| Pos | standard Number | publication date | Language | Description | 
| 1 | SAE AS5878-2005 | 2005-06-01(R 2013) | English | Nut, Self-Locking, Nickel Alloy, UNS N07001, 1400 °F, 180,000 psi, UNJ Thread Procurement Specification | 
| 2 | SAE AS5182B-2005 | 2005-06-01(R 2013) | English | FITTING, ELBOW, 45 DEGREES, BULKHEAD, FLARED TO HOSE | 
| 3 | SAE ARP5007A-2005 | 2005-06-01(R 2012) | English | Development Process - Aerospace Fly-By-Wire Actuation System | 
| 4 | SAE AS5054A-2005 | 2005-06-01(R 2012) | English | Areas for Calculating Stress or Load Values for Externally and Internally Threaded Fasteners | 
| 5 | SAE AIR5875-2005 | 2005-06-01(R 2011) | English | Methodology for Investigation of Flight Control System Anomalies | 
| 6 | SAE ARP5293-2005 | 2005-06-01(R 2010) | English | Safety Considerations for Lasers Projected in the Navigable Airspace | 
| 7 | SAE AIR5642-2005 | 2005-06-01 | English | The Effect of Installation Power Losses on the Overall Performance of a Helicopter | 
| 8 | SAE ARP5007A-2005 | 2005-06-01 | English | Development Process - Aerospace Fly-By-Wire Actuation System | 
| 9 | SAE AIR5601-2005 | 2005-06-01 | English | A Guideline for Application of RF Photonics to Aerospace Platforms | 
| 10 | SAE J492-2005 | 2005-06-01 | English | (R) Guide for Rivet Selection and Design Consideration DoD Adopted
 | 
| 11 | SAE AS5182B-2005 | 2005-06-01 | English | Fitting, Elbow, 45 Degrees, Bulkhead, Flared to Hose DoD Adopted
 | 
| 12 | SAE AS5878-2005 | 2005-06-01 | English | Nut, Self-Locking, Nickel Alloy, UNS N07001, 1400 Degrees F, 180,000 psi, UNJ Thread Procurement Specification | 
| 13 | SAE AIR5642-2005 | 2005-06-01 | English | The Effect of Installation Power Losses on the Overall Performance of a Helicopter | 
| 14 | SAE AS5054A-2005 | 2005-06-01 | English | Areas for Calculating Stress or Load Values for Externally and Internally Threaded Fasteners | 
| 15 | SAE AMS3378A-2005 | 2005-06-01 | English | Sealant, Silicone, Two-Part, General Purpose Room Temperature Vulcanizing Non-Fuel Resistant | 
| 16 | SAE ARP5007A-2005 | 2005-06-01 | English | Development Process - Aerospace Fly-By-Wire Actuation System | 
| 17 | SAE USCAR-28-2005 | 2005-06-01 | English | Initiator Technical Requirements and Validation | 
| 18 | SAE J562-2005 | 2005-06-01 | English | Nonmetallic Loom | 
| 19 | SAE J306-2005 | 2005-06-01 | English | Automotive Gear Lubricant Viscosity Classification | 
| 20 | SAE J2683-2005 | 2005-06-01 | English | Refrigerant Purity and Container Requirements for Carbon Dioxide (CO2 R-744) Used in Mobile Air-Conditioning Systems | 
| 21 | SAE ARP9005-2005 | 2005-06-01 | English | Aerospace Guidance for Non-Deliverable Software | 
| 22 | SAE AS5054A-2005 | 2005-06-01 | English | Areas for Calculating Stress or Load Values for Externally and Internally Threaded Fasteners | 
| 23 | SAE AIR5875-2005 | 2005-06-01 | English | Methodology for Investigation of Flight Control System Anomalies | 
| 24 | SAE J2616-2005 | 2005-06-01 | English | Testing Performance of the Fuel Processor Subsystem of an Automotive Fuel Cell System | 
| 25 | SAE J651-2005 | 2005-06-01 | English | Passenger Car and Light Truck Automatic Transmission and Automatic Transaxle Test Code | 
| 26 | SAE AS7466B-2005 | 2005-06-01 | English | Bolts and Screws, Nickel Alloy, UNS N07718 Tensile Strength 185 ksi Fatigue Rated, Procurement Specification - UNS N07718 DoD Adopted
 | 
| 27 | SAE AIR1828B-2005 | 2005-06-01 | English | (R) Guide to Engine Lubrication System Monitoring | 
| 28 | SAE ARP24D-2005 | 2005-06-01 | English | (R) Determination of Hydraulic Pressure Drop DoD Adopted
 | 
| 29 | SAE AS5202A-2005 | 2005-05-01(R 2013) | English | PORT OR FITTING END, INTERNAL STRAIGHT THREAD, DESIGN STANDARD | 
| 30 | SAE AS85049/131-2005 | 2005-05-01(R 2011) | English | CONNECTOR ACCESSORIES, FIBER OPTIC BACKSHELL, STRAIGHT, SELF-LOCKING CATEGORY 3B FOR MIL-DTL-38999 SERIES III & SAE AS5590/1 CONNECTORS | 
| 31 | SAE AS85049/133-2005 | 2005-05-01(R 2011) | English | CONNECTOR ACCESSORIES, FIBER OPTIC BACKSHELL, 90°, SELF-LOCKING CATEGORY 3B FOR MIL-DTL-38999 SERIES III & SAE AS5590/1 CONNECTORS | 
| 32 | SAE AS4059E-2005 | 2005-05-01(R 2011) | English | (R) Aerospace Fluid Power - Cleanliness Classification for Hydraulic Fluids DoD Adopted
 | 
| 33 | SAE ARP1786B-2005 | 2005-05-01(R 2010) | English | (R) Wheel Roll on Rim Criteria for Aircraft Application | 
| 34 | SAE ARP5600-2005 | 2005-05-01(R 2010) | English | Disposition of Damaged Wheels Involved in Accidents/Incidents | 
| 35 | SAE AS5202A-2005 | 2005-05-01 | English | PORT OR FITTING END, INTERNAL STRAIGHT THREAD, DESIGN STANDARD DoD Adopted
 | 
| 36 | SAE AMS4750D-2005 | 2005-05-01 | English | Solder, Tin-Lead 45Sn - 55Pb DoD Adopted
 | 
| 37 | SAE AMS4751C-2005 | 2005-05-01 | English | Tin - Lead Eutectic 63Sn - 37Pb - UNS L13630 | 
| 38 | SAE AS4059E-2005 | 2005-05-01 | English | (R) Aerospace Fluid Power - Cleanliness Classification for Hydraulic Fluids DoD Adopted
 | 
| 39 | SAE AMS4434L-2005 | 2005-05-01 | English | Magnesium Alloy Castings, Sand 9.0Al - 2.0Zn (AZ92-T6) Solution and Precipitation Heat Treated | 
| 40 | SAE AS85049/133-2005 | 2005-05-01 | English | CONNECTOR ACCESSORIES, FIBER OPTIC BACKSHELL, 90°, SELF-LOCKING CATEGORY 3B FOR MIL-DTL-38999 SERIES III & SAE AS5590/1 CONNECTORS | 
| 41 | SAE AIR5788-2005 | 2005-05-01 | English | Common Launch Acceptability Region (CLAR) Truth Data Generator Interface Control Document (ICD) for the CLAR Approach (CLARA) | 
| 42 | SAE ARP9162-2005 | 2005-05-01 | English | Aerospace Operator Self-Verification Programs | 
| 43 | SAE ARP5600-2005 | 2005-05-01 | English | Disposition of Damaged Wheels Involved in Accidents/Incidents | 
| 44 | SAE AS85049/131-2005 | 2005-05-01 | English | CONNECTOR ACCESSORIES, FIBER OPTIC BACKSHELL, STRAIGHT, SELF-LOCKING CATEGORY 3B FOR MIL-DTL-38999 SERIES III & SAE AS5590/1 CONNECTORS | 
| 45 | SAE J1776-2005 | 2005-05-01 | English | (R) Marine VehiclesHydraulic PumpsDesign and Specification Guide DoD Adopted
 | 
| 46 | SAE J1787-2005 | 2005-05-01 | English | Measurement of the Total Ash Content of Aviation Piston Engine Oils by a Calculation Method | 
| 47 | SAE J1796-2005 | 2005-05-01 | English | Spectral Transmission Test | 
| 48 | SAE AS85049/131-2005 | 2005-05-01 | English | CONNECTOR ACCESSORIES, FIBER OPTIC BACKSHELL, STRAIGHT, SELF-LOCKING CATEGORY 3B FOR MIL-DTL-38999 SERIES III & SAE AS5590/1 CONNECTORS - FSC 5935 | 
| 49 | SAE AS39631A-2005 | 2005-05-01 | English | Universal Joint, Antifriction Bearings | 
| 50 | SAE J2051-2005 | 2005-05-01 | English | Qualifications for Four-Way Subbase Mounted Air Valves for Automotive Manufacturing Applications | 
| 51 | SAE AS85049/133-2005 | 2005-05-01 | English | CONNECTOR ACCESSORIES, FIBER OPTIC BACKSHELL, 90掳, SELF-LOCKING CATEGORY 3B FOR MIL-DTL-38999 SERIES III & SAE AS5590/1 CONNECTORS - FSC 5935 | 
| 52 | SAE AMS2759/11-2005 | 2005-04-01(R 2014) | English | Stress Relief of Steel Parts | 
| 53 | SAE AS4751-2005 | 2005-04-01(R 2013) | English | Coupling Assembly, V-Band Sheet Metal Wide Flange, Pneumatic Tube | 
| 54 | SAE AS4751/2-2005 | 2005-04-01(R 2013) | English | FLANGE, SHEET METAL, WIDE | 
| 55 | SAE AS4751/3-2005 | 2005-04-01(R 2013) | English | FLANGE END, SOLID, WIDE DESIGN STANDARD | 
| 56 | SAE AS4751/1-2005 | 2005-04-01(R 2013) | English | COUPLING, SHEET METAL, 40° V-BAND, WIDE, STANDARD LATCH | 
| 57 | SAE AS24333B-2005 | 2005-04-01(R 2013) | English | COUPLING ASSEMBLY, HYDRAULIC, SELF-SEALING, QUICK DISCONNECT, FLARED FITTING TO INTERNAL THREAD BOSS | 
| 58 | SAE AS24334B-2005 | 2005-04-01(R 2013) | English | COUPLING ASSEMBLY, HYDRAULIC, SELF-SEALING, FLARELESS FITTING TO INTERNAL THREAD BOSS | 
| 59 | SAE ARP1328B-2005 | 2005-04-01(R 2012) | English | Aircraft Ground Support Equipment - Wind Stability Determination | 
| 60 | SAE AS9885A-2005 | 2005-04-01(R 2012) | English | BOLT, MACHINE - DOUBLE HEXAGON EXTENDED WASHER HEAD, PD SHANK, CORROSION AND HEAT RESISTANT STEEL, UNS S41800, 140 KSI MIN, .1900-32 UNJF-3A | 
| 61 | SAE AMS5932B-2005 | 2005-04-01(R 2012) | English | Steel, Corrosion and Heat-Resistant, Bars, Forgings and Tubing 14.5Cr - 2.3Ni - 12.5Co - 4.0Mo - 0.60V - 0.03Cb(Nb) Carburizing, Premium Aircraft-Quality, Double Vacuum Melted - UNS S42640 | 
| 62 | SAE AMS4203C-2005 | 2005-04-01(R 2012) | English | Aluminum Alloy, Plate 6.2Zn - 1.8Cu - 2.4Mg - 0.13Zr (7010-T7351) Solution Heat Treated, Stress Relieved, and Precipitation Heat Treated - UNS A97010 DoD Adopted
 | 
| 63 | SAE AS9566A-2005 | 2005-04-01(R 2012) | English | BOLT, MACHINE - DOUBLE HEXAGON EXTENDED WASHER HEAD, DRILLED, PD SHANK, CRES UNS S66286, 130 KSI MIN .2500-28 UNJF-3A | 
