| Pos | standard Number | publication date | Language | Description |
| 1 | SAE AMS4442F-2007 | 2007-01-01 | English | Magnesium Alloy Sand Castings 3.2 Rare Earths - 2.5Zn - 0.70Zr (EZ33A-T5) Precipitation Heat Treated - UNS M12330 |
| 2 | SAE J901-2007 | 2007-01-01 | English | Universal Joints and Driveshafts - Nomenclature - Terminology - Application |
| 3 | SAE AMS4928R-2007 | 2007-01-01 | English | Titanium Alloy Bars, Wire, Forgings, Rings, and Drawn Shapes 6Al - 4V Annealed - UNS R56400
DoD Adopted |
| 4 | SAE AMS3021D-2007 | 2007-01-01 | English | Fluid, Reference for Testing Di-Ester (Polyol) Resistant Material
DoD Adopted |
| 5 | SAE J1362-2007 | 2007-01-01 | English | Graphical Symbols for Operator Controls and Displays on Off-Road Self-Propelled Work Machines
DoD Adopted |
| 6 | SAE R-377-2007 | 2007-01-01 | English | Automotive Safety Handbook - Second Edition; To Purchase Call 1-800-854-7179 USA/Canada or 303-397-7956 Worldwide |
| 7 | SAE MS1008-2007 | 2007-01-01 | English | Lubricants, Industrial Oils, and Related Products Type M (Metal Removal Fluids) - Specification |
| 8 | SAE AMS5339F-2007 | 2007-01-01 | English | Steel, Maraging, Investment Castings 17Ni - 10Co - 4.6Mo - 0.30Ti - 0.06Al Vacuum Melted Homogenized, Overaged, and Solution Heat Treated - UNS J93010
DoD Adopted |
| 9 | SAE J1861-2007 | 2007-01-01 | English | Air Brake Valve Input-Output Characteristic Requirements |
| 10 | SAE AMS4439F-2007 | 2007-01-01 | English | Magnesium Alloy Castings 4.2Zn - 1.2Rare Earths - 0.7Zr (ZE41A-T5) Precipitation Heat Treated - UNS M16410 |
| 11 | SAE ARP997C-2007 | 2007-01-01 | English | (R) Installation and Stowage Provisions for Emergency Equipment in the Transport Aircraft Passenger Cabin |
| 12 | SAE AMS5337D-2007 | 2007-01-01 | English | Steel, Maraging, Investment Castings 18.5Ni - 9.0Co - 5.0Mo - 0.70Ti - 0.12Al Vacuum Melted Homogenized, Overaged, and Solution Heat Treated - UNS J93150
DoD Adopted |
| 13 | SAE AMS5586G-2007 | 2007-01-01 | English | Nickel Alloy, Corrosion and Heat-Resistant, Welded Tubing 57Ni - 19.5Cr - 13.5Co - 4.2Mo - 2.9Ti - 1.4Al - 0.006B - 0.08Zr Consumable Electrode Remelted or Vacuum Induction Melted, Annealed - UNS N07001
DoD Adopted |
| 14 | SAE AS22073A-2007 | 2007-01-01 | English | (R) CIRCUIT BREAKER, TRIP-FREE, PUSH-PULL 1/2 THRU 20 AMP, TYPE I
DoD Adopted |
| 15 | SAE AS85421 SUP 1-2007 | 2007-01-01 | English | Fittings, Tube, Fluid Systems, Separable, Beam Seal, 3000/4000 psi, General Specification For (Supplement 1)
DoD Adopted |
| 16 | SAE AS5692/1-2007 | 2007-01-01 | English | ARC FAULT CIRCUIT BREAKER, TRIP FREE, PUSH-PULL, FUSIBLE LINK DESIGN, 2 陆 -15 AMPS, TYPE I |
| 17 | SAE SHEETMETAL-2007 | 2007-01-01 | English | Mechanics Modeling of Sheet Metal Forming |
| 18 | SAE AS85421A-2007 | 2007-01-01 | English | (R) Fittings, Tube, Fluid Systems, Separable, Beam Seal, 3000/4000 psi, General Specification For
DoD Adopted |
| 19 | SAE J95-2007 | 2007-01-01 | English | Headlamps for Industrial Equipment |
