A. | |
| Amendment 1 of AS58091. | |
| Amendment 2 of AS5756. | |
| No scope available. | |
| Technical Standard | |
| The primary function of this specification is to cover the general requirements for 28 VDC manual reset trip-free arc fault/thermal circuit breakers for use in aircraft electrical systems conforming to... | |
| The primary function of this specification is to cover the general requirements for manual reset trip-free arc fault/thermal circuit breakers for use in aircraft electrical systems conforming to MIL-STD-704. As... | |
| The primary function of this specification is to cover the general requirements of one-, two-, and three-phase (often referred to as poles) trip-free circuit breakers for use in aircraft electric... | |
| The primary function of this specification is to cover the general requirements of one-, two-, and three-pole trip-free circuit breakers for use in aircraft electric systems conforming to MIL-STD-704. As... | |
| The SAE Aerospace Information Report AIR5315 - Generic Open Architecture (GOA) defines "a framework to identify interface classes for applying open systems to the design of a specific hardware/software system."... | |
| The scope of this document is to: Provide a requirements document for RFID Tag Manufacturers to produce active RFID tags for the Aerospace industry. Identify the minimum performance requirements for... | |
| This aerospace specification defines the requirements for a threadless, flexible, conductive, self-bonding coupling assembly which, when installed on fixed cavity ferrules, provides a flexible, current carrying connection for joining tubing... | |
| This Aerospace Standard (AS) assures that new transport type aircraft will provide adequate visibility from the flight deck. Background - Prior to updating this AS, the committee re-evaluated flight deck... | |
| This Aerospace Standard (AS) covers scarf-cut polytetrafluoroethyl ene (PTFE) retainers (back-up rings) for use in static glands in accordance with AS5857. They are for use in hydraulic and pneumatic system... | |
| This Aerospace Standard specifies the inside diameters, cross-sections, tolerances, and size identification codes (dash numbers) for O-rings used in sealing applications and for straight thread tube fitting boss gaskets. The... | |
| This Common Interface Control Plan (CICP) establishes the methodology for developing, controlling and managing the technical interfaces between and within systems. The document is not intended to directly control any... | |
| This Common Interface Control Plan (CICP) establishes the methodology for developing, controlling, and managing the technical interfaces between and within systems. An interface defines the interaction at a defined point... | |
| This Core Specification is intended as a standardization document for the basic performance requirements for 5 cSt grade aircraft gas turbine engine lubricants. It will be subject to change to... | |
| This document addresses AS8879 thread inspection issues relating to selection, usage and capability of gages. It addresses the selection of calibrated measurement gages, the need for defined quality metrics, the... | |
| This document covers minimum performance standards for protective equipment used on the flight deck during rapid decompression (5 to 30 seconds) up to a maximum pressure altitude of 45000 feet. | |
| This document defines a quantified means of specifying a digital fiber optic link loss budget: Between end users and system integrators Between system integrators and subsystem suppliers Between subsystem suppliers... | |
| This document defines a set of standard application layer 2x interfaces called JAUS Core Services . JAUS Services provide the means for software entities in an unmanned system or system... | |