| 64 | SAE AS9564A-2005 | 2005-04-01(R 2012) | English | SCREW, MACHINE - DOUBLE HEXAGON EXTENDED WASHER HEAD, DRILLED, PD SHANK, CRES UNS S66286, 130 KSI MIN .1640-36 UNJF-3A | 
| 65 | SAE AMS4250A-2005 | 2005-04-01(R 2012) | English | Aluminum Alloy, Plate 8.1Zn - 2.3Mg - 1.0Cu - Zr (7449-T7651) Solution Heat Treated, Stress Relieved, and Overaged - UNS A97449 | 
| 66 | SAE AIR36105-2005 | 2005-04-01(R 2011) | English | Air Cargo Unit Load Devices - Reference Standards | 
| 67 | SAE AMS6522C-2005 | 2005-04-01(R 2011) | English | Steel Plate 2.0Cr - 10Ni - 14Co - 1.0Mo (0.13 - 0.17C) Vacuum Melted, Normalized, and Overaged - UNS K92571 | 
| 68 | SAE AMS6533C-2005 | 2005-04-01(R 2011) | English | Steel, Welding Wire 2.0Cr - 10Ni - 14Co - 1.0Mo - (0.13 - 0.17C) Vacuum Melted, Environment Controlled Packaging - UNS K92571 DoD Adopted
 | 
| 69 | SAE ARP5936-2005 | 2005-04-01(R 2010) | English | Landing Gear Storage | 
| 70 | SAE AMS6527D-2005 | 2005-04-01(R 2009) | English | Steel, Bars and Forgings 2.0Cr - 10Ni - 14Co - 1.0Mo (0.15 - 0.19C) Vacuum Melted, Normalized and Overaged - UNS K92571 DoD Adopted
 | 
| 71 | SAE AMS6362F-2005 | 2005-04-01(R 2009) | English | Steel Tubing, Seamless 0.95Cr - 0.20Mo (0.28 - 0.33C) (SAE 4130) 150 ksi (1034 MPa) Tensile Strength - UNS G41300 DoD Adopted
 | 
| 72 | SAE AS7108/2A-2005 | 2005-04-01 | English | National Aerospace and Defense Contractors Accreditation Program Requirements for Etch Processes (Macrostructure, Nital, Temper, Blue Etch Anodize) | 
| 73 | SAE ARP5936-2005 | 2005-04-01 | English | Landing Gear Storage | 
| 74 | SAE AS9885A-2005 | 2005-04-01 | English | (R) BOLT, MACHINE - DOUBLE HEXAGON EXTENDED WASHER HEAD, PD SHANK, CORROSION AND HEAT RESISTANT STEEL, UNS S41800, 140 KSI MIN, .1900-32 UNJF-3A DoD Adopted
 | 
| 75 | SAE J2312-2005 | 2005-04-01 | English | Automatic Transmission Intake Filter Test Procedure | 
| 76 | SAE AIR36105-2005 | 2005-04-01 | English | Air Cargo Unit Load Devices - Reference Standards | 
| 77 | SAE ARP4926A-2005 | 2005-04-01 | English | Alloy Verification and Chemical Composition Inspection of Welding Wire | 
| 78 | SAE J3046-1-2005 | 2005-04-01 | English | Reciprocating Internal Combustion EnginesPerformance Part 1: Standard Reference Conditions, Declarations of Power, Fuel and Lubricating Oil Consumptions, and Test Methods | 
| 79 | SAE AS121501 THRU AS121525A-2005 | 2005-04-01 | English | (R) NUT, PLAIN - HEXAGON, STEEL UNS G87400, CADMIUM PLATED, 125 KSI MIN. | 
| 80 | SAE AMS6533C-2005 | 2005-04-01 | English | Steel, Welding Wire 2.0Cr - 10Ni - 14Co - 1.0Mo - (0.13 - 0.17C) Vacuum Melted, Environment Controlled Packaging - UNS K92571 | 
| 81 | SAE AMS6533C-2005 | 2005-04-01 | English | Steel, Welding Wire 2.0Cr - 10Ni - 14Co - 1.0Mo - (0.13 - 0.17C) Vacuum Melted, Environment Controlled Packaging - UNS K92571 DoD Adopted
 | 
| 82 | SAE AS4751/1-2005 | 2005-04-01 | English | COUPLING, SHEET METAL, 40 DEGREES V-BAND, WIDE, STANDARD LATCH - FSC 5342 | 
| 83 | SAE AMS5388H-2005 | 2005-04-01 | English | Nickel Alloy, Corrosion and Heat-Resistant, Investment Castings 53.3Ni - 16.5Cr - 17Mo - 4.5W - 5.8Fe - 0.40V (CW-12MW) As-Cast - UNS N10002 DoD Adopted
 | 
| 84 | SAE AS4751/2-2005 | 2005-04-01 | English | FLANGE, SHEET METAL, WIDE - FSC 5342 | 
| 85 | SAE ARP5936-2005 | 2005-04-01 | English | Landing Gear Storage | 
| 86 | SAE AS24334B-2005 | 2005-04-01 | English | Coupling Assembly, Hydraulic, Self-Sealing, Flareless Fitting to Internal Thread Boss | 
| 87 | SAE AS24333B-2005 | 2005-04-01 | English | Coupling Assembly, Hydraulic, Self-Sealing, Quick Disconnect, Flared Fitting to Internal Thread Boss | 
| 88 | SAE AMS5932B-2005 | 2005-04-01 | English | Steel, Corrosion and Heat-Resistant, Bars, Forgings and Tubing 14.5Cr - 2.3Ni - 12.5Co - 4.0Mo - 0.60V - 0.03Cb(Nb) Carburizing, Premium Aircraft-Quality, Double Vacuum Melted - UNS S42640 | 
| 89 | SAE AMS4203C-2005 | 2005-04-01 | English | Aluminum Alloy, Plate 6.2Zn - 1.8Cu - 2.4Mg - 0.13Zr (7010-T7351) Solution Heat Treated, Stress Relieved, and Precipitation Heat Treated (UNS A97010) DoD Adopted
 | 
| 90 | SAE AMS4250A-2005 | 2005-04-01 | English | Aluminum Alloy, Plate 8.1Zn - 2.3Mg - 1.0Cu - Zr (7449-T7651) Solution Heat Treated, Stress Relieved, and Overaged - UNS A97449 | 
| 91 | SAE AMS2308A-2005 | 2005-04-01 | English | Magnetic Rubber Inspection | 
| 92 | SAE J756-2005 | 2005-04-01 | English | Marine Propeller-Shaft Couplings | 
| 93 | SAE AS9564A-2005 | 2005-04-01 | English | R) SCREW, MACHINE - DOUBLE HEXAGON EXTENDED WASHER HEAD, DRILLED, PD SHANK, CRES UNS S66286, 130 KSI MIN .1640-36 UNJF-3A DoD Adopted
 | 
| 94 | SAE AS4751/3-2005 | 2005-04-01 | English | FLANGE END, SOLID, WIDE DESIGN STANDARD - FSC 5342 | 
| 95 | SAE AMS4203C-2005 | 2005-04-01 | English | Aluminum Alloy, Plate 6.2Zn - 1.8Cu - 2.4Mg - 0.13Zr (7010-T7351) Solution Heat Treated, Stress Relieved, and Precipitation Heat Treated - UNS A97010 | 
| 96 | SAE AS9566A-2005 | 2005-04-01 | English | R) BOLT, MACHINE - DOUBLE HEXAGON EXTENDED WASHER HEAD, DRILLED, PD SHANK, CRES UNS S66286, 130 KSI MIN .2500-28 UNJF-3A DoD Adopted
 | 
| 97 | SAE AMS6522C-2005 | 2005-04-01 | English | Steel Plate 2.0Cr - 10Ni - 14Co - 1.0Mo (0.13 - 0.17C) Vacuum Melted, Normalized, and Overaged - UNS K92571 | 
| 98 | SAE AMS3284A-2005 | 2005-04-01 | English | Sealing Compound, Low Adhesion, for Removable Panels and Fuel Tank Inspection Plates | 
| 99 | SAE AMS2759/11-2005 | 2005-04-01 | English | Stress Relief of Steel Parts | 
| 100 | SAE ARP1328B-2005 | 2005-04-01 | English | Aircraft Ground Support Equipment - Wind Stability Determination | 
| 101 | SAE AS4751-2005 | 2005-04-01 | English | Coupling Assembly, V-Band Sheet Metal Wide Flange, Pneumatic Tube | 
| 102 | SAE J1766-2005 | 2005-04-01 | English | (R) Recommended Practice for Electric and Hybrid Electric Vehicle Battery Systems Crash Integrity Testing | 
| 103 | SAE J1532-2005 | 2005-03-01(R 2014) | English | (R) Transmission Oil Cooler Hose | 
| 104 | SAE AS4851A-2005 | 2005-03-01(R 2012) | English | Relative Thermal Life and Temperature Index for Insulated Electric Wire | 
| 105 | SAE AS9464C-2005 | 2005-03-01(R 2012) | English | PIN, STRAIGHT, HEADED, .248 DIAMETER, CRES, UNS S66286 | 
| 106 | SAE AMS4249A-2005 | 2005-03-01(R 2012) | English | Aluminum Alloy Castings 7.0Si - 0.58Mg - 0.15Ti - 0.06Be (D357.0-T6) Solution and Precipitation Heat Treated (Requiring Fatigue and Fracture Toughness Testing) - UNS A43570 | 
| 107 | SAE AMS4210K-2005 | 2005-03-01(R 2012) | English | Aluminum Alloy, Castings 5.0Si - 1.2Cu - 0.50Mg (355.0-T51) Precipitation Heat Treated - UNS A03550 | 
| 108 | SAE AMS4252B-2005 | 2005-03-01(R 2012) | English | Aluminum Alloy, Plate 6.4Zn - 2.4Mg - 2.2Cu - 0.12Zr (7150-T7751) Solution Heat Treated, Stress Relieved, and Overaged - UNS A97150 | 
| 109 | SAE AMS4255B-2005 | 2005-03-01(R 2012) | English | Aluminum Allloy, Clad One Side Sheet 0.6Mg - 0.35Si - 0.28Cu (No. 21 Brazing Sheet) As Fabricated - UNS A86951 | 
| 110 | SAE AMS4256B-2005 | 2005-03-01(R 2012) | English | Aluminum Alloy, Clad Two Sides Sheet 0.6Mg - 0.35Si - 0.28Cu (No. 22 Brazing Sheet) As Fabricated - UNS A86951 | 
| 111 | SAE AMS4345B-2005 | 2005-03-01(R 2012) | English | Aluminum Alloy, Extrusions 6.4Zn - 2.4Mg - 2.2Cu - 0.12Zr (7150-T77511) Solution Heat Treated, Stress-Relieved, Straightened, and Overaged - UNS A97150 | 
| 112 | SAE AS9600A-2005 | 2005-03-01(R 2012) | English | BRACKET, ANGLE, 90°, CORROSION AND HEAT RESISTANT STEEL UNS S41000, .190 BOLT | 
| 113 | SAE AS36102-2005 | 2005-03-01(R 2011) | English | Air Cargo Unit Load Devices - Testing Methods | 
| 114 | SAE AIR1609A-2005 | 2005-03-01(R 2010) | English | (R) Aircraft Humidification | 
| 115 | SAE AMS-S-8802B-2005 | 2005-03-01 | English | Sealing Compound, Temperature Resistant, Integral Fuel Tanks and Fuel Cell Cavities, High Adhesion DoD Adopted
 | 
| 116 | SAE J2376-2005 | 2005-03-01 | English | New-Vehicle Collision Repair Information | 
| 117 | SAE AMS4256B-2005 | 2005-03-01 | English | Aluminum Alloy, Clad Two Sides Sheet 0.6Mg - 0.35Si - 0.28Cu (No. 22 Brazing Sheet) As Fabricated - UNS A86951 | 
| 118 | SAE AS20708/94A-2005 | 2005-03-01 | English | Synchro, 60 and 400 Hz, Size 23 | 
| 119 | SAE J47-2005 | 2005-03-01 | English | Maximum Sound Level Potential for Motorcycles | 
| 120 | SAE J1698-1-2005 | 2005-03-01 | English | Vehicle Event Data InterfaceOutput Data Definition | 
| 121 | SAE AS36102-2005 | 2005-03-01 | English | Air Cargo Unit Load Devices - Testing Methods | 
| 122 | SAE ARP5596A-2005 | 2005-03-01 | English | Cargo Shoring Guidelines | 