| 20 | SAE ARP4769A-2007 | 2007-01-01 | English | Crew Rest Container for Main Deck or Lower Deck
ANSI Approved |
| 21 | SAE AMS4407-2007 | 2007-01-01 | English | Aluminum Alloy, Plate (7056-T7651) 9.1Zn - 1.6Cu - 1.9Mg Solution Heat Treated, Stress Relieved, and Overaged - UNS A97056 |
| 22 | SAE AMS6435E-2007 | 2007-01-01 | English | Steel, Sheet, Strip, and Plate 0.75Mn - 0.78Cr - 1.8Ni - 0.35Mo - 0.20V (0.33 - 0.38C)(SAE 4335 Mod) Vacuum Consumable Electrode Melted, Annealed - UNS K33517
DoD Adopted |
| 23 | SAE AMS5773E-2007 | 2007-01-01 | English | Steel, Corrosion-Resistant, Bars, Wire, Forgings, Tubing, and Rings 15Cr - 6.5Ni - 0.75Mo - 0.30 Cb (Nb) - 1.5Cu Consumable Electrode Remelted, Solution Heat Treated Precipitation Hardenable - UNS S45000 |
| 24 | SAE AMS6455J-2007 | 2007-01-01 | English | Steel, Sheet, Strip, and Plate 0.95Cr - 0.22V (0.48 - 0.53C) (SAE 6150) - UNS G61500
DoD Adopted |
| 25 | SAE AMS6434F-2007 | 2007-01-01 | English | Steel, Sheet, Strip, and Plate 0.78Cr - 1.8Ni - 0.35Mo - 0.20V (0.33 - 0.38C)(SAE 4335 Mod) - UNS K33517
DoD Adopted |
| 26 | SAE AS5692/2-2007 | 2007-01-01 | English | ARC FAULT CIRCUIT BREAKER - AIRCRAFT, TRIP FREE, 1-20 AMP, TYPE I |
| 27 | SAE J1029-2007 | 2007-01-01 | English | Lighting and Marking of Construction, Earthmoving Machinery
DoD Adopted |
| 28 | SAE AS5663-2007 | 2007-01-01 | English | Minimum Performance Requirements for Transport Airplane Wheel and Brake Assemblies Using Electric Power Actuation |
| 29 | SAE R-374-2006 | 2006-12-06 | English | LOST FIGHTERS A History of U.S. Jet Fighter Programs That Didnt Make It - To Purchase Call 1-800-854-7179 USA/Canada or 303-397-7956 Worldwide |
| 30 | SAE J1044-2006 | 2006-12-01(R 2012) | English | World Manufacturer Identifier |
| 31 | SAE AS1046C-2006 | 2006-12-01(R 2012) | English | (R) Minimum Standard for Portable Gaseous, Oxygen Equipment |
| 32 | SAE AIR5314-2006 | 2006-12-01(R 2011) | English | Introduction to Generic Open Architecture (GOA) Family of Documents |
| 33 | SAE J1177-2006 | 2006-12-01(R 2002) | English | Hydraulic Excavator Operator Controls
DoD Adopted |
| 34 | SAE AS1046C-2006 | 2006-12-01 | English | (R) Minimum Standard for Portable Gaseous, Oxygen Equipment |
| 35 | SAE J578-2006 | 2006-12-01 | English | Color Specification
DoD Adopted |
| 36 | SAE AS1046C-2006 | 2006-12-01 | English | (R) Minimum Standard for Portable Gaseous, Oxygen Equipment |
| 37 | SAE J1044-2006 | 2006-12-01 | English | (R) World Manufacturer Identifier |
| 38 | SAE AS22759/90B-2006 | 2006-12-01 | English | (R) WIRE, ELECTRICAL, POLYTETRAFLUOROETHYLENE/ POLYIMIDE INSULATED, NORMAL WEIGHT, NICKEL COATED, HIGH STRENGTH OR ULTRA HIGH STRENGTH COPPER, ALLOY, 260 掳C, 600 VOLTS
DoD Adopted |
| 39 | SAE AS5382/4A-2006 | 2006-12-01 | English | CABLE, FIBER OPTIC, SINGLE-MODE, 4.6/125/450 um, HERMETIC COATED, TIGHT BUFFER |
| 40 | SAE AS1046C-2006 | 2006-12-01 | English | (R) Minimum Standard for Portable Gaseous, Oxygen Equipment |