| This document defines a set of standard application layer interfaces called JAUS Core Services . JAUS Services provide the means for software entities in an unmanned system or system of... | |
| This document defines a set of standard application layer interfaces called JAUS Core Services. JAUS Services provide the means for software entities in an unmanned system or system of unmanned... | |
| This document defines a set of standard application layer interfaces called JAUS HMI Services. JAUS Services provide the means for software entities in an unmanned system or system of unmanned... | |
| This document defines a set of standard application layer interfaces called JAUS Mobility Services . JAUS Services provide the means for software entities in an unmanned system or system of... | |
| This document defines a set of standard application layer interfaces called JAUS Mobility Services. JAUS Services provide the means for software entities in an unmanned system or system of unmanned... | |
| This document defines the requirements for polytetrafluoroethyl ene (PTFE) lined, metallic braid reinforced, hose assembly suitable for use in 400 °F (204 °C), 5080 psi (35 000 kPa) aircraft hydraulic... | |
| This document defines the requirements for polytetrafluoroethyl ene (PTFE) lined, metallic braid reinforced, hose assembly suitable for use in 400 °F (204 °C), 5080 psi (35000 kPa) aircraft hydraulic systems. | |
| This document defines the requirements for polytetrafluoroethyl ene (PTFE) lined, para-aramid reinforced, hose assemblies suitable for use in 275 °F (135 °C), 5080 psi (35,000 kPa) aircraft hydraulic systems. NOTE:... | |
| This document defines the requirements for polytetrafluoroethyl ene (PTFE) lined, para-aramid reinforced, hose assemblies suitable for use in 275 °F (135 °C), 5080 psi (35000 kPa) aircraft hydraulic systems. | |
| This document defines the requirements for polytetrafluoroethyl ene (PTFE) lined, paraaramid reinforced, hose assemblies suitable for use in 275 °F (135 °C), 5080 psi (35,000 kPa) aircraft hydraulic systems. NOTE:... | |
| This document describes engineering requirements for installation of externally swaged fittings used in aerospace fluid systems. | |
| This document establishes test plans/procedures for the AS5643/1 Slash Sheet. The AS5643/1 Slash Sheet establishes guidelines for the use of IEEE Std 1394-2008 as a data bus network in military... | |
| This document establishes test plans/procedures for the AS5643/1 Slash Sheet. The AS5643/1 Slash Sheet establishes guidelines for the use of IEEE-1394b as a data bus network in military and aerospace... | |
| This document establishes the minimum requirements for an environmental test chamber, and test procedures to carry out anti-icing performance tests according to the current materials specification for aircraft deicing/anti-icing fluids. | |
| This document provides guidance for laser operators and aviation authorities to determine the performance criteria that laser hazard control measures shall meet for the operation of an outdoor laser system... | |
| This document provides requirements and guidance for laser proponents and aviation authorities to determine the criteria that laser hazard control measures shall meet for the operation of an outdoor laser... | |
| This drawing specifies parts AS56910, AS56911, AS56912, AS56913, AS56914, AS56915, AS56916, AS56917, AS56918, AS56919, AS56920, AS56921, AS56922, AS56923, AS56924, AS56925, AS56926, AS56927, AS56928, AS56929, AS56930, AS56931, AS56932, AS56934, AS56936, AS56938,... | |
| This drawing specifies parts AS57012, AS57013, AS57014, AS57015, AS57016, AS57017, AS57018, AS57019, AS57020, AS57021, AS57022, AS57023, AS57024, AS57025, AS57026, AS57027, AS57028, AS57029, AS57030, AS57031, AS57032, AS57034, AS57036, AS57038, AS57040, AS57042,... | |
| This drawing specifies parts AS57109, AS57110, AS57111, AS57112, AS57113, AS57114, AS57115, AS57116, AS57117, AS57118, AS57119, AS57120, AS57121, AS57122, AS57123, AS57124, AS57125, AS57126, AS57127, AS57128, AS57129, AS57130, AS57131, AS57132, AS57134, AS57136,... | |