| 123 | SAE AS4851A-2005 | 2005-03-01 | English | Relative Thermal Life and Temperature Index for Insulated Electric Wire | 
| 124 | SAE J1685-2005 | 2005-03-01 | English | Classification System for Automotive Acrylonitrile/Butadiene/Styrene (ABS) and ABS + Polycarbonate Blends (ABS+PC) Based Plastics | 
| 125 | SAE AS9598A-2005 | 2005-03-01 | English | (R) BRACKET, ANGLE 90掳, CADMIUM PLATED, ALLOY STEEL UNS G41300, .190 X .312 BOLT DoD Adopted
 | 
| 126 | SAE AMS4255B-2005 | 2005-03-01 | English | Aluminum Alloy, Clad One Side Sheet 0.6Mg - 0.35Si - 0.28Cu (No. 21 Brazing Sheet) As Fabricated - UNS A86951 | 
| 127 | SAE AS9599A-2005 | 2005-03-01 | English | (R) BRACKET, ANGLE 90掳, CADMIUM PLATED, ALLOY STEEL UNS G41300, .190 X .375 BOLT DoD Adopted
 | 
| 128 | SAE AS4851A-2005 | 2005-03-01 | English | Relative Thermal Life and Temperature Index for Insulated Electric Wire | 
| 129 | SAE AS9600A-2005 | 2005-03-01 | English | (R) BRACKET, ANGLE 90掳, CORROSION AND HEAT RESISTANT STEEL UNS S41000, .190 BOLT DoD Adopted
 | 
| 130 | SAE AMS4252B-2005 | 2005-03-01 | English | Aluminum Alloy, Plate 6.4Zn - 2.4Mg - 2.2Cu - 0.12Zr (7150-T7751) Solution Heat Treated, Stress Relieved, and Overaged - UNS A97150 | 
| 131 | SAE ARP5638-2005 | 2005-03-01 | English | RMS Terms and Definitions | 
| 132 | SAE USCAR-1-2005 | 2005-03-01 | English | SALT SPRAY TESTING AND EVALUATION OF FASTENER FINISHES - Revision 1 | 
| 133 | SAE AIR1609A-2005 | 2005-03-01 | English | (R) Aircraft Humidification | 
| 134 | SAE J1981-2005 | 2005-03-01 | English | Road Hazard Impact Test for Wheel and Tire Assemblies (Passenger Car, Light Truck, and Multipurpose Vehicles) | 
| 135 | SAE AMS4210K-2005 | 2005-03-01 | English | Aluminum Alloy, Castings 5.0Si - 1.2Cu - 0.50Mg (355.0-T51) Precipitation Heat Treated - UNS A03550 | 
| 136 | SAE AMS4345B-2005 | 2005-03-01 | English | Aluminum Alloy, Extrusions 6.4Zn - 2.4Mg - 2.2Cu - 0.12Zr (7150-T77511) Solution Heat Treated, Stress-Relieved, Straightened, and Overaged - UNS A97150 | 
| 137 | SAE AMS4249A-2005 | 2005-03-01 | English | Aluminum Alloy Castings 7.0Si - 0.58Mg - 0.15Ti - 0.06Be (D357.0-T6) Solution and Precipitation Heat Treated (Requiring Fatigue and Fracture Toughness Testing) - UNS A43570 | 
| 138 | SAE J1532-2005 | 2005-03-01 | English | (R) Transmission Oil Cooler Hose | 
| 139 | SAE J1403-2005 | 2005-03-01 | English | Vacuum Brake Hose | 
| 140 | SAE ARP5416-2005 | 2005-03-01 | English | Aircraft Lightning Test Methods | 
| 141 | SAE AS9464C-2005 | 2005-03-01 | English | (R) PIN, STRAIGHT, HEADED, .248 DIAMETER, CRES, UNS S66286 DoD Adopted
 | 
| 142 | SAE J398-2005 | 2005-03-01 | English | (R) Rated (Advertised) Fuel CapacityPassenger Car, Multi-Purpose Passenger Vehicles, and Light Duty Trucks | 
| 143 | SAE ARP5637-2005 | 2005-03-01 | English | Design and Maintenance Considerations For Aircraft Exterior Lighting Plastic Lenses | 
| 144 | SAE AS9111W-2005 | 2005-02-22 | English | Quality Management System Assessment for Maintenance Organizations (Based on ISO 9001:2000) Word Format - See Also SAE AS9111; Includes Access to Additional Content | 
| 145 | SAE AS1214B-2005 | 2005-02-01(R 2018) | English | (R) Minimum Standards for Valve, High Pressure Oxygen, Line Shut Off, Manually Operated | 
| 146 | SAE AS1214B-2005 | 2005-02-01(R 2013) | English | (R) Minimum Standards for Valve, High Pressure Oxygen, Line Shut Off, Manually Operated | 
| 147 | SAE ARP5533-2005 | 2005-02-01(R 2013) | English | Stationary Runway Weather Information System (In-Pavement) | 
| 148 | SAE AMS4084D-2005 | 2005-02-01(R 2012) | English | (R) Aluminum Alloy Sheet 5.7Zn - 2.2Mg - 1.6Cu - 0.22Cr (7475-T61) Solution and Precipitation Heat Treated - UNS A97475 | 
| 149 | SAE AIR4175A-2005 | 2005-02-01(R 2012) | English | (R) A Guide to the Development of a Ground Station for Engine Condition Monitoring | 
| 150 | SAE ARP5414A-2005 | 2005-02-01(R 2012) | English | Aircraft Lightning Zone | 
| 151 | SAE AMS4200B-2005 | 2005-02-01(R 2012) | English | Aluminum Alloy Plate 7.7Zn - 2.4Mg - 1.6Cu - 0.16Cr (7049-T7351) Solution Heat Treated, Stress Relieved, and Precipitation Heat Treated - UNS A97049 DoD Adopted
 | 
| 152 | SAE AMS4314D-2005 | 2005-02-01(R 2012) | English | Aluminum Alloy Rings, Rolled or Forged 4.5Cu - 0.85Si - 0.80Mn - 0.50Mg (2014-T651, 2014-T652) Solution Heat Treated, Mechanically Stress Relieved, and Precipitation Heat Treated - UNS A92014 DoD Adopted
 | 
| 153 | SAE AS3507B-2005 | 2005-02-01(R 2012) | English | Insert -Thin Wall , Self-Locking Short and Long Length Installation and Removal of | 
| 154 | SAE AIR4766/2-2005 | 2005-02-01(R 2011) | English | Airborne Chemicals in Aircraft Cabins | 
| 155 | SAE AIR4766/1-2005 | 2005-02-01(R 2011) | English | Air Quality for Commercial Aircraft Cabin Particulate Contaminants | 
| 156 | SAE AIR1277B-2005 | 2005-02-01(R 2010) | English | (R) Cooling of Military Avionic Equipment | 
| 157 | SAE AS1219A-2005 | 2005-02-01(R 2010) | English | Aircraft Oxygen Replenishment Coupling for Civil Transport Aircraft (Design Standard) | 
| 158 | SAE AS1214B-2005 | 2005-02-01(R 2008) | English | (R) Minimum Standards for Valve, High Pressure Oxygen, Line Shut Off, Manually Operated | 
| 159 | SAE MA2051B-2005 | 2005-02-01 | English | (R) FITTING ASSEMBLY, TEE, THIN WALL, RETAINED NUT ON SIDE, FLARELESS, METRIC | 
| 160 | SAE AS9111-2005 | 2005-02-01 | English | Quality Management System Assessment for Maintenance Organizations (Based on ISO 9001:2000) | 
| 161 | SAE AS9132A-2005 | 2005-02-01 | English | (R) Data Matrix Quality Requirements for Parts Marking | 
| 162 | SAE MA2085B-2005 | 2005-02-01 | English | HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, CRES REINFORCED, 204 ⁰C, 21,000 KPA, 60-DEG CONE, TO 90-DEG TO 90-DEG, LIGHTWEIGHT, METRIC | 
| 163 | SAE MA2051B-2005 | 2005-02-01 | English | (R) FITTING ASSEMBLY, TEE, THIN WALL, RETAINED NUT ON SIDE, FLARELESS, METRIC | 
| 164 | SAE MA2126B-2005 | 2005-02-01 | English | Hose Assembly, Polytetrafluoroethylene (PTFE), up to 232 °C and 10 500 kPa Procurement Specification, Metric (ISO/DIS 10502) | 
| 165 | SAE AIR1277B-2005 | 2005-02-01 | English | (R) Cooling of Military Avionic Equipment | 
| 166 | SAE MA2050B-2005 | 2005-02-01 | English | (R) FITTING ASSEMBLY, ELBOW, 90⁰, THIN WALL, RETAINED NUT, FLARELESS, METRIC | 
| 167 | SAE AIR4175A-2005 | 2005-02-01 | English | (R) A Guide to the Development of a Ground Station for Engine Condition Monitoring | 
| 168 | SAE AMS-QQ-P-35A-2005 | 2005-02-01 | English | Passivation Treatments for Corrosion-Resistant Steel DoD Adopted
 | 
| 169 | SAE AMS-W-21425B-2005 | 2005-02-01 | English | Wire, Steel, High Carbon, Square, Uncoated, for Mechanical Springs (General Purpose) | 
| 170 | SAE AIR4766/1-2005 | 2005-02-01 | English | Air Quality for Commercial Aircraft Cabin Particulate Contaminants | 
| 171 | SAE AMS3416B-2005 | 2005-02-01 | English | Flux, Aluminum Dip Brazing 1090掳F (588掳C), Fusion Point | 
| 172 | SAE AS3507B-2005 | 2005-02-01 | English | (R) Insert -Thin Wall , Self-Locking Short and Long Length Installation and Removal of | 
| 173 | SAE AMS4021G-2005 | 2005-02-01 | English | (R) ALUMINUM ALLOY, ALCLAD SHEET AND PLATE, 1.0Mg - 0.60Si - 0.28Cu - 0.20Cr (Alclad 6061-0) Annealed DoD Adopted
 | 
| 174 | SAE AMS4194C-2005 | 2005-02-01 | English | Aluminum Alloy Sheet and Plate, Alclad 4.4Cu - 1.5Mg - 0.60Mn (Alclad 2024 and 1-1/2% Alclad 2024-T361 Flat Sheet; 1-1/2% Alclad 2024-T361 Plate) Solution Heat Treated and Cold Worked | 
| 175 | SAE AMS4200B-2005 | 2005-02-01 | English | Aluminum Alloy Plate 7.7Zn - 2.4Mg - 1.6Cu - 0.16Cr (7049-T7351) Solution Heat Treated, Stress Relieved, and Precipitation Heat Treated DoD Adopted
 | 
| 176 | SAE MA2048B-2005 | 2005-02-01 | English | (R) FITTING ASSEMBLY, ELBOW, 45 DEGREES, THIN WALL, RETAINED NUT, FLARELESS, METRIC | 
| 177 | SAE MA2049B-2005 | 2005-02-01 | English | (R) FITTING ASSEMBLY, TEE, THIN WALL, RETAINED NUT ON RUN, FLARELESS, METRIC | 
| 178 | SAE MA2050B-2005 | 2005-02-01 | English | (R) FITTING ASSEMBLY, ELBOW, 90 DEGREES, THIN WALL, RETAINED NUT, FLARELESS, METRIC | 
| 179 | SAE MA2126B-2005 | 2005-02-01 | English | Hose Assembly, Polytetrafluoroethylene (PTFE), up to 232 DEGREES C and 10 500 kPa Procurement Specification, Metric (ISO/DIS 10502) | 
| 180 | SAE AS1219A-2005 | 2005-02-01 | English | Aircraft Oxygen Replenishment Coupling for Civil Transport Aircraft (Design Standard) | 
| 181 | SAE ARP5414A-2005 | 2005-02-01 | English | Aircraft Lightning Zoning | 
| 182 | SAE ARP4171A-2005 | 2005-02-01 | English | Safety Considerations of Food and Beverage Service Carts | 
| 183 | SAE AMS4084D-2005 | 2005-02-01 | English | (R) Aluminum Alloy Sheet 5.7Zn - 2.2Mg - 1.6Cu - 0.22Cr (7475-T61) Solution and Precipitation Heat Treated DoD Adopted