| 41 | SAE AS22759A-2006 | 2006-12-01 | English | (R) Wire, Electrical, Fluoropolymer-Insulated, Copper or Copper Alloy
DoD Adopted |
| 42 | SAE J222-2006 | 2006-12-01 | English | Parking Lamps (Front Position Lamps)
DoD Adopted |
| 43 | SAE AS22759/83B-2006 | 2006-12-01 | English | (R) WIRE, ELECTRICAL, POLYTETRAFLUOROETHYLENE/ POLYIMIDE INSULATED, NORMAL WEIGHT, SILVER COATED, COPPER CONDUCTOR, 200 掳C, 600-VOLT
DoD Adopted |
| 44 | SAE AS22759/80B-2006 | 2006-12-01 | English | (R) WIRE, ELECTRICAL, POLYTETRAFLUOROETHYLENE/ POLYIMIDE INSULATED, LIGHT WEIGHT, TIN COATED, COPPER CONDUCTOR, 150 掳C, 600 VOLTS
DoD Adopted |
| 45 | SAE AIR5314-2006 | 2006-12-01 | English | Introduction to Generic Open Architecture (GOA) Family of Documents |
| 46 | SAE R-303-2006 | 2006-12-01 | English | Diesel Emissions and Their Control - To Purchase Call 1-800-854-7179 USA/Canada or 303-397-7956 Worldwide |
| 47 | SAE AS22759/84B-2006 | 2006-12-01 | English | (R) WIRE, ELECTRICAL, POLYTETRAFLUOROETHYLENE/ POLYIMIDE INSULATED, NORMAL WEIGHT, NICKEL COATED, COPPER CONDUCTOR, 260 掳C, 600-VOLT
DoD Adopted |
| 48 | SAE AS22759/85B-2006 | 2006-12-01 | English | (R) WIRE, ELECTRICAL, POLYTETRAFLUOROETHYLENE/ POLYIMIDE INSULATED, NORMAL WEIGHT, TIN COATED, COPPER CONDUCTOR, 150 掳C, 600-VOLT
DoD Adopted |
| 49 | SAE AS5678-2006 | 2006-12-01 | English | Passive RFID Tags Intended for Aircraft Use |
| 50 | SAE J2468-2006 | 2006-12-01 | English | (R) Road Vehicles - Brake Linings - Compressibility Test Procedure |
| 51 | SAE/TP 2006-01-2568-2006 | 2006-11-21 | English | EMI Effects in Electro-Electronic Equipments/Systems of Aircraft |
| 52 | SAE/TP 2006-01-2878-2006 | 2006-11-21 | English | Description of preliminary Study for Technology Transfer of an Ethanol Mixture Preparation System from Automotive Application to a 4-Cylinder 5.9 liter Aircraft Engine. |
| 53 | SAE/TP 2006-01-2562-2006 | 2006-11-21 | English | Aircraft cabin thermal comfort evaluation using numerical manikins |
| 54 | SAE/TP 2006-01-2551-2006 | 2006-11-21 | English | Measurements and SEA Modeling of the Sound Transmission of Ribbed-stiffened Panels |
| 55 | SAE/TP 2006-01-2882-2006 | 2006-11-21 | English | Crosswind Effects in Rear-Mounted Aircraft Engine Installation |
| 56 | SAE/TP 2006-01-2777-2006 | 2006-11-21 | English | Development of an UAV Aircraft for General Purposes |
| 57 | SAE/TP 2006-01-2818-2006 | 2006-11-21 | English | A Fast Aerodynamic Procedure for a Complete Aircraft Design Using the Know Airfoil Characteristics |
| 58 | SAE/TP 2006-01-2865-2006 | 2006-11-21 | English | Sub-optimal control laws for minimization of take-off distance for aircrafts |
| 59 | SAE/TP 2006-01-2639-2006 | 2006-11-21 | English | Obtainment of beta titanium alloys for aerospace applications by powder metallurgy |
| 60 | SAE/TP 2006-01-2788-2006 | 2006-11-21 | English | Development of equations for longitudinal static stability and control calculus adapted to all-flying tail. |
| 61 | SAE/TP 2006-01-2853-2006 | 2006-11-21 | English | Light Aircraft Ground Steering Simulation |