| This drawing specifies parts AS57213, AS57214, AS57215, AS57216, AS57217, AS57218, AS57219, AS57220, AS57221, AS57222, AS57223, AS57224, AS57225, AS57226, AS57227, AS57228, AS57229, AS57230, AS57231, AS57232, AS57234, AS57236, AS57238, AS57240, AS57242, AS57244,... | |
| This drawing specifies parts AS57314, AS57315, AS57316, AS57317, AS57318, AS57319, AS57320, AS57321, AS57322, AS57323, AS57324, AS57325, AS57326, AS57327, AS57328, AS57329, AS57330, AS57331, AS57332, AS57334, AS57336, AS57338, AS57340, AS57342, AS57344, AS57346,... | |
| This drawing specifies parts AS57416, AS57417, AS57418, AS57419, AS57420, AS57421, AS57422, AS57423, AS57424, AS57425, AS57426, AS57427, AS57428, AS57429, AS57430, AS57431, AS57432, AS57434, AS57436, AS57438, AS57440, AS57442, AS57444, AS57446, AS57448, AS57450,... | |
| This drawing specifies parts AS57518, AS57519, AS57520, AS57521, AS57522, AS57523, AS57524, AS57525, AS57526, AS57527, AS57528, AS57529, AS57530, AS57531, AS57532, AS57534, AS57536, AS57538, AS57540, AS57542, AS57544, AS57546, AS57548, AS57550, AS57552, AS57554,... | |
| This drawing specifies parts AS57620, AS57621, AS57622, AS57623, AS57624, AS57625, AS57626, AS57627, AS57628, AS57629, AS57630, AS57631, AS57632, AS57634, AS57636, AS57638, AS57640, AS57642, AS57644, AS57646, AS57648, AS57650, AS57652, AS57654, AS57656, AS57658,... | |
| This drawing specifies parts AS57813, AS57814, AS57815, AS57816, AS57817, AS57818, AS57819, AS57820, AS57821, AS57822, AS57823, AS57824, AS57825, AS57826, AS57827, AS57828, AS57829, AS57830, AS57831, AS57832, AS57834, AS57836, AS57838, AS57840, AS57842, AS57844,... | |
| This drawing specifies parts AS57914, AS57915, AS57916, AS57917, AS57918, AS57919, AS57920, AS57921, AS57922, AS57923, AS57924, AS57925, AS57926, AS57927, AS57928, AS57929, AS57930, AS57931, AS57932, AS57934, AS57936, AS57938, AS57940, AS57942, AS57944, AS57946,... | |
| This drawing specifies parts AS58016, AS58017, AS58018, AS58019, AS58020, AS58021, AS58022, AS58023, AS58024, AS58025, AS58026, AS58027, AS58028, AS58029, AS58030, AS58031, AS58032, AS58034, AS58036, AS58038, AS58040, AS58042, AS58044, AS58046, AS58048, AS58050,... | |
| This drawing specifies parts AS58118, AS58119, AS58120, AS58121, AS58122, AS58123, AS58124, AS58125, AS58126, AS58127, AS58128, AS58129, AS58130, AS58131, AS58132, AS58134, AS58136, AS58138, AS58140, AS58142, AS58144, AS58146, AS58148, AS58150, AS58152, AS58154,... | |
| This drawing specifies parts AS58220, AS58221, AS58222, AS58223, AS58224, AS58225, AS58226, AS58227, AS58228, AS58229, AS58230, AS58231, AS58232, AS58234, AS58236, AS58238, AS58240, AS58242, AS58244, AS58246, AS58248, AS58250, AS58252, AS58254, AS58256, AS58258,... | |
| This drawing specifies parts AS58309, AS58310, AS58311, AS58312, AS58313, AS58314, AS58315, AS58316, AS58317, AS58318, AS58319, AS58320, AS58321, AS58322, AS58323, AS58324, AS58325, AS58326, AS58327, AS58328, AS58329, AS58330, AS58331, AS58332, AS58334, AS58336,... | |
| This drawing specifies parts AS58411, AS58412, AS58413, AS58414, AS58415, AS58416, AS58417, AS58418, AS58419, AS58420, AS58421, AS58422, AS58423, AS58424, AS58425, AS58426, AS58427, AS58428, AS58429, AS58430, AS58431, AS58432, AS58434, AS58436, AS58438, AS58440,... | |
| This drawing specifies parts AS58512, AS58513, AS58514, AS58515, AS58516, AS58517, AS58518, AS58519, AS58520, AS58521, AS58522, AS58523, AS58524, AS58525, AS58526, AS58527, AS58528, AS58529, AS58530, AS58531, AS58532, AS58534, AS58536, AS58538, AS58540, AS58542,... | |
| This drawing specifies parts AS58614, AS58615, AS58616, AS58617, AS58618, AS58619, AS58620, AS58621, AS58622, AS58623, AS58624, AS58625, AS58626, AS58627, AS58628, AS58629, AS58630, AS58631, AS58632, AS58634, AS58636, AS58638, AS58640, AS58642, AS58644, AS58646,... | |