 | 
| 184 | SAE AMS-T-81556A-2005 | 2005-02-01 | English | Titanium and Titanium Alloys, Extruded Bars snd Shapes, Aircraft Quality | 
| 185 | SAE AMS2421C-2005 | 2005-02-01 | English | Plating Magnesium for Solderability Zinc Immersion Process | 
| 186 | SAE AS8952A-2005 | 2005-02-01 | English | Bearings, Roller, Rod End, Antifriction Self-Aligning DoD Adopted
 | 
| 187 | SAE ARP5412A-2005 | 2005-02-01 | English | Aircraft Lightning Environment and Related Test Waveforms | 
| 188 | SAE ARP5533-2005 | 2005-02-01 | English | Stationary Runway Weather Information System (In-Pavement) | 
| 189 | SAE AMS4267-2005 | 2005-02-01 | English | Aluminum Alloy, Sheet (7055-O) 8.0Zn - 2.3Cu - 2.0Mg - 0.16Zr Annealed - UNS A97055 | 
| 190 | SAE AMS4051G-2005 | 2005-02-01 | English | Aluminum Alloy Sheet and Plate, Alclad 6.8Zn - 2.8Mg - 2.0Cu - 0.23Cr (Alclad 7178-0) Annealed | 
| 191 | SAE AS81934A-2005 | 2005-02-01 | English | (R) Bearings, Sleeve, Plain and Flanged, Self-Lubricating DoD Adopted
 | 
| 192 | SAE J1698-2005 | 2005-02-01 | English | (R) Vehicle Event Data InterfaceVehicular Output Data Definition | 
| 193 | SAE MA2085B-2005 | 2005-02-01 | English | HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, CRES REINFORCED, 204 DEGREES C, 21,000 KPA, 60-DEG CONE, TO 90-DEG TO 90-DEG, LIGHTWEIGHT, METRIC DoD Adopted
 | 
| 194 | SAE AMS4307B-2005 | 2005-02-01 | English | Aluminum Alloy, Extrusions 6.4Zn - 2.4Mg - 2.2Cu - 0.12Zr (7150-T61511) Solution Heat Treated, Stress Relieved by Stretching, Straightened, and Precipitation Heat Treated | 
| 195 | SAE AMS4009B-2005 | 2005-02-01 | English | Aluminum Alloy Foil 1.0Mg - 0.6Si - 0.30Cu - 0.20Cr (6061-0) Annealed DoD Adopted
 | 
| 196 | SAE AMS4318A-2005 | 2005-02-01 | English | Aluminum Alloy, Rolled or Cold Finished Bars and Rods 12.2Si - 1.0Mg - 0.90Cu - 0.90Ni (4032-T86) Solution Heat Treated, Cold Worked, and Artificially Aged | 
| 197 | SAE AMS4231G-2005 | 2005-02-01 | English | Castings, Sand 4.5Cu - 1.1Si Solution and Precipitation Heat Treated | 
| 198 | SAE AMS4240G-2005 | 2005-02-01 | English | Castings, Sand 10Mg Solution Heat Treated and Naturally Aged | 
| 199 | SAE AS5635-2005 | 2005-02-01 | English | Message Boards (Deicing Facilities) | 
| 200 | SAE AMS4314D-2005 | 2005-02-01 | English | (R) Aluminum Alloy Rings, Rolled or Forged 4.5Cu - 0.85Si - 0.80Mn - 0.50Mg (2014-T651, 2014-T652) Solution Heat Treated, Mechanically Stress Relieved, and Precipitation Heat Treated DoD Adopted
 | 
| 201 | SAE AMS3159F-2005 | 2005-02-01 | English | Leak Test Solution Liquid Oxygen Compatible | 
| 202 | SAE AS5586-2005 | 2005-02-01 | English | Aerospace   General Requirements for Hydraulic System Reservoirs | 
| 203 | SAE J1884-2005 | 2005-02-01 | English | Vehicle Jack Requirements and Test Procedure | 
| 204 | SAE AMS2465C-2005 | 2005-02-01 | English | Disilicide Diffusion Coating of Molybdenum and Molybdenum Alloys Pack Cementation Method DoD Adopted
 | 
| 205 | SAE J328-2005 | 2005-02-01 | English | WheelsPassenger Car and Light Truck Performance Requirements and Test Procedures | 
| 206 | SAE J164-2005 | 2005-02-01 | English | Radiator Caps and Filler Necks DoD Adopted
 | 
| 207 | SAE AMS-S-11310B-2005 | 2005-02-01 | English | Steel Bars, Carbon, Hot Rolled, for Cold Shaping, Including Cold Extrusion | 
| 208 | SAE AMS-S-6050B-2005 | 2005-02-01 | English | Steel, Chrome-Nickel-Molybdenum (8630) Bars and Reforging Stock (Aircraft Quality) | 
| 209 | SAE J2707-2005 | 2005-02-01 | English | Wear Test Procedure on Inertia Dynamometer for Brake Friction Materials | 
| 210 | SAE AS9104A-2005 | 2005-01-01(R 2013) | English | Requirements for Aerospace Quality Management System Certification/Registrations Programs | 
| 211 | SAE AS933D-2005 | 2005-01-01(R 2013) | English | FITTING, ADAPTER, UNION, FLARED TO BOSS | 
| 212 | SAE AS4227A-2005 | 2005-01-01(R 2013) | English | FITTING ASSEMBLY, ADAPTER, INTERNAL THREAD, BEAM SEAL TO INTEGRAL WELD RING | 
| 213 | SAE AS4859A-2005 | 2005-01-01(R 2013) | English | FITTING, COUPLING, PIPE, INTERNAL THREAD | 
| 214 | SAE AMS4193C-2005 | 2005-01-01(R 2012) | English | Aluminum Alloy Sheet and Plate 4.4Cu - 1.5Mg - 0.60Mn (2024-T861) Solution Heat Treated, Cold Worked, and Precipitation Heat Treated - UNS A92024 | 
| 215 | SAE AMS4299-2005 | 2005-01-01(R 2012) | English | Aluminum Alloy, Plate (7449-T7951) 8.1Zn - 1.8Cu - 2.3Mg Solution Heat Treated, Stress Relieved, and Overaged - UNS A97449 | 
| 216 | SAE AMS4332-2005 | 2005-01-01(R 2012) | English | Aluminum Alloy, Extruded Profiles (7349-T76511) 8.1Zn - 1.7Cu - 2.2Mg - 0.16Zr Solution Heat Treated, Stress-Relieved, and Overaged | 
| 217 | SAE AIR4985-2005 | 2005-01-01(R 2012) | English | A Methodology for Quantifying the Performance of an Engine Monitoring System | 
| 218 | SAE J2580-2005 | 2005-01-01(R 2011) | English | Identification and Installation of Air Brake System Components | 
| 219 | SAE AS50141A-2005 | 2005-01-01(R 2010) | English | (R) Tube, Pneumatic Tire, Aircraft DoD Adopted
 | 
| 220 | SAE J2704-2005 | 2005-01-01(R 2010) | English | Tire Normal Force/Deflection and Gross Footprint Dimension Test | 
| 221 | SAE AMS4299-2005 | 2005-01-01 | English | Aluminum Alloy, Plate (7449-T7951) 8.1Zn - 1.8Cu - 2.3Mg Solution Heat Treated, Stress Relieved, and Overaged - UNS A97449 | 
| 222 | SAE AS8049B-2005 | 2005-01-01 | English | Performance Standard for Seats in Civil Rotorcraft, Transport Aircraft, and General Aviation Aircraft | 
| 223 | SAE J1352-2005 | 2005-01-01 | English | Compression and Recovery of Insulation Paddings | 
| 224 | SAE AS25281A-2005 | 2005-01-01 | English | Clamp, Loop, Plastic, Wire Support DoD Adopted
 | 
| 225 | SAE ARP5589-2005 | 2005-01-01 | English | Human Engineering Considerations for Design and Implementation of Perspective Flight Guidance Displays | 
| 226 | SAE AIR4985-2005 | 2005-01-01 | English | A Methodology for Quantifying the Performance of an Engine Monitoring System | 
| 227 | SAE J2615-2005 | 2005-01-01 | English | Testing Performance of Fuel Cell Systems for Automotive Applications | 
| 228 | SAE AMS4167H-2005 | 2005-01-01 | English | Aluminum Alloy, Extrusions 5.6Zn - 2.5Mg - 1.6Cu - 0.23Cr (7075-T73511) Solution Heat Treated, Stress Relieved by Stretching, and Overaged - UNS A97075 DoD Adopted
 | 
| 229 | SAE AS933D-2005 | 2005-01-01 | English | FITTING, ADAPTER, UNION, FLARED TO BOSS DoD Adopted
 | 
| 230 | SAE J1352-2005 | 2005-01-01 | English | Compression and Recovery of Insulation Paddings | 
| 231 | SAE J100-2005 | 2005-01-01 | English | Class "A" Vehicle Glazing Shade Bands | 
| 232 | SAE J2580-2005 | 2005-01-01 | English | Identification and Installation of Air Brake System Components | 
| 233 | SAE AS5198C-2005 | 2005-01-01 | English | FITTING, TEE, FLARED TO PIPE ON RUN DoD Adopted
 | 
| 234 | SAE AS5196C-2005 | 2005-01-01 | English | FITTING, ELBOW, 45 DEGREES, FLARED TO PIPE DoD Adopted
 | 
| 235 | SAE AS4859A-2005 | 2005-01-01 | English | (R) FITTING, COUPLING, PIPE, INTERNAL THREAD DoD Adopted
 | 
| 236 | SAE J1499-2005 | 2005-01-01 | English | SAE Band Friction Test Machine Guidelines | 
| 237 | SAE AS4227A-2005 | 2005-01-01 | English | (R) FITTING ASSEMBLY, ADAPTER, INTERNAL THREAD, BEAM SEAL TO INTEGRAL WELD RING | 
| 238 | SAE AS5406C-2005 | 2005-01-01 | English | FITTING, UNION, TUBE, .375 BULKHEAD DoD Adopted
 | 
| 239 | SAE AMS4193C-2005 | 2005-01-01 | English | Aluminum Alloy Sheet and Plate 4.4Cu - 1.5Mg - 0.60Mn (2024-T861) Solution Heat Treated, Cold Worked, and Precipitation Heat Treated - UNS A92024 | 
| 240 | SAE AS9104A-2005 | 2005-01-01 | English | Requirements for Aerospace Quality Management System Certification/Registrations Programs | 
| 241 | SAE J2580-2005 | 2005-01-01 | English | Identification and Installation of Air Brake System Components | 
| 242 | SAE J100-2005 | 2005-01-01 | English | Class "A" Vehicle Glazing Shade Bands | 
| 243 | SAE AIR4985-2005 | 2005-01-01 | English | A Methodology for Quantifying the Performance of an Engine Monitoring System | 
| 244 | SAE AMS4334A-2005 | 2005-01-01 | English | Aluminum Alloy, Forgings 7.8Zn - 2.2Mg - 1.6Cu - 0.15Cr (7249-T74 and -T7452) DoD Adopted
 | 
| 245 | SAE AMS4332-2005 | 2005-01-01 | English | Aluminum Alloy, Extruded Profiles (7349-T76511) 8.1Zn - 1.7Cu - 2.2Mg - 0.16Zr Solution Heat Treated, Stress-Relieved, and Overaged | 
| 246 | SAE J1825-2005 | 2005-01-01 | English | Shelf Storage of Hydraulic Brake Components | 
| 247 | SAE AMS5390E-2005 | 2005-01-01 | English | Nickel Alloy, Corrosion and Heat-Resistant, Investment Castings 47.5Ni - 22Cr - 1.5Co - 9Mo - 0.60W - 18.5Fe (N-12MV) As-Cast - UNS N06002 DoD Adopted