| 62 | SAE/TP 2006-01-2851-2006 | 2006-11-21 | English | Production of Ti-10V-2Fe-3Al Alloy by Powder Metallurgy for Aerospace Applications |
| 63 | SAE/TP 2006-32-0056-2006 | 2006-11-13 | English | Performance Evaluation of a Mini I.C. Engine |
| 64 | SAE/TP 2006-01-3063-2006 | 2006-11-07 | English | Pool Boiling Experiments Using Surface Micromachined Thermocouples |
| 65 | SAE/TP 2006-01-3061-2006 | 2006-11-07 | English | An Electric Power Generation System for Launch Vehicles |
| 66 | SAE/TP 2006-01-3024-2006 | 2006-11-07 | English | Evaluation of Life Cycle Performance of Lithium Ion Cells for Space Applications |
| 67 | SAE/TP 2006-01-3062-2006 | 2006-11-07 | English | System Evaluation of Cavitation Enhanced Heat Transfer in Microchannels |
| 68 | SAE/TP 2006-01-3088-2006 | 2006-11-07 | English | Advances in Active Power Converter Topologies for Power Quality Solution for More Electric Aircraft |
| 69 | SAE/TP 2006-01-3089-2006 | 2006-11-07 | English | Hybrid Power Generation for Achieving Airship Neutral Buoyancy |
| 70 | SAE/TP 2006-01-3027-2006 | 2006-11-07 | English | High Efficiency Cockpit Instrument Lamp Dimmers, An Overview |
| 71 | SAE/TP 2006-01-3044-2006 | 2006-11-07 | English | Improvements in the Distributed Heterogeneous Simulation of Aircraft Electric Power Systems |
| 72 | SAE/TP 2006-01-3108-2006 | 2006-11-07 | English | Turbomachinery Aero Design; Getting It Right the First Time |
| 73 | SAE/TP 2006-01-3043-2006 | 2006-11-07 | English | Modeling Approach for the Integrated Secondary Electric Power Distribution System with Solid State Power Controllers |
| 74 | SAE/TP 2006-01-3107-2006 | 2006-11-07 | English | Total Battery Management System for Aviation Batteries |
| 75 | SAE/TP 2006-01-3042-2006 | 2006-11-07 | English | Distributed Heterogeneous Simulation of a Hybrid-Electric Vehicle Drive System Using the Simplorer Software Product |
| 76 | SAE/TP 2006-01-3041-2006 | 2006-11-07 | English | Nonlinear Electrical Simulation of High-Power Synchronous Generator System |
| 77 | SAE/TP 2006-01-3040-2006 | 2006-11-07 | English | Transient Turbine Engine Modeling and Real-Time System Integration Prototyping |
| 78 | SAE/TP 2006-01-3039-2006 | 2006-11-07 | English | Electrical Modeling and Simulation with Matlab/Simulink and Graphical User Interface Software |
| 79 | SAE/TP 2006-01-3106-2006 | 2006-11-07 | English | High Temperature Packaging and Pulse Testing of Parallel SiC Thyristors |
| 80 | SAE/TP 2006-01-3105-2006 | 2006-11-07 | English | Applications for High-Temperature (HT) Power Electronic Systems within the Drilling Industry |
| 81 | SAE/TP 2006-01-3038-2006 | 2006-11-07 | English | Modeling Considerations and Stability Analysis of Aerospace Power Systems with Hybrid AC/DC Distribution |
| 82 | SAE/TP 2006-01-3102-2006 | 2006-11-07 | English | Real-time Thermal Observer for Electric Machines |
| 83 | SAE/TP 2006-01-3036-2006 | 2006-11-07 | English | An Automated Average-Value Modeling Methodology for Power Electronic Sources and Loads |