| This drawing specifies parts AS58716, AS58717, AS58718, AS58719, AS58720, AS58721, AS58722, AS58723, AS58724, AS58725, AS58726, AS58727, AS58728, AS58729, AS58730, AS58731, AS58732, AS58734, AS58736, AS58738, AS58740, AS58742, AS58744, AS58746, AS58748, AS58750,... | |
| This drawing specifies parts AS58818, AS58819, AS58820, AS58821, AS58822, AS58823, AS58824, AS58825, AS58826, AS58827, AS58828, AS58829, AS58830, AS58831, AS58832, AS58834, AS58836, AS58838, AS58840, AS58842, AS58844, AS58846, AS58848, AS58850, AS58852, AS58854,... | |
| This drawing specifies parts AS58905, AS58906, AS58907, AS58908, AS58909, AS58910, AS58911, AS58912, AS58913, AS58914, AS58915, AS58916, AS58917, AS58918, AS58919, AS58920, AS58921, AS58922, AS58923, AS58924, AS58925, AS58926, AS58927, AS58928, AS58929, AS58930,... | |
| This drawing specifies parts AS59006, AS59007, AS59008, AS59009, AS59010, AS59011, AS59012, AS59013, AS59014, AS59015, AS59016, AS59017, AS59018, AS59019, AS59020, AS59021, AS59022, AS59023, AS59024, AS59025, AS59026, AS59027, AS59028, AS59029, AS59030, AS59031,... | |
| This drawing specifies parts AS59107, AS59108, AS59109, AS59110, AS59111, AS59112, AS59113, AS59114, AS59115, AS59116, AS59117, AS59118, AS59119, AS59120, AS59121, AS59122, AS59123, AS59124, AS59125, AS59126, AS59127, AS59128, AS59129, AS59130, AS59131, AS59132,... | |
| This drawing specifies parts AS59208, AS59209, AS59210, AS59211, AS59212, AS59213, AS59214, AS59215, AS59216, AS59217, AS59218, AS59219, AS59220, AS59221, AS59222, AS59223, AS59224, AS59225, AS59226, AS59227, AS59228, AS59229, AS59230, AS59231, AS59232, AS59234,... | |
| This drawing specifies parts AS59310, AS59311, AS59312, AS59313, AS59314, AS59315, AS59316, AS59317, AS59318, AS59319, AS59320, AS59321, AS59322, AS59323, AS59324, AS59325, AS59326, AS59327, AS59328, AS59329, AS59330, AS59331, AS59332, AS59334, AS59336, AS59338,... | |
| This drawing specifies parts AS59412, AS59413, AS59414, AS59415, AS59416, AS59417, AS59418, AS59419, AS59420, AS59421, AS59422, AS59423, AS59424, AS59425, AS59426, AS59427, AS59428, AS59429, AS59430, AS59431, AS59432, AS59434, AS59436, AS59438, AS59440, AS59442,... | |
| This drawing specifies parts AS59507, AS59508, AS59509, AS59510, AS59511, AS59512, AS59513, AS59514, AS59515, AS59516, AS59517, AS59518, AS59519, AS59520, AS59521, AS59522, AS59523, AS59524, AS59525, AS59526, AS59527, AS59528, AS59529, AS59530, AS59531, AS59532,... | |
| This drawing specifies parts AS59609, AS59610, AS59611, AS59612, AS59613, AS59614, AS59615, AS59616, AS59617, AS59618, AS59619, AS59620, AS59621, AS59622, AS59623, AS59624, AS59625, AS59626, AS59627, AS59628, AS59629, AS59630, AS59631, AS59632, AS59634, AS59636,... | |
| This drawing specifies parts AS59710, AS59711, AS59712, AS59713, AS59714, AS59715, AS59716, AS59717, AS59718, AS59719, AS59720, AS59721, AS59722, AS59723, AS59724, AS59725, AS59726, AS59727, AS59728, AS59729, AS59730, AS59731, AS59732, AS59734, AS59736, AS59738,... | |
| This drawing specifies parts AS59811, AS59812, AS59813, AS59814, AS59815, AS59816, AS59817, AS59818, AS59819, AS59820, AS59821, AS59822, AS59823, AS59824, AS59825, AS59826, AS59827, AS59828, AS59829, AS59830, AS59831, AS59832, AS59834, AS59836, AS59838, AS59840,... | |
| This drawing specifies parts AS59913, AS59914, AS59915, AS59916, AS59917, AS59918, AS59919, AS59920, AS59921, AS59922, AS59923, AS59924, AS59925, AS59926, AS59927, AS59928, AS59929, AS59930, AS59931, AS59932, AS59934, AS59936, AS59938, AS59940, AS59942, AS59944,... | |
| This drawing specifies parts AS60014, AS60015, AS60016, AS60017, AS60018, AS60019, AS60020, AS60021, AS60022, AS60023, AS60024, AS60025, AS60026, AS60027, AS60028, AS60029, AS60030, AS60031, AS60032, AS60034, AS60036, AS60038, AS60040, AS60042, AS60044, AS60046,... | |