 | 
| 248 | SAE AS5195C-2005 | 2005-01-01 | English | FITTING, ELBOW, 90 DEGREES, FLARED TO PIPE DoD Adopted
 | 
| 249 | SAE AMS5391F-2005 | 2005-01-01 | English | Nickel Alloy, Corrosion and Heat-Resistant, Investment Castings 73Ni - 0.14C - 13Cr - 4.5Mo - 2.3Cb - 0.75Ti - 6.0Al - 0.010B - 0.10Zr Vacuum Cast, As-Cast - UNS N07713 DoD Adopted
 | 
| 250 | SAE AMS5396D-2005 | 2005-01-01 | English | Nickel Alloy, Corrosion and Heat-Resistant, Investment Castings 65Ni - 28Mo - 5.5Fe - 0.40V (N-12MV) As-Cast - UNS N10001 DoD Adopted
 | 
| 251 | SAE R-345-2004 | 2004-12-06 | English | Internal Combustion Engine Handbook Basics, Components, Systems, and Perspectives - To Purchase Call 1-800-854-7179 USA/Canada or 303-397-7956 Worldwide | 
| 252 | SAE AS9310B-2004 | 2004-12-01(S 2014) | English | (R) STUD, SHOULDERED, HEX, WRENCHING, DRILLED, STEEL UNS G87400, CAD, PLATED, 125 KSI MIN, .2500-28 UNF-3A X .2500-28 UNF-3A(DoD Adopted) | 
| 253 | SAE AMS4017K-2004 | 2004-12-01(R 2012) | English | Aluminum Alloy Sheet and Plate 2.5Mg - 0.25Cr (5052-H34) Strain-Hardened, Half-Hard, and Stabilized - UNS A95052 | 
| 254 | SAE MA3286B-2004 | 2004-12-01(R 2012) | English | (R) BOLT, MACHINE - HEXAGON HEAD, PD SHANK, MJ THREAD, CORROSION AND HEAT RESISTANT STEEL, UNS S66286, 900 MPA MIN, METRIC | 
| 255 | SAE AIR5431-2004 | 2004-12-01(R 2011) | English | Repair Tooling | 
| 256 | SAE AS4775A-2004 | 2004-12-01(R 2011) | English | Aircraft Maintenance Jacks - General Requirements | 
| 257 | SAE AIR5885-2004 | 2004-12-01(R 2009) | English | Landing Gear Common Repairs | 
| 258 | SAE ARP5492-2004 | 2004-12-01(R 2009) | English | Aircraft Cargo Systems - Missing Restraint Limitations Layouts | 
| 259 | SAE AIR5052A-2004 | 2004-12-01 | English | Crack Initiation and Growth Considerations for Landing Gear Steel with Emphasis on AerMet 100 | 
| 260 | SAE ARP5916-2004 | 2004-12-01 | English | Design Specification for Regional Aircraft Towbarless Tow Vehicle for Pushback and/or Maintenance Towing Operations | 
| 261 | SAE AIR5431-2004 | 2004-12-01 | English | Repair Tooling | 
| 262 | SAE J2534-1-2004 | 2004-12-01 | English | (R) Recommended Practice for Pass-Thru Vehicle Programming | 
| 263 | SAE AMS3095A-2004 | 2004-12-01 | English | Paint: High Gloss For Airline Exterior System | 
| 264 | SAE AMS4343D-2004 | 2004-12-01 | English | Aluminum Alloy, Extrusions 7.7Zn - 2.4Mg - 1.6Cu - 0.16Cr (7149-T73511) Solution Heat Treated, Stress Relieved by Stretching, and Overaged - UNS A97149 DoD Adopted
 | 
| 265 | SAE AMS4017K-2004 | 2004-12-01 | English | Aluminum Alloy Sheet and Plate 2.5Mg - 0.25Cr (5052-H34) Strain- Hardened, Half-Hard, and Stabilized - UNS A95052 | 
| 266 | SAE AMS-R-81841A-2004 | 2004-12-01 | English | Rotary Flap Peening of Metal Parts | 
| 267 | SAE J2657-2004 | 2004-12-01 | English | Tire Pressure Monitoring Systems for Light Duty Highway Vehicles | 
| 268 | SAE AS9312A-2004 | 2004-12-01 | English | (R) STUD, SHOULDERED, STEPPED, HEX, WRENCHING, DRILLED, STEEL UNS G87400, CAD, PLATED, 125 KSI MIN, .2500-28 UNF-3A X .3750-24 UNF-3A DoD Adopted
 | 
| 269 | SAE J917-2004 | 2004-12-01 | English | (R) Marine Push-Pull Control Cables DoD Adopted
 | 
| 270 | SAE AMS4429-2004 | 2004-12-01 | English | Magnesium Alloy Castings, Sand 2.8Nd - 1.4Gd - 0.4Zn - 0.6Zr (EV31A - T6) Solution and Precipitation Heat Treated - UNS M12310 | 
| 271 | SAE AS5643/1-2004 | 2004-12-01 | English | S400 Copper Media Interface Characteristics Over Extended Distances | 
| 272 | SAE AS81044-A1-2004 | 2004-12-01 | English | Wire, Electrical, Crosslinked Polyalkene, Crosslinked Alkane- Imide Polymer, or Polyarlyene Insulated, Copper or Copper Alloy DoD Adopted
 | 
| 273 | SAE J2657-2004 | 2004-12-01 | English | Tire Pressure Monitoring Systems for Light Duty Highway Vehicles | 
| 274 | SAE AIR9968A-2004 | 2004-12-01 | English | Viscosity Test of Thickened Aircraft Deicing/Anti-icing Fluids | 
| 275 | SAE AMS-L-81846A-2004 | 2004-12-01 | English | Lubricating Oil, Instrument, Ball Bearing, High Flash Point | 
| 276 | SAE AMS-P-81985A-2004 | 2004-12-01 | English | Peening of Metals | 
| 277 | SAE AS9308A-2004 | 2004-12-01 | English | (R) STUD, SHOULDERED, HEX, WRENCHING, DRILLED, STEEL UNS G87400, CAD, PLATED, 125 KSI MIN, .1900-32 UNF-3A X .1900-32 UNF-3A DoD Adopted
 | 
| 278 | SAE MA3286B-2004 | 2004-12-01 | English | (R) BOLT, MACHINE - HEXAGON HEAD, PD SHANK, MJ THREAD, CORROSION AND HEAT RESISTANT STEEL, UNS S66286, 900 MPA MIN, METRIC DoD Adopted
 | 
| 279 | SAE AS9309A-2004 | 2004-12-01 | English | (R) STUD, SHOULDERED, STEPPED, HEX, WRENCHING, DRILLED, STEEL UNS G87400, CAD, PLATED, 125 KSI MIN, .1900-32 UNF-3A X .2500-28 UNF-3A DoD Adopted
 | 
| 280 | SAE AS9310A-2004 | 2004-12-01 | English | (R) STUD, SHOULDERED, HEX, WRENCHING, DRILLED, STEEL UNS G87400, CAD, PLATED, 125 KSI MIN, .2500-28 UNF-3A X .2500-28 UNF-3A DoD Adopted
 | 
| 281 | SAE AS9311A-2004 | 2004-12-01 | English | (R) STUD, SHOULDERED, STEPPED, HEX, WRENCHING, DRILLED, STEEL UNS G87400, CAD, PLATED, 125 KSI MIN, .2500-28 UNF-3A X .3125-24 UNF-3A DoD Adopted
 | 
| 282 | SAE AS506-2004 | 2004-12-01 | English | High Temperature Insulated Terminals & Splices | 
| 283 | SAE R-358-2004 | 2004-11-30 | English | Pioneers, Engineers, and Scoundrels The Dawn of the Automobile in America - To Purchase Call 1-800-854-7179 USA/Canada or 303-397-7956 Worldwide | 
| 284 | SAE AIR5693-2004 | 2004-11-01(R 2014) | English | Compatibility of PTFE Hose Assemblies With Typical Fluids Found in Aerospace Applications | 
| 285 | SAE AMS5364C-2004 | 2004-11-01(R 2012) | English | Steel, Corrosion and Heat-Resistant, Investment Castings 19.5Cr - 10.5Ni - 0.65Cb (CF-8C) Solution Heat Treated - UNS J92710 | 
| 286 | SAE AMS5368D-2004 | 2004-11-01(R 2012) | English | Steel, Corrosion-Resistant, Investment Castings 15Cr - 4.0Ni - 2.3Mo - 0.09N Solution Heat Treated - UNS J92001 | 
| 287 | SAE AMS5366E-2004 | 2004-11-01(R 2012) | English | Steel, Corrosion and Heat-Resistant, Investment Castings 25Cr - 20Ni (CK-20) As-Cast - UNS J94211 | 
| 288 | SAE AMS5370D-2004 | 2004-11-01(R 2012) | English | Steel, Corrosion and Heat-Resistant, Investment Castings 19Cr - 9.5Ni (CF-3) Solution Heat Treated - UNS J92620 | 
| 289 | SAE AS7283B-2004 | 2004-11-01(R 2012) | English | Gaskets, Type XX Engine Accessory Drive Corrosion Resistant Steel Screen Reinforced Controlled Performance | 
| 290 | SAE AMS4330B-2004 | 2004-11-01(R 2012) | English | Aluminum Alloy, Plate (2297-T87) 2.8Cu - 1.5Li - 0.30Mn - 0.12Zr Solution Heat Treated, Stretched, and Artificially Aged - UNS A92297 | 
| 291 | SAE AMS4326-2004 | 2004-11-01(R 2012) | English | Aluminum Alloy, 2013, Extruded Bar, Rod, and Profiles 1.0 Mg - 0.80 Si - 1.8 Cu - 0.20 Cr (2013 -T6511) Solution Heat Treated, Stress-Relieved by Stretching, and Aged - UNS A92013 | 
| 292 | SAE AMS4095C-2004 | 2004-11-01(R 2012) | English | Aluminum Alloy, Alclad Sheet and Plate 6.3Cu - 0.30Mn - 0.18Zr - 0.10V - 0.06Ti Alclad 2219-T31; Sheet, Solution Heat Treated and Cold Worked Alclad 2219-T351; Plate, Solution Heat Treated and Stress Relieved - UNS A82219 | 
| 293 | SAE AMS4094C-2004 | 2004-11-01(R 2012) | English | (R) Aluminum Alloy, Sheet and Plate, Alclad 6.3Cu - 0.30Mn - 0.18Zr - 0.10V - 0.06Ti Alclad 2219-T81 Sheet Solution Heat Treated, Cold Worked, and Precipitation Heat Treated Alclad 2219-T851 Plate Solution Heat Treated, Stress Relieved, and Precipitation | 
| 294 | SAE ARP5621-2004 | 2004-11-01(R 2011) | English | Electronic Display of Aeronautical Information (Charts) | 
| 295 | SAE J1113-13-2004 | 2004-11-01(R 2011) | English | Electromagnetic Compatibility Measurement Procedure for Vehicle ComponentsPart 13: Immunity to Electrostatic Discharge | 
| 296 | SAE AS85049/127A-2004 | 2004-11-01(R 2011) | English | CONNECTOR ACCESSORIES, ELECTRICAL, BUSHING STRIP CATEGORY 7 (FOR USE WITH SAE AS85049/118, /120, /121, /123, /124, /126) DoD Adopted
 | 
| 297 | SAE AMS2757B-2004 | 2004-11-01(R 2010) | English | Gaseous Nitrocarburizing | 
| 298 | SAE AS8056-2004 | 2004-11-01(R 2009) | English | Minimum Design and Performance of Airplane Galley In-Flight Carts, Containers, and Associated Components | 
| 299 | SAE AIR5693-2004 | 2004-11-01 | English | Compatibility of PTFE Hose Assemblies With Typical Fluids Found in Aerospace Applications | 
| 300 | SAE AS4877B-2004 | 2004-11-01 | English | Bolts and Screws, Nickel Alloy UNS N07718, Classification: 185 ksi/1200 掳F Procurement Specification DoD Adopted
 | 
| 301 | SAE J1113-13-2004 | 2004-11-01 | English | Electromagnetic Compatibility Measurement Procedure for Vehicle ComponentsPart 13: Immunity to Electrostatic Discharge | 