| 84 | SAE/TP 2006-01-3035-2006 | 2006-11-07 | English | Integrated Hardware-in-the-Loop Simulation of a Complex Turbine Engine and Power System |
| 85 | SAE/TP 2006-01-3101-2006 | 2006-11-07 | English | Field Auxiliary Power Unit using Advanced Large Format Lithium-Ion Cells |
| 86 | SAE/TP 2006-01-3028-2006 | 2006-11-07 | English | Aircraft High-Power Semiconductor Line Contactors |
| 87 | SAE/TP 2006-01-3034-2006 | 2006-11-07 | English | Power Management Software Interfaces Standard |
| 88 | SAE/TP 2006-01-3078-2006 | 2006-11-07 | English | Switching Harmonics in a Three-Phase PWM Inverter |
| 89 | SAE/TP 2006-01-3077-2006 | 2006-11-07 | English | Robust Control Techniques Enabling Duty Cycle Experiments Utilizing a 6-DOF Crewstation Motion Base, a Full Scale Combat Hybrid Electric Power System, and Long Distance Internet Communications |
| 90 | SAE/TP 2006-01-3076-2006 | 2006-11-07 | English | High-Reactance Permanent Magnet Machine for High-Performance Power Generation Systems |
| 91 | SAE/TP 2006-01-3074-2006 | 2006-11-07 | English | A 10KW Modular Inverter for 28 VDC to 120/240 VAC Power Conversion |
| 92 | SAE/TP 2006-01-3031-2006 | 2006-11-07 | English | AC-link Converter Topology for Power-Dense AC and DC Applications |
| 93 | SAE/TP 2006-01-3025-2006 | 2006-11-07 | English | High Temperature Battery for Space Applications |
| 94 | SAE/TP 2006-01-3070-2006 | 2006-11-07 | English | A Novel Control Scheme to Increase Electrical Torque of a Drive System for Aircraft Main Engine and APU Start |
| 95 | SAE/TP 2006-01-3068-2006 | 2006-11-07 | English | Effect of Thermal Conductivity and Latent Heat of Vaporization of Liquid on Heat Transfer in Spray Cooling |
| 96 | SAE/TP 2006-01-3023-2006 | 2006-11-07 | English | Advanced Bipolar Lithium Ion Battery |
| 97 | SAE/TP 2006-01-3067-2006 | 2006-11-07 | English | The Heat Transfer Effects of Nanotube Surfaces Treatments and a Means for Growing the Nanotube Coated Surfaces |
| 98 | SAE/TP 2006-01-3066-2006 | 2006-11-07 | English | Aircraft Thermal Management Using Loop Heat Pipes: Experimental Simulation of High Acceleration Environments Using the Centrifuge Table Test Bed |
| 99 | SAE/TP 2006-01-3065-2006 | 2006-11-07 | English | Centrifuge Testing of a Partially-Confined FC-72 Spray |
| 100 | SAE/TP 2006-01-3064-2006 | 2006-11-07 | English | Electrical Force Effects on Spray Cooling |
| 101 | SAE/TP 2006-01-3046-2006 | 2006-11-07 | English | Modeling and Analysis of a Main Engine Start Power Flow |
| 102 | SAE/TP 2006-01-3050-2006 | 2006-11-07 | English | Modeling and Simulation of an Electric Warship Integrated Engineering Plant |
| 103 | SAE/TP 2006-01-3048-2006 | 2006-11-07 | English | Coupled-Circuit Modeling of 3, 6, and 9-Phase Induction Machine Drive Systems |
| 104 | SAE/TP 2006-01-3051-2006 | 2006-11-07 | English | Closed Loop Controlled High Speed Induction Generators Using Adaptive Control Technique |
| 105 | SAE/TP 2006-01-3053-2006 | 2006-11-07 | English | Electrical System Evaluation Platform for Uninhabited Autonomous Vehicles |