| This interface standard applies to fuzes/fuzing systems (referred to as fuzing system hereafter) in airborne weapons that use a MIL-STD-1760 interface. It defines the powers, the discrete signals and the... | |
| This interface standard applies to fuzes/fuzing systems (referred to as fuzing system hereafter) in airborne weapons that use a MIL-STD-1760 type interface. It defines the powers, the discrete signals and... | |
| This procedure establishes the instructions to prepare tube ends and install and inspect axially swaged permanent tube fittings qualified to AS5958. This procedure is applicable when specified on the engineering... | |
| This procurement specification covers inserts made from A286 alloy (UNS S66286) which have self-locking internal threads and integrated locking keys to positively secure the insert against rotation when properly installed... | |
| This SAE Aerospace Specification (AS) is applicable to all aircraft. This AS defines the minimum design and operating requirements for the aircraft refueling interface. These requirements establish the minimum criteria... | |
| This SAE Aerospace Standard (AS) covers adjustable and non-adjustable spanner wrenches generally used for aerospace machinery maintenance and for tightening and loosening hose couplings and hydrant caps. Inclusion of dimensional... | |
| This SAE Aerospace Standard (AS) covers scarf-cut polytetrafluoroethyl ene (PTFE) retainers (back-up rings) for use in static glands in accordance with AS5857. They are for use in hydraulic and pneumatic... | |
| This SAE Aerospace Standard (AS) covers scarf-cut polytetrafluoroethyl ene (PTFE) retainers (backup rings) for use in glands in accordance with AS4716. They are for use in hydraulic and pneumatic system... | |
| This SAE Aerospace Standard (AS) covers sealed, self-aligning, anti-friction, rod end ball bearings with application in temperature ranges (1) -65 to 250 °F and (2) -65 to 300 °F with... | |
| This SAE Aerospace Standard (AS) covers solid polytetrafluoroethyl ene (PTFE) retainers (back-up rings) for use in static glands in accordance with AS5857. They are for use in hydraulic and pneumatic... | |
| This SAE Aerospace Standard (AS) covers solid, uncut polytetrafluoroethyl ene (PTFE) retainers (backup rings) for use in glands in accordance with AS4716. They are for use in hydraulic and pneumatic... | |
| This SAE Aerospace Standard (AS) covers the design, fabrication, performance, and testing requirements for general-purpose, base-restrained, containers requiring airworthiness approval for installation/use in aircraft lower deck compartments. See 10.1 and... | |
| This SAE Aerospace Standard (AS) defines implementation requirements for the electrical interface between: a Aircraft carried miniature store carriage systems and miniature stores b Aircraft parent carriage and miniature stores... | |
| This SAE Aerospace Standard (AS) defines the items that shall be considered when creating a fiber optic cable assembly specification and source control drawing intended for installation on aerospace platforms. | |
| This SAE Aerospace Standard (AS) defines the materials, apparatus and procedure for microscopic sizing and counting of particulate contamination of fluid power systems by membrane filtration using microscopic counting. | |
| This SAE Aerospace Standard (AS) defines the materials, apparatus and procedure for sizing and counting of particulate contamination, 5 μm or greater, in hydraulic fluid samples by membrane filtration with... | |
| This SAE Aerospace Standard (AS) describes taps, thread plug gages, inserting tools, expanding tools, offset and staking tools, tang break-off tools, extracting tools and thread repair kits. | |
| This SAE Aerospace Standard (AS) establishes the aerodynamic flow-off requirements and test procedures for AMS1424 Type I and AMS1428 Type II, III and IV fluids used to deice and/or anti-ice... | |