| 302 | SAE J1842-2004 | 2004-11-01 | English | (R) Disc Wheel Hub/Spoke Wheel and Axle Interface DimensionsCommercial Vehicles | 
| 303 | SAE AS85049/77A-2004 | 2004-11-01 | English | CONNECTOR ACCESSORIES, ELECTRICAL, BACKSHELL, ENVIRONMENTAL, 45掳, SHIELD TERMINATION, CATEGORY 2B, NONSELF-LOCKING (MIL-DTL-38999 SERIES I AND II CONNECTORS) - FSC 5935 DoD Adopted
 | 
| 304 | SAE AS85049/78A-2004 | 2004-11-01 | English | CONNECTOR ACCESSORIES, ELECTRICAL, BACKSHELL, ENVIRONMENTAL, 45掳, SHIELD TERMINATION, CATEGORY 2B, NONSELF-LOCKING (MIL-DTL-38999 SERIES III AND IV CONNECTORS) - FSC 5935 DoD Adopted
 | 
| 305 | SAE AS85049/127A-2004 | 2004-11-01 | English | CONNECTOR ACCESSORIES, ELECTRICAL,BUSHING STRIP CATEGORY 7 DoD Adopted
 | 
| 306 | SAE AMS4095C-2004 | 2004-11-01 | English | Aluminum Alloy, Alclad Sheet and Plate 6.3Cu - 0.30Mn - 0.18Zr - 0.10V - 0.06Ti Alclad 2219-T31; Sheet, Solution Heat Treated and Cold Worked Alclad 2219-T351; Plate, Solution Heat Treated and Stress Relieved - UNS A82219 | 
| 307 | SAE AMS4094C-2004 | 2004-11-01 | English | (R) Aluminum Alloy, Sheet and Plate, Alclad 6.3Cu - 0.30Mn - 0.18Zr - 0.10V - 0.06Ti Alclad 2219-T81 Sheet Solution Heat Treated, Cold Worked, and Precipitation Heat Treated Alclad 2219-T851 Plate Solution Heat Treated, Stress Relieved, and Precipitation Heat Treated - UNS A822190 | 
| 308 | SAE J2409-2004 | 2004-11-01 | English | (R) Strain-Life Fatigue Data File Format | 
| 309 | SAE AMS4418G-2004 | 2004-11-01 | English | Magnesium Alloy, Sand Castings 2.5Ag - 2.1Di - 0.70Zr (QE22A-T6) Solution and Precipitation Heat Treated DoD Adopted
 | 
| 310 | SAE J2260-2004 | 2004-11-01 | English | Nonmetallic Fuel System Tubing with One or More Layers | 
| 311 | SAE AS85049/53A-2004 | 2004-11-01 | English | CONNECTOR ACCESSORIES, ELECTRICAL, STRAIN RELIEF, NONENVIRONMENTAL, STRAIGHT, CATEGORY 4C (FOR MIL-DTL-5015 CRIMP, MIL-DTL-26482 SERIES 2, AS81703 SERIES 3, AND MIL-DTL-83723 SERIES III CONNECTORS) DoD Adopted
 | 
| 312 | SAE AS85049/54A-2004 | 2004-11-01 | English | CONNECTOR ACCESSORIES, ELECTRICAL, STRAIN RELIEF, NONENVIRONMENTAL, 45掳, CATEGORY 4C (FOR MIL-DTL-5015 CRIMP, MIL-DTL-26482 SERIES 2, AS81703 SERIES 3, AND MIL-DTL-83723 SERIES III CONNECTORS) DoD Adopted
 | 
| 313 | SAE AS85049/55B-2004 | 2004-11-01 | English | (R) CONNECTOR ACCESSORIES, ELECTRICAL, STRAIN RELIEF, NON-ENVIRONMENTAL, 90掳, SELF-LOCKING AND NON-SELF-LOCKING, CATEGORY 4C (FOR MIL-DTL-5015 CRIMP, MIL-DTL-26482 SERIES 2, AS81703 SERIES 3, AND MIL-DTL-83723 SERIES III CONNECTORS) DoD Adopted
 | 
| 314 | SAE AS85049/128A-2004 | 2004-11-01 | English | CONNECTOR ACCESSORIES, ELECTRICAL BACKSHELL, SHIELD BAND, CAGEGORY 7 (FOR AS85049/82 - /90, /93, /109 - /117 ACCESSORIES) - FSC 5935 | 
| 315 | SAE USCAR-17-2004 | 2004-11-01 | English | Performance Specification for Automotive RF Connector Systems - Revision 2 | 
| 316 | SAE AMS4326-2004 | 2004-11-01 | English | Aluminum Alloy, 2013, Extruded Bar, Rod, and Profiles 1.0 Mg - 0.80 Si - 1.8 Cu - 0.20 Cr (2013 -T6511) Solution Heat Treated, Stress-Relieved by Stretching, and Aged - UNS A92013 | 
| 317 | SAE J1638-2004 | 2004-11-01 | English | Compression Set of Hoses or Solid Discs DoD Adopted
 | 
| 318 | SAE MA2106B-2004 | 2004-11-01 | English | HOSE ASSEMBLY, METAL, MEDIUM PRESSURE FLARELESS, WELDED, 90掳 TO 90掳 FITTING ENDS, METRIC DoD Adopted
 | 
| 319 | SAE J1393-2004 | 2004-11-01 | English | (R) Heavy Duty Vehicle Cooling Test Code R | 
| 320 | SAE AMS4330B-2004 | 2004-11-01 | English | Aluminum Alloy, Plate (2297-T87) 2.8Cu - 1.5Li - 0.30Mn - 0.12Zr Solution Heat Treated, Stretched, and Artificially Aged - UNS A92297 | 
| 321 | SAE J775-2004 | 2004-11-01 | English | (R) Engine Poppet Valve Information Report | 
| 322 | SAE AS8056-2004 | 2004-11-01 | English | Minimum Design and Performance of Airplane Galley In-Flight Carts, Containers, and Associated Components | 
| 323 | SAE MA2103A-2004 | 2004-11-01 | English | HOSE ASSEMBLY, METAL, MEDIUM PRESSURE, FLARELESS, WELDED, STRAIGHT TO 90⁰ FITTING ENDS, METRIC | 
| 324 | SAE MA2101A-2004 | 2004-11-01 | English | HOSE ASSEMBLY, METAL, MEDIUM PRESSURE FLARELESS, WELDED, STRAIGHT TO STRAIGHT FITTING ENDS, METRIC | 
| 325 | SAE MA2178B-2004 | 2004-11-01 | English | HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, PTFE CRES REINFORCED, 232 ⁰C, 10,500 KPA, BEAM SEAL, STRAIGHT TO 90⁰, METRIC | 
| 326 | SAE AS13441A-2004 | 2004-11-01 | English | Test Methods for Electrical Connectors | 
| 327 | SAE J1737-2004 | 2004-11-01 | English | Test Procedure to Determine the Hydrocarbon Losses from Fuel Tubes, Hoses, Fittings, and Fuel Line Assemblies by Recirculation | 
| 328 | SAE AMS4186C-2004 | 2004-11-01 | English | (R) Aluminum Alloy Bars, Rods, and Wire, Rolled or Cold Finished 5.6Zn - 2.5Mg - 1.6Cu - 0.23Cr (7075-F) As Fabricated - UNS A97075 DoD Adopted
 | 
| 329 | SAE MA2102A-2004 | 2004-11-01 | English | HOSE ASSEMBLY, METAL, MEDIUM PRESSURE FLARELESS, WELDED, STRAIGHT TO 45掳 FITTING ENDS, METRIC DoD Adopted
 | 
| 330 | SAE AMS5377F-2004 | 2004-11-01 | English | Nickel Alloy, Corrosion and Heat-Resistant, Investment Castings 73Ni - 12Cr - 4.5Mo - 2.0Cb - 0.70Ti - 0.05C - 6.0Al - 0.010B - 0.10Zr Vacuum Cast, As-Cast DoD Adopted
 | 
| 331 | SAE AS7283B-2004 | 2004-11-01 | English | Gaskets, Type XX Engine Accessory Drive Corrosion Resistant Steel Screen Reinforced Controlled Performance DoD Adopted
 | 
| 332 | SAE AS21429A-2004 | 2004-11-01 | English | (R) BEARING, ROLLER, ANTIFRICTION, ROD END, EXTERNAL THREAD, SELF-ALIGNING, AIR FRAME, -67 DEGREES F, TO 350 DEGREES F TYPE 1, HEAVY DUTY, SEALED DoD Adopted
 | 
| 333 | SAE AS83413/8A-2004 | 2004-11-01 | English | CONNECTORS AND ASSEMBLIES, ELECTRICAL, AIRCRAFT GROUNDING: TYPE IV JUMPER CABLE ASSEMBLY, LEAD, ELECTRICAL | 
| 334 | SAE MA2103A-2004 | 2004-11-01 | English | HOSE ASSEMBLY, METAL, MEDIUM PRESSURE FLARELESS, WELDED, STRAIGHT TO 90掳 FITTING ENDS, METRIC DoD Adopted
 | 
| 335 | SAE MA2104A-2004 | 2004-11-01 | English | HOSE ASSEMBLY, METAL, MEDIUM PRESSURE FLARELESS, WELDED, 45掳 TO 45掳 FITTING ENDS, METRIC DoD Adopted
 | 
| 336 | SAE ARP1928A-2004 | 2004-11-01 | English | Torque Recommendations for Attaching Electrical Wiring Devices to Terminal Boards or Blocks, Studs, Posts, etc. | 
| 337 | SAE J1116-2004 | 2004-11-01 | English | Categories of Off-Road Self-Propelled Work Machines | 
| 338 | SAE J844-2004 | 2004-11-01 | English | (R) Nonmetallic Air Brake System Tubing DoD Adopted
 | 
| 339 | SAE MA2101A-2004 | 2004-11-01 | English | HOSE ASSEMBLY, METAL, MEDIUM PRESSURE FLARELESS, WELDED, STRAIGHT TO STRAIGHT FITTING ENDS, METRIC DoD Adopted
 | 
| 340 | SAE AMS5370D-2004 | 2004-11-01 | English | Steel, Corrosion and Heat-Resistant, Investment Castings 19Cr - 9.5Ni (CF-3) Solution Heat Treated DoD Adopted
 | 
| 341 | SAE MA2105A-2004 | 2004-11-01 | English | HOSE ASSEMBLY, METAL, MEDIUM PRESSURE FLARELESS, WELDED, 45掳 TO 90掳 FITTING ENDS, METRIC DoD Adopted
 | 
| 342 | SAE AMS5364C-2004 | 2004-11-01 | English | Steel, Corrosion and Heat-Resistant, Investment Castings 19.5Cr - 10.5Ni - 0.65Cb (CF-8C) Solution Heat Treated | 
| 343 | SAE AMS5360F-2004 | 2004-11-01 | English | Steel, Corrosion and Heat-Resistant, Investment Castings 17Cr - 13Ni - 1.9Mo Solution Heat Treated - UNS J92951 DoD Adopted
 | 
| 344 | SAE AS81934/2A-2004 | 2004-11-01 | English | (R) BEARING, SLEEVE, FLANGED, SELF-LUBRICATING, -65 掳F TO 325 掳F DoD Adopted
 | 
| 345 | SAE AMS5366E-2004 | 2004-11-01 | English | Steel, Corrosion and Heat-Resistant, Investment Castings 25Cr - 20Ni (CK-20) As-Cast DoD Adopted
 | 
| 346 | SAE MA2178B-2004 | 2004-11-01 | English | HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, PTFE CRES REINFORCED, 232 掳C, 10 500 KPA, BEAM SEAL, STRAIGHT TO 90掳, METRIC DoD Adopted
 | 
| 347 | SAE AMS5368D-2004 | 2004-11-01 | English | Steel, Corrosion-Resistant, Investment Castings 15Cr - 4.0Ni - 2.3Mo - 0.09N Solution Heat Treated DoD Adopted
 | 
| 348 | SAE AS81934/1A-2004 | 2004-11-01 | English | (R) BEARING, SLEEVE, PLAIN, SELF-LUBRICATING, -65 掳F TO 325 掳F DoD Adopted
 | 
| 349 | SAE AS9226A-2004 | 2004-10-01(S 2014) | English | WIRE - STEEL, CORROSION AND HEAT RESISTANT, SAFETY, 1800 DEGREES F | 
| 350 | SAE J891-2004 | 2004-10-01(R 2013) | English | Spring Nuts | 
| 351 | SAE AMS2433C-2004 | 2004-10-01(R 2011) | English | Plating, Nickel-Thallium-Boron or Nickel-Boron Electroless Deposition DoD Adopted
 | 
| 352 | SAE AMS2403L-2004 | 2004-10-01(R 2009) | English | Plating, Nickel General Purpose | 
| 353 | SAE ARP583H-2004 | 2004-10-01(R 2009) | English | Flight Attendant Stations | 