| 106 | SAE/TP 2006-01-3054-2006 | 2006-11-07 | English | GCU for Megawatt Class Directed Energy Weapons Pulse Generators |
| 107 | SAE/TP 2006-01-3045-2006 | 2006-11-07 | English | Automated Evolutionary Design of a Hybrid-Electric Vehicle Power System using Distributed Heterogeneous Optimization |
| 108 | SAE/TP 2006-01-3055-2006 | 2006-11-07 | English | The Quest for Oil-Free Gas Turbine Engines |
| 109 | SAE/TP 2006-01-3026-2006 | 2006-11-07 | English | Super NiCd Applications and Mission History |
| 110 | SAE/TP 2006-01-3056-2006 | 2006-11-07 | English | Altitude Performance Test Results for Low Pressure Turbine Mounted Generator |
| 111 | SAE/TP 2006-01-3058-2006 | 2006-11-07 | English | Power Distribution for Spacecraft Payloads that Employ State of the Art Radiation Hardened Integrated Circuits |
| 112 | SAE/TP 2006-01-3059-2006 | 2006-11-07 | English | Multi-Objective Optimization of Spacecraft Electrical Power Subsystem Design/Sizing |
| 113 | SAE/TP 2006-01-3100-2006 | 2006-11-07 | English | The Bipolar Nickel Metal Hydride High Energy Army Silent Watch Battery |
| 114 | SAE/TP 2006-01-3099-2006 | 2006-11-07 | English | 3.2 KWH Battery Pack Using 18 Army Standard Lithium ion Rechargeable Batteries |
| 115 | SAE/TP 2006-01-3098-2006 | 2006-11-07 | English | High Specific Energy Rechargeable Battery for the Tactical Warfighter |
| 116 | SAE/TP 2006-01-3097-2006 | 2006-11-07 | English | Towards Electric Aircraft: Progress under the NASA URETI for Aeropropulsion and Power Technology |
| 117 | SAE/TP 2006-01-3020-2006 | 2006-11-07 | English | The Bipolar Nickel-Metal Hydride Battery for Advanced Transportation and High Voltage Power and Energy Storage Systems |
| 118 | SAE/TP 2006-01-3096-2006 | 2006-11-07 | English | High Temperature Polymer Electrolyte Membrane Fuel Cells (HT-PEMFCs) for Portable Power |
| 119 | SAE/TP 2006-01-3021-2006 | 2006-11-07 | English | SAFT Li-ion Technology for High Rate Applications |
| 120 | SAE/TP 2006-01-3022-2006 | 2006-11-07 | English | Cell Equalization of Lithium Ion Cells |
| 121 | SAE/TP 2006-01-3033-2006 | 2006-11-07 | English | High Power Semiconductor Switching |
| 122 | SAE/TP 2006-01-3095-2006 | 2006-11-07 | English | Reformation of Jet Fuels for Navy Ground Cart Applications |
| 123 | SAE/TP 2006-01-3093-2006 | 2006-11-07 | English | Aeronautical Fuel Cell System Application and Associated Standardization Work |
| 124 | SAE/TP 2006-01-3092-2006 | 2006-11-07 | English | Test Results for a Fuel Cell-Powered Demonstration Aircraft |
| 125 | SAE/TP 2006-01-3091-2006 | 2006-11-07 | English | Aircraft Electrical System Monitoring with Arc Fault Circuit Protection and Automatic Fault Location |
| 126 | SAE/TP 2006-01-3090-2006 | 2006-11-07 | English | Arc Fault Detection through Model Reference Estimation |
| 127 | SAE/TP 2006-01-3086-2006 | 2006-11-07 | English | Power Conversion Technologies for Reducing Harmonics on the More Electric Aircraft |