| This SAE Aerospace Standard (AS) establishes the aerodynamic flow-off requirements and test procedures for AMS1424 Type I and AMS1428 Type II, III, and IV fluids used to deice and/or anti-ice... | |
| This SAE Aerospace Standard (AS) establishes the aerodynamic flow-off requirements for SAE AMS 1424 Type I and SAE AMS 1428 Type II, III and IV fluids used to deice and/or... | |
| This SAE Aerospace Standard (AS) establishes the aerodynamic flow-off requirements for SAE AMS 1424 Type I and SAE AMS 1428 Type II, III and IV. Fluids used to deice and/or... | |
| This SAE Aerospace Standard (AS) establishes the general requirements for pressure compensated, variable delivery hydraulic pumps, suitable for use in commercial aircraft hydraulic systems. This document shall be used in... | |
| This SAE Aerospace Standard (AS) establishes the general requirements for the design, construction, acceptance and qualification test of pressure compensated, variable delivery hydraulic pumps, used in civil aircraft hydraulic systems. | |
| 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 civil aircraft... | |
| This SAE Aerospace Standard (AS) establishes the requirements and procedures for impulse testing of hose, tubing, and fitting assemblies for use in aerospace hydraulic systems of 8000 psi nominal operating... | |
| This SAE Aerospace Standard (AS) establishes the requirements for axially swaged titanium fittings on titanium, CRES, and aluminum tubing with flareless separable fitting ends for use in hydraulic supply and... | |
| This SAE Aerospace Standard (AS) establishes the requirements for externally swaged titanium tube fittings on titanium and CRES tubing with flareless separable fitting for use in hydraulic supply and return... | |
| This SAE Aerospace Standard (AS) establishes the requirements for externally swaged titanium tube fittings on titanium tubing with flareless separable fitting for use in hydraulic supply and return aerospace fluid... | |
| This SAE Aerospace Standard (AS) establishes the specification for TTP communication protocol functionality as a core networking component for design of synchronous, time-triggered distributed real-time communication networks. This document is... | |
| This SAE Aerospace Standard (AS) is applicable to military and commercial aircraft. It specifies the dimensions, tolerances and size codes (dash numbers) for use in glands per MIL-G-5514 where squeeze... | |
| This SAE Aerospace Standard (AS) prescribes requirements for the various types of nozzles that are used for the refueling and defueling of aircraft fitted with pressure fuel servicing systems. It... | |
| This SAE Aerospace Standard (AS) prescribes requirements for the various types of nozzles that are used for the refueling of aircraft fitted with pressure fuel servicing systems. It is to... | |
| This SAE Aerospace Standard (AS) prescribes the Minimum Performance Standards (MPS) for wheel, brake, and wheel and brake assemblies to be used on aircraft certificated under 14 CFR Parts 23,... | |
| This SAE Aerospace Standard (AS) provides general design and test requirements for a flat cut-off pressure compensated, variable delivery hydraulic pump for use in a civil aircraft hydraulic system with... | |
| This SAE Aerospace Standard (AS) provides standardized gland (groove) design criteria and dimensions for elastomeric seal glands for static applications. The glands have been specifically designed for applications using SAE... | |
| This SAE Aerospace Standard (AS) sets forth the minimum quality required for aircraft wheel and brake castings. Its use will establish minimum acceptable requirements for internal structure and surface conditions... | |
| This SAE Aerospace Standard (AS) specifies scarf-cut polytetrafluoroethyl ene (PTFE) retainers (backup rings) for use in glands in accordance with AS4716. They are usually used in hydraulic and pneumatic system... | |