| 354 | SAE AS85049/46A-2004 | 2004-10-01 | English | CONNECTOR ACCESSORIES, ELECTRICAL, STRAIN RELIEF, 90掳, NONMETALLIC, CATEGORY 4C (FOR MIL-C-27599 SERIES I AND MIL-DTL-38999 SERIES I AND II CONNECTORS) - FSC 5935 DoD Adopted
 | 
| 355 | SAE AS85049/50A-2004 | 2004-10-01 | English | CONNECTOR ACCESSORIES, ELECTRICAL, STRAIN RELIEF, 90掳, CATEGORY 7 (FOR MIL-DTL-24308 CONNECTORS) - FSC 5935 DoD Adopted
 | 
| 356 | SAE J2266-2004 | 2004-10-01 | English | Location Referencing Message Specification (LRMS) | 
| 357 | SAE MS1000-2004 | 2004-10-01 | English | Lubricants, Industrial Oils, and Related ProductsClassification | 
| 358 | SAE AS9226-2004 | 2004-10-01 | English | WIRE - STEEL, CORROSION AND HEAT RESISTANT, SAFETY, 1800 DEGREES F | 
| 359 | SAE AMS4339A-2004 | 2004-10-01 | English | Aluminum Alloy, Rolled or Cold Finished Bars and Rods 4.4Cu - 1.5Mg - 0.60Mn (2024-T851) Solution Heat Treated, Cold Worked, and Artificially Aged - UNS A92024 | 
| 360 | SAE J378-2004 | 2004-10-01 | English | (R) Marine Propulsion System Wiring | 
| 361 | SAE J891-2004 | 2004-10-01 | English | Spring Nuts | 
| 362 | SAE AS85049/85A-2004 | 2004-10-01 | English | CONNECTOR ACCESSORIES, ELECTRICAL, BACKSHELL, STRAIGHT, SELF-LOCKING, SHIELD BAND TERMINATION (RFI/EMI), SHRINK BOOT ACCOMMODATION, CATEGORY 3B (FOR MIL-DTL-38999 SERIES I AND II CONNECTORS) - FSC 5935 DoD Adopted
 | 
| 363 | SAE AS85049/82A-2004 | 2004-10-01 | English | CONNECTOR ACCESSORIES, ELECTRICAL, BACKSHELL, STRAIGHT, SELF-LOCKING, SHIELD BAND TERMINATION (RFI/EMI), SHRINK SLEEVE ACCOMMODATION, CATEGORY 3B (FOR MIL-DTL-5015 CRIMP, MIL-DTL-26482 SERIES 2, AS81703 SERIES 3 AND MIL-DTL-83723 SERIES III CONNECTORS) DoD Adopted
 | 
| 364 | SAE AS85049/69A-2004 | 2004-10-01 | English | CONNECTOR ACCESSORIES, ELECTRICAL, ADAPTER, SHRINKBOOT, CATEGORY 5 (MIL-DTL-38999 SERIES III AND IV CONNECTORS) - FSC 5935 DoD Adopted
 | 
| 365 | SAE AS85049/33A-2004 | 2004-10-01 | English | CONNECTOR ACCESSORIES, ELECTRICAL, BACKSHELL, NONENVIRONMENTAL, STRAIGHT, SHIELDED TERMINATION, CATEGORY 7 (FOR MIL-DTL-38999 SERIES I AND II CONNECTORS) - FSC 5935 DoD Adopted
 | 
| 366 | SAE J2667-2004 | 2004-10-01 | English | STRSW (Squeeze Type Resistance Spot Welding) Equipment Acceptance Criteria for the Collision Repair Industry | 
| 367 | SAE AS85049/79A-2004 | 2004-10-01 | English | CONNECTOR ACCESSORIES, ELECTRICAL, BACKSHELL, ENVIRONMENTAL, 90掳, SHIELD TERMINATION, CATEGORY 2B, NONSELF-LOCKING (MIL-DTL-38999 SERIES III AND IV CONNECTORS) - FSC 5935 DoD Adopted
 | 
| 368 | SAE AS3066A-2004 | 2004-10-01 | English | Nut, Self-Locking, Double Hexagon, Reduced Envelope, AMS 7251 - FSC 5310 | 
| 369 | SAE AS4074/3A-2004 | 2004-10-01 | English | Type E-1 Electrical Media Interface Characteristics | 
| 370 | SAE AMS2433C-2004 | 2004-10-01 | English | Plating, Nickel-Thallium-Boron or Nickel-Boron Electroless Deposition DoD Adopted
 | 
| 371 | SAE J274-2004 | 2004-10-01 | English | Rated Suspension Spring Capacity | 
| 372 | SAE AS4074A-2004 | 2004-10-01 | English | Linear Token Passing Multiplex Data Bus | 
| 373 | SAE J1122-2004 | 2004-10-01 | English | Helical Springs: Specification Check Lists | 
| 374 | SAE AS4074/2A-2004 | 2004-10-01 | English | Type F-2 Fiber Optic Media Interface Characteristics | 
| 375 | SAE AS4074/1A-2004 | 2004-10-01 | English | Type F-1 Fiber Optic Media Interface Characteristics | 
| 376 | SAE J2596-2004 | 2004-10-01 | English | Fastener Part StandardTapping Screws and Metallic Drive Screws (Inch Dimensioned) | 
| 377 | SAE J1464-2004 | 2004-10-01 | English | Identification Terminology of Loaders/Tractors with Forks and Rough Terrain Forklifts | 
| 378 | SAE R-349-2004 | 2004-09-27 | English | Finite Element Analysis for Design Engineers - To Purchase Call 1-800-854-7179 USA/Canada or 303-397-7956 Worldwide | 
| 379 | SAE AS9842A-2004 | 2004-09-01(R 2018) | English | (R) PIN, STRAIGHT, HEADED, .0937 DIAMETER, UNS S41800 | 
| 380 | SAE AS9842A-2004 | 2004-09-01(R 2013) | English | (R) PIN, STRAIGHT, HEADED, .0937 DIAMETER, UNS S41800(DoD Adopted) | 
| 381 | SAE AS20005-2004 | 2004-09-01(R 2012) | English | DRIVE - TYPE XV ENGINE ACCESSORY - DESIGN STANDARD FOR | 
| 382 | SAE AS20010-2004 | 2004-09-01(R 2012) | English | DRIVE - TYPE XX ENGINE ACCESSORY - DESIGN STANDARD FOR | 
| 383 | SAE AS9846A-2004 | 2004-09-01(R 2012) | English | PIN, STRAIGHT, HEADED, .3124 DIAMETER, UNS S41800 | 
| 384 | SAE AS9845A-2004 | 2004-09-01(R 2012) | English | PIN, STRAIGHT, HEADED, .2499 DIAMETER, UNS S41800 | 
| 385 | SAE AS9843A-2004 | 2004-09-01(R 2012) | English | PIN, STRAIGHT, HEADED, .1249 DIAMETER, UNS S41800 | 
| 386 | SAE AS9847A-2004 | 2004-09-01(R 2012) | English | PIN, STRAIGHT, HEADED, .3749 DIAMETER, UNS S41800 | 
| 387 | SAE AS9844A-2004 | 2004-09-01(R 2012) | English | PIN, STRAIGHT, HEADED, .1874 DIAMETER, UNS S41800 | 
| 388 | SAE AS9848A-2004 | 2004-09-01(R 2012) | English | PIN, STRAIGHT, HEADED, .49999 DIAMETER, UNS S41800 | 
| 389 | SAE J268-2004 | 2004-09-01(R 2010) | English | Rear View Mirrors鈥擬otorcycles | 
| 390 | SAE J1939-74-2004 | 2004-09-01(R 2010) | English | Application-Configurable Messaging | 
| 391 | SAE J913-2004 | 2004-09-01(R 2010) | English | Test Method for Wicking of Automotive Fabrics and Fibrous Materials | 
| 392 | SAE J315-2004 | 2004-09-01(R 2010) | English | Fiberboard Test Procedure | 
| 393 | SAE J1625-2004 | 2004-09-01 | English | Heavy-Duty Circuit Breakers | 
| 394 | SAE AS9842A-2004 | 2004-09-01 | English | (R) PIN, STRAIGHT, HEADED, .0937 DIAMETER, UNS S41800 DoD Adopted
 | 
| 395 | SAE AS20005-2004 | 2004-09-01 | English | DRIVE - TYPE XV ENGINE ACCESSORY - DESIGN STANDARD FOR | 
| 396 | SAE AS20010-2004 | 2004-09-01 | English | DRIVE - TYPE XX ENGINE ACCESSORY - DESIGN STANDARD FOR | 
| 397 | SAE J1160-2004 | 2004-09-01 | English | Operator Ear Sound Level Measurement Procedure for Snow Vehicles | 
| 398 | SAE AS9843A-2004 | 2004-09-01 | English | (R) PIN, STRAIGHT, HEADED, .1249 DIAMETER, UNS S41800 DoD Adopted
 | 
| 399 | SAE J1503-2004 | 2004-09-01 | English | Performance Test for Air-Conditioned, Heated, and Ventilated Off-Road, Self-Propelled Work Machines | 
| 400 | SAE J913-2004 | 2004-09-01 | English | Test Method for Wicking of Automotive Fabrics and Fibrous Materials | 
| 401 | SAE AS9848A-2004 | 2004-09-01 | English | (R) PIN, STRAIGHT, HEADED, .4999 DIAMETER, UNS S41800 DoD Adopted
 | 
| 402 | SAE AS9847A-2004 | 2004-09-01 | English | (R) PIN, STRAIGHT, HEADED, .3749 DIAMETER, UNS S41800 DoD Adopted
 | 
| 403 | SAE AS9846A-2004 | 2004-09-01 | English | (R) PIN, STRAIGHT, HEADED, .3124 DIAMETER, UNS S41800 DoD Adopted
 | 
| 404 | SAE AS9845A-2004 | 2004-09-01 | English | (R) PIN, STRAIGHT, HEADED, .2499 DIAMETER, UNS S41800 DoD Adopted
 | 
| 405 | SAE AS9844A-2004 | 2004-09-01 | English | (R) PIN, STRAIGHT, HEADED, .1874 DIAMETER, UNS S41800 DoD Adopted
 | 
| 406 | SAE J1654-2004 | 2004-09-01 | English | High Voltage Primary Cable | 
| 407 | SAE J1503-2004 | 2004-09-01 | English | Performance Test for Air-Conditioned, Heated, and Ventilated Off-Road, Self-Propelled Work Machines DoD Adopted
 | 
| 408 | SAE J514-2004 | 2004-09-01 | English | Hydraulic Tube Fittings DoD Adopted
 | 
| 409 | SAE AS9104-2004 | 2004-09-01 | English | Requirements for Aerospace Quality Management System Certification/Registrations Programs | 
| 410 | SAE J268-2004 | 2004-09-01 | English | Rear View Mirrors—Motorcycles | 
| 411 | SAE AS85049/58A-2004 | 2004-09-01 | English | Connector Accessories, Electrical, Ring, Potting Boot, Category 5 (MIL-DTL-38999 Series I and II Connectors) DoD Adopted
 | 
| 412 | SAE J1487-2004 | 2004-09-01 | English | Rating Air-Conditioner Evaporator Air Delivery and Cooling Capacities | 
| 413 | SAE AS83519A-A1-2004 | 2004-09-01 | English | Shield Termination, Solder Style, Insulated, Heat-Shrinkable, Environment Resistant General Specification For DoD Adopted
 | 
| 414 | SAE AIR1168/12-2004 | 2004-09-01 | English | Spacecraft Thermal Balance | 
| 415 | SAE AMS2546-2004 | 2004-08-01(R 2019) | English | Laser Peening | 
| 416 | SAE ARP1785B-2004 | 2004-08-01(R 2013) | English | Standard Codes for Outer Sleeving on Hose Assemblies | 
| 417 | SAE AS8879D-2004 | 2004-08-01(R 2012) | English | Screw Threads - UNJ Profile, Inch Controlled Radius Root with Increased Minor Diameter | 
| 418 | SAE J2654-2004 | 2004-08-01(R 2012) | English | Hardness of Brake Lining | 
| 419 | SAE J294-2004 | 2004-08-01(R 2011) | English | Service Brake Structural Integrity Test Procedure鈥擵ehicles Over 4500 kg (10 000 lb) GVWR | 
| 420 | SAE J2621-2004 | 2004-08-01(R 2011) | English | Qualifying Aftermarket Two-Component Structural Foams | 
| 421 | SAE J1774-2004 | 2004-08-01(R 2010) | English | Design Guidelines for Fiberboard Materials | 