| 128 | SAE/TP 2006-01-3084-2006 | 2006-11-07 | English | Replacement of Sealed Nickel-Cadmium Batteries on EA-6B Aircraft with Valve Regulated Lead-Acid Batteries |
| 129 | SAE/TP 2006-01-3083-2006 | 2006-11-07 | English | Rechargeable Lithium-Ion Based Batteries and Thermal Management for Airborne High Energy Electric Lasers |
| 130 | SAE/TP 2006-01-3082-2006 | 2006-11-07 | English | NiCd Battery Performance for Aircraft Applications |
| 131 | SAE/TP 2006-01-3081-2006 | 2006-11-07 | English | Aircraft Battery Design Concept for Improved Ultra Low Temperature Performance |
| 132 | SAE/TP 2006-01-3080-2006 | 2006-11-07 | English | E-6 and E-3 Main Battery and Charger Upgrade |
| 133 | SAE/TP 2006-01-3079-2006 | 2006-11-07 | English | Aircraft Battery Servicing Systems |
| 134 | SAE AS7240-2006 | 2006-11-06 | English | Washers, Spring Lock, Carbon Steel, Procurement Specification for - :1992 |
| 135 | SAE AIR5120-2006 | 2006-11-01(R 2014) | English | Engine Monitoring System Reliability and Validity |
| 136 | SAE J1781-2006 | 2006-11-01(R 2013) | English | Ship Systems and Equipment – Materials for Fluid Systems |
| 137 | SAE AS5868A-2006 | 2006-11-01(R 2013) | English | FITTING ASSEMBLY, ADAPTER, BULKHEAD FLARELESS, AXIALLY SWAGED, HYDRAULIC, 5080 PSI |
| 138 | SAE AS861B-2006 | 2006-11-01(R 2012) | English | Minimum General Standards for Oxygen Systems |
| 139 | SAE J2731-2006 | 2006-11-01 | English | Low Speed Enveloping Test with Perpendicular and Inclined Cleats |
| 140 | SAE AS861B-2006 | 2006-11-01 | English | Minimum General Standards for Oxygen Systems |
| 141 | SAE AS5868A-2006 | 2006-11-01 | English | FITTING ASSEMBLY, ADAPTER, BULKHEAD FLARELESS, AXIALLY SWAGED, HYDRAULIC, 5080 PSI |
| 142 | SAE AS116101 THRU AS116150A-2006 | 2006-11-01 | English | (R) SCREW - FLAT FILLISTER, DRILLED HEAD, CADMIUM PLATED, STEEL UNS G87400, 125 KSI MIN .3750-24 UNF-3A
DoD Adopted |
| 143 | SAE J1939-74-2006 | 2006-11-01 | English | Application-Configurable Messaging |
| 144 | SAE AS116051 THRU AS116100A-2006 | 2006-11-01 | English | (R) SCREW - FLAT FILLISTER, DRILLED HEAD, CADMIUM PLATED, STEEL UNS G87400, 125 KSI MIN .3750-16 UNC-3A
DoD Adopted |
| 145 | SAE AS116001 THRU AS116050A-2006 | 2006-11-01 | English | (R) SCREW - FLAT FILLISTER, DRILLED HEAD, CADMIUM PLATED, STEEL UNS G87400, 125 KSI MIN .3125-24 UNF-3A
DoD Adopted |
| 146 | SAE ARP5297-2006 | 2006-11-01 | English | Recommended Qualification Tests for Halogen Miniature Lamps Less Than 35 Watts for Aircraft Applications |
| 147 | SAE AS7241-2006 | 2006-11-01 | English | Washers, Spring Lock, Corrosion Resistant Steel 18Cr - 9Ni (UNS S30200), Procurement Specification for |
| 148 | SAE J2785-2006 | 2006-11-01 | English | Standardization of Color and Verbiage for Fuel Inlet Closures |
| 149 | SAE J2747-2006 | 2006-11-01 | English | Hydraulic Pump Airborne Noise Bench Test |
| 150 | SAE ARP4156B-2006 | 2006-11-01 | English | Color-Coded Incandescent Flange Base T-1 and T-1 3/4 Lamps for Voltage Identification |