| This SAE Aerospace Standard (AS) specifies scarf-cut polytetrafluoroethyl ene (PTFE) retainers (backup rings) for use in static glands in accordance with AS5857. They are usually for use in hydraulic and... | |
| This SAE Aerospace Standard (AS) specifies solid polytetrafluoroethyl ene (PTFE) retainers (backup rings) for use in static glands in accordance with AS5857. They are usually for use in hydraulic and... | |
| This SAE Aerospace Standard (AS) specifies solid, un-cut polytetrafluoroethyl ene (PTFE) retainers (backup rings) for use in glands in accordance with AS4716. They are usually used in hydraulic and pneumatic... | |
| This SAE Aerospace Standard (AS) specifies solid, uncut polytetrafluoroethyl ene (PTFE) retainers (backup rings) for use in glands in accordance with AS4716. They are usually used in hydraulic and pneumatic... | |
| This SAE Aerospace Standard (AS) specifies the dimensions, tolerances and size codes (dash numbers) for O-rings with a larger cross-section than those to AS568, for use in glands per MIL-G-5514... | |
| This SAE Aerospace Standard (AS) specifies the inside diameters, cross-sections, tolerances, and size identification codes (dash numbers) for O-rings used in sealing applications and for straight thread tube fitting boss... | |
| This SAE Aerospace Standard (AS)/Minimum Operational Performance Specification (MOPS) specifies the minimum performance requirements of remote on-ground ice detection systems (ROGIDS). These systems are ground based. They provide information that... | |
| This SAE Aerospace Standard (AS)/Minimum Operational Performance Specification (MOPS) specifies the minimum performance requirements of Remote On-Ground Ice Detection Systems (ROGIDS). These systems are ground-based. They provide information that indicates... | |
| This specification covers 600 V heavy duty, portable, power, single and multiconductor, electrical cable for severe flexing service (see detail specifications for voltage limitations). The AS5756 insulation system has been... | |
| This specification covers 600-volt heavy duty, portable, power, single and multiconductor, electrical cable for severe flexing service (see detail specifications for voltage limitations). | |
| This specification covers 600-volt heavy duty, portable, power, single and multiconductor, electrical cable for severe flexing service. | |
| This specification covers a corrosion resistant steel in the form of wire type identified under the Unified Numbering System as UNS S30500. | |
| This specification covers antifriction bellcrank ball bearings intended primarily for airframe use. | |
| This specification covers design requirements, performance requirements, and methods of procurement for tools and associated accessories used to strip aerospace vehicle electrical wire and cable. Aerospace vehicle electrical wire has... | |
| This specification covers general requirements for covers intended to protect the following aircraft parts: Cockpit Fuselage Canopy Engine Armament Propeller or Rotor Miscellaneous | |
| This specification covers heavy braid hose assemblies intended for use in high-temperature, 400°F (204°C, high-pressure, 3000 psi (210 bar) aircraft hydraulic systems, also for use in pneumatic systems which allow... | |
| This specification covers manual pressure-generating brake control units as defined by Specification MIL-H-5440. | |
| This specification covers sealed, self-aligning, anti-friction, rod end ball bearings with application in temperature ranges (1) −65°F to 250°F and (2) −65°F to 300°F with 20% reduction of dynamic load... | |
| This specification covers sealed, self-aligning, anti-friction, rod end ball bearings with application in temperature ranges (1) -65 °F to 250 °F and (2) -65 °F to 300 °F with 20%... | |