| 422 | SAE AMS2546-2004 | 2004-08-01(R 2010) | English | Laser Peening | 
| 423 | SAE AS755D-2004 | 2004-08-01(R 2009) | English | (R) Aircraft Propulsion System Performance Station Designation and Nomenclature DoD Adopted
 | 
| 424 | SAE J379-2004 | 2004-08-01(R 2009) | English | (R) Gogan Hardness of Brake Lining DoD Adopted
 | 
| 425 | SAE ARP5542-2004 | 2004-08-01(R 2009) | English | Hand Held Aircraft Tire Inflation Pressure Gauges | 
| 426 | SAE AS5688A-2004 | 2004-08-01 | English | Cable Assemblies; Aircraft, Proof Testing and Prestretching of | 
| 427 | SAE J2588-2004 | 2004-08-01 | English | Remote Steering Control Systems | 
| 428 | SAE AS81659-A1-2004 | 2004-08-01 | English | Connector, Electrical, Rectangular Crimp Contacts General Specification For DoD Adopted
 | 
| 429 | SAE MA2096C-2004 | 2004-08-01 | English | (R) FITTING END, 24掳 CONE, BULKHEAD, DESIGN STANDARD, METRIC | 
| 430 | SAE AMS-QQ-A-225B-2004 | 2004-08-01 | English | Aluminum and Aluminum Alloy, Bar, Rod, Wire, or Special Shapes; Rolled, Drawn, or Cold Finished; General Specification For DoD Adopted
 | 
| 431 | SAE AS8879D-2004 | 2004-08-01 | English | Screw Threads - UNJ Profile, Inch Controlled Radius Root with Increased Minor Diameter DoD Adopted
 | 
| 432 | SAE J1004-2004 | 2004-08-01 | English | Glossary of Engine Cooling System Terms | 
| 433 | SAE AMS-QQ-A-200B-2004 | 2004-08-01 | English | Aluminum Alloy, Bar, Rod, Shapes, Structural Shapes, Tube, and Wire, Extruded: General Specification for DoD Adopted
 | 
| 434 | SAE MA2095C-2004 | 2004-08-01 | English | (R) FITTING END, 24掳 CONE, DESIGN STANDARD, METRIC | 
| 435 | SAE AS8879D-2004 | 2004-08-01 | English | Screw Threads - UNJ Profile, Inch Controlled Radius Root with Increased Minor Diameter - Best Copy Available | 
| 436 | SAE AS9144A-2004 | 2004-08-01 | English | (R) Gasket - Type XX Engine Accessory Drive DoD Adopted
 | 
| 437 | SAE J1941-2004 | 2004-08-01 | English | Coolant Concentrate (Low Silicate, Ethylene Glycol Type Requiring an Initial Charge of Supplemental Coolant Additive) for Heavy-Duty Engines | 
| 438 | SAE AS7949B-2004 | 2004-08-01 | English | (R) Bearings, Ball, Airframe, Antifriction, General Standard for DoD Adopted
 | 
| 439 | SAE J2494-1-2004 | 2004-08-01 | English | Dimensional Specifications for Metallic Body Push-to-Connect Fittings Used on a Vehicular Air Brake System | 
| 440 | SAE ARP1785B-2004 | 2004-08-01 | English | (R) Standard Codes for Outer Sleeving on Hose Assemblies | 
| 441 | SAE JA1010-1-2004 | 2004-08-01 | English | Maintainability Program Standard Implementation Guide | 
| 442 | SAE J1231-2004 | 2004-08-01 | English | Formed Tube Ends for Hose Connections and Hose Fittings DoD Adopted
 | 
| 443 | SAE J294-2004 | 2004-08-01 | English | Service Brake Structural Integrity Test Procedure - Vehicles Over 4500 kg (10 000 lb) GVWR | 
| 444 | SAE AS55151A-2004 | 2004-08-01 | English | Pump, Hydraulic, Ram, Hand Driven | 
| 445 | SAE MA2095C-2004 | 2004-08-01 | English | (R) FITTING END, 24° CONE, DESIGN STANDARD, METRIC | 
| 446 | SAE AS5382/2-2004 | 2004-08-01 | English | CABLE, FIBER OPTIC, MULTIMODE, 100/140/172 micro m GRADED INDEX, NONHERMETIC, LOOSE TUBE | 
| 447 | SAE MA2096C-2004 | 2004-08-01 | English | (R) FITTING END, 24° CONE, BULKHEAD, DESIGN STANDARD, METRIC | 
| 448 | SAE AMS-QQ-A-250A-2004 | 2004-08-01 | English | Aluminum and Aluminum Alloy, Plate and Sheet General Specification for DoD Adopted
 | 
| 449 | SAE J2671-2004 | 2004-08-01 | English | Reduced Effort Brakes and Reduced Effort Vacuum Powered Brake Backup Systems | 
| 450 | SAE J2364-2004 | 2004-08-01 | English | Navigation and Route Guidance Function Accessibility While Driving | 
| 451 | SAE J2643-2004 | 2004-08-01 | English | Standard Reference Elastomers (SRE) for Characterizing the Effect of Liquids on Vulcanized RubberS | 
| 452 | SAE J2649-2004 | 2004-08-01 | English | Strain-Life Overload Fatigue Data File Format | 
| 453 | SAE J2654-2004 | 2004-08-01 | English | Hardness of Brake Lining | 
| 454 | SAE J2672-2004 | 2004-08-01 | English | Reduced Effort Power Steering and Power Steering Backup Systems | 
| 455 | SAE J2678-2004 | 2004-08-01 | English | Navigation and Route Guidance Function Accessibility While Driving Rationale | 
| 456 | SAE ARP4992A-2004 | 2004-08-01 | English | Periodic Test Plan for Processing Solutions | 
| 457 | SAE J294-2004 | 2004-08-01 | English | Service Brake Structural Integrity Test ProcedureVehicles Over 4500 kg (10 000 lb) GVWR | 
| 458 | SAE J1113-4-2004 | 2004-08-01 | English | (R) Immunity to Radiated Electromagnetic FieldsBulk Current Injection (BCI) Method | 
| 459 | SAE J887-2004 | 2004-08-01 | English | School Bus Warning Lamps | 
| 460 | SAE MA2073-2004 | 2004-07-20 | English | NUT, MALE, OLIVE, FLARELESS, 20000 KPA, METRIC | 
| 461 | SAE AMS3267B-2004 | 2004-07-20 | English | Sealing Compound, Low Adhesion, Corrosion Inhibiting for Removable Panels and Fuel Tank Inspection Plates | 
| 462 | SAE AS83-2004 | 2004-07-19 | English | SCREW THREADS, AERONAUTICAL | 
| 463 | SAE AS77-2004 | 2004-07-19 | English | SCREW - DE-ICER | 
| 464 | SAE AS79-2004 | 2004-07-19 | English | CATALOGS, SPARE PARTS, FOR AIRCRAFT ENGINES | 
| 465 | SAE AS80-2004 | 2004-07-19 | English | CATALOGS, OVERHAUL TOOL, FOR AIRCRAFT ENGINES | 
| 466 | SAE AS76-2004 | 2004-07-19 | English | RIVNUT, DE-ICER ATTACHMENT (KEYLESS) | 
| 467 | SAE AS78-2004 | 2004-07-19 | English | SCREW, DE-ICER RIVNUT PLUG | 
| 468 | SAE AS E25-2004 | 2004-07-19 | English | HARDWARE SPECIFICATIONS SUBSCRIPTION | 
| 469 | SAE AS8A-2004 | 2004-07-19 | English | PLUG, DEHYDRATOR | 
| 470 | SAE AS9B-2004 | 2004-07-19 | English | PROTECTOR & CABLE ATTACHMENT, SPARK PLUG TERMINAL (AIRCRAFT ENGINE) | 
| 471 | SAE AS73-2004 | 2004-07-19 | English | DE-ICER, ATTACHMENT ASSEMBLIES (INFLATABLE TYPE) | 
| 472 | SAE AS74-2004 | 2004-07-19 | English | FAIRING, DE-ICER ATTACHMENT | 
| 473 | SAE AS75-2004 | 2004-07-19 | English | PEG, DE-ICER POSITIONING | 
| 474 | SAE AS66-2004 | 2004-07-16 | English | CARBURETOR FLANGE, AIRCRAFT, DOUBLE BARREL - SIZE 24 (REMOTE FUEL DISCHARGE TYPE) | 
| 475 | SAE AS67-2004 | 2004-07-16 | English | CARBURETOR FLANGE, AIRCRAFT, RECTANGULAR - NO. 9 AND SIZE 12 | 
| 476 | SAE AS68-2004 | 2004-07-16 | English | CARBURETOR FLANGE, AIRCRAFT, RECTANGULAR - SIZE 24 AND 30 | 
| 477 | SAE AS69-2004 | 2004-07-16 | English | CARBURETOR FLANGE, AIRCRAFT, TRIPLE BARREL - SIZE 41 | 
| 478 | SAE AS70-2004 | 2004-07-16 | English | FLANGE, TUBE - TWO BOLT TYPE - AIRCRAFT ENGINE | 
| 479 | SAE AS65-2004 | 2004-07-16 | English | CARBURETOR FLANGE, AIRCRAFT, DOUBLE BARREL - SIZE 24 | 
| 480 | SAE AS64-2004 | 2004-07-16 | English | CARBURETOR FLANGE, AIRCRAFT, DOUBLE BARREL - SIZE 12 AND 16 | 
| 481 | SAE ARP87-2004 | 2004-07-16 | English | HEATER, AIRPLANE, STEAM TYPE | 
| 482 | SAE AS7B-2004 | 2004-07-16 | English | PLUG, DEHYDRATOR (CABLE SUPPORTING) | 
| 483 | SAE AS213-2004 | 2004-07-15 | English | CRANKING MOTORS - 12 VOLT | 
| 484 | SAE AS215-2004 | 2004-07-15 | English | GENERATOR CONTROL UNIT - 12 VOLT | 
| 485 | SAE AS216-2004 | 2004-07-15 | English | MAGNETIC SWITCHES - 12 VOLT | 
| 486 | SAE AS235-2004 | 2004-07-15 | English | TERMINAL, THERMO-SENSITIVE ELEMENT | 
| 487 | SAE AS15-2004 | 2004-07-15 | English | MAGNETOS, AIRCRAFT, TESTS OF | 
| 488 | SAE AS10B-2004 | 2004-07-15 | English | INDICATOR, HUMIDITY, LARGE | 
| 489 | SAE AS6A-2004 | 2004-07-15 | English | ENCLOSURE, STORAGE AND SHIPPING (AIRCRAFT ENGINE) | 
| 490 | SAE AS11A-2004 | 2004-07-15 | English | EQUIPMENT, SPRAY, CORROSION-PREVENTATIVE COMPOUND | 
| 491 | SAE AS16A-2004 | 2004-07-15 | English | PERFORMANCE PRESENTATION, AIRCRAFT RECIPROCATING ENGINE - SINGLE SPEED ENGINE | 
| 492 | SAE AS17A-2004 | 2004-07-15 | English | PERFORMANCE PRESENTATION, AIRCRAFT RECIPROCATING ENGINE - TWO SPEED ENGINE | 
| 493 | SAE AS18A-2004 | 2004-07-15 | English | PERFORMANCE PRESENTATION, AIRCRAFT RECIPORCATING ENGINE - TWO SPEED ENGINE | 
| 494 | SAE AS170-2004 | 2004-07-15 | English | CAP, THREAD PROTECTOR (INBOARD) - DUAL PROPELLER SHAFTS | 
| 495 | SAE AS172-2004 | 2004-07-15 | English | NUT, PROPELLER SHAFT, SHIPPING | 
| 496 | SAE AS173-2004 | 2004-07-15 | English | CAP, PROPELLER SHAFT, SHIPPING | 
| 497 | SAE AS1567-2004 | 2004-07-15 | English | No Title Available | 
| 498 | SAE AS174-2004 | 2004-07-15 | English | SERVICE BULLETINS FOR AIRCRAFT ENGINES, PREPARATION OF | 
| 499 | SAE AS181-2004 | 2004-07-15 | English | WHEEL AND AXLE DIMENSIONS, TAIL WHEEL, HIGH PRESSURE - STRAIGHT AXLE TYPE | 
| 500 | SAE AS184-2004 | 2004-07-15 | English | WHEEL AND AXLE DIMENSIONS, LOW - PROFILE - STUB AXLE TYPE | 
  
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