| This specification covers sealed, self-aligning, anti-friction, rod end ball bearings with application in temperature ranges (1) -65°F to 250°F and (2) -65°F to 300°F with 20% reduction of dynamic load... | |
| This specification covers the general requirements for aircraft slings used to lift and transport aircraft or aircraft components which may be bulky or fragile. | |
| This specification covers the requirements for the procurement of three types of puncturable-seal carbon dioxide filled cylinders. | |
| This specification defines basic physical, chemical, and performance limits for 5 cSt grades of gas turbine engine lubricating oils used in aero and aero-derived marine and industrial applications, along with... | |
| This specification establishes the common requirements and provides a guide for special requirements for variable delivery hydraulic pumps, suitable for use in civil aircraft. It also specifies the methods to... | |
| This specification establishes the common requirements for variable delivery electric motor driven, hydraulic pump units, suitable for use in aircraft hydraulic systems. | |
| This specification establishes the common requirements for variable delivery, hydraulic pumps, suitable for use in aircraft; and the methods to be used for demonstrating compliance with these requirements. | |
| This specification establishes the performance requirements for the identification of wire and cable by indirect markings that have been applied to electrical insulating materials including heat shrink sleeving, wrap around... | |
| This specification establishes the requirements for the following types of self-locking nuts in thread diameter sizes 0.1380 through 0.6250 inch: a Wrenching Nuts: i.e., hexagon, double hexagon, and spline nuts. | |
| This specification establishes the requirements for the following types of self-locking nuts in thread diameter sizes 0.1380 through 0.6250 inches: a Wrenching Nuts: i.e., hexagon, double hexagon and spline nuts. | |
| This specification presents the standard method for the proof testing and prestretching of aircraft cable assemblies. | |
| This standard defines implementation requirements for the electrical interface between: a aircraft carried miniature store carriage systems and miniature stores b aircraft parent carriage and miniature stores c surface based... | |
| This standard defines the requirements and characteristics of electrical power for spacecraft. This standard also defines analysis, verification, and testing methodologies to be used to ensure that the loads operate... | |
| THIS STANDARD ESTABLISHES THE DIMENSIONAL AND VISUAL QUALITY REQUIREMENTS, LOT REQUIREMENTS AND PACKAGING AND LABELING REQUIREMENTS FOR O-RINGS MOLDED FROM AMS7379 FLUOROCARBON (FKM) RUBBER. IT SHALL BE USED FOR PROCUREMENT... | |
| This standard only defines interconnect, electrical and logical (functional) requirements for the interface between a Micro Munition and the Host. The physical and mechanical interface between the Micro Munition and... | |
| This standard provides the following: a The required surface finish criteria for the designed function of the parts b The definition of surface imperfections and defects that affect surface quality... | |
| This standard sets forth the minimum quality required for aircraft wheel and brake castings. Its use will establish minimum acceptable requirements for internal structure and surface conditions and is predicated... | |
| This supplement forms a part of the Aerospace Standard AS5951, Hose Assembly, Polytrafluoroethyloe ne,Para-Aramid Reinforced, 5080 psi (35,000 kPa), 275°F (135°C), Aircraft Hydraulic Systems, and shall be used to identify... | |
| This supplement forms a part of the Aerospace Standard AS5960, Hose Assembly, Polytrafluoroethyloe ne, Metallic Braid Reinforced, 5080 psi (35,000 kPa), 400°F (204°C), Aircraft Hydraulic Systems, and shall be used... |
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