| 151 | SAE AS861B-2006 | 2006-11-01 | English | Minimum General Standards for Oxygen Systems |
| 152 | SAE J1781-2006 | 2006-11-01 | English | (R) Ship Systems and Equipment 鈥?Materials for Fluid Systems
DoD Adopted |
| 153 | SAE USCAR-30-2006 | 2006-11-01 | English | Performance Specification for Automotive Universal Serial Bus (USB) Connection System |
| 154 | SAE J703-2006 | 2006-11-01 | English | Fuel Systems - Truck and Truck Tractors |
| 155 | SAE J357-2006 | 2006-11-01 | English | Physical and Chemical Properties of Engine Oils |
| 156 | SAE ARP5107B-2006 | 2006-11-01 | English | Guidelines for Time-Limited-Dispatch (TLD) Analysis for Electronic Engine Control Systems |
| 157 | SAE AS861B-2006 | 2006-11-01 | English | Minimum General Standards for Oxygen Systems |
| 158 | SAE J1577-2006 | 2006-11-01 | English | Replaceable Motorcycle Headlamp Bulbs |
| 159 | SAE ARP1256C-2006 | 2006-11-01 | English | (R) Procedure for the Continuous Sampling and Measurement of Gaseous Emissions from Aircraft Turbine Engines
DoD Adopted |
| 160 | SAE AIR5120-2006 | 2006-11-01 | English | Engine Monitoring System Reliability and Validity |
| 161 | SAE R-339-2006 | 2006-10-27 | English | Introduction to Engine Valvetrains - To Purchase Call 1-800-854-7179 USA/Canada or 303-397-7956 Worldwide |
| 162 | SAE R-359-2006 | 2006-10-23 | English | Technologies for Near-Zero-Emission Gasoline-Powered Vehicles - To Purchase Call 1-800-854-7179 USA/Canada or 303-397-7956 Worldwide |
| 163 | SAE AMS5682E-2006 | 2006-10-01(R 2018) | English | Nickel Alloy, Corrosion and Heat-Resistant, Welding Wire 78Ni - 20Cr - UNS 06003 |
| 164 | SAE AS5643A-2006 | 2006-10-01(R 2013) | English | IEEE-1394b Interface Requirements for Military and Aerospace Vehicle Applications |
| 165 | SAE ARP5151-2006 | 2006-10-01(R 2013) | English | Safety Assessment of General Aviation Airplanes and Rotorcraft in Commercial Service |
| 166 | SAE AMS5905B-2006 | 2006-10-01(R 2012) | English | Steel, Corrosion Resistant, Sheet and Strip 18Cr - 9.0Ni (SAE 30302) Cold Rolled, 3/4 Hard, 175 ksi (1207 MPa) Tensile Strength - UNS S30200
DoD Adopted |
| 167 | SAE AMS5635F-2006 | 2006-10-01(R 2012) | English | Steel, Corrosion-Resistant, Bars, Wire, and Forgings 18Cr - 9Ni - 0.21Pb (303Pb) Free-Machining, Solution Heat Treated - UNS S30360
DoD Adopted |
| 168 | SAE AMS5682E-2006 | 2006-10-01(R 2012) | English | Nickel Alloy, Corrosion and Heat-Resistant, Welding Wire 78Ni - 20Cr - UNS 06003
DoD Adopted |
| 169 | SAE AMS5904B-2006 | 2006-10-01(R 2012) | English | Steel, Corrosion-Resistant, Sheet and Strip 18Cr - 9.0Ni (SAE 30302) Cold Rolled, 1/2 Hard, 150 ksi (1034 MPa) Tensile Strength - UNS S30200
DoD Adopted |
| 170 | SAE AMS5903B-2006 | 2006-10-01(R 2012) | English | Steel, Corrosion-Resistant, Sheet, Strip, and Plate 18Cr - 9.0Ni (SAE 30302) Cold Rolled, 1/4 Hard, 125 ksi (862 MPa) Tensile Strength - UNS S30200
DoD Adopted |
| 171 | SAE AMS4297A-2006 | 2006-10-01(R 2011) | English | Aluminum Alloy Sheet 4.4Cu - 1.5Mg - 0.60Mn (2024; -T4 Flat Sheet) Solution Heat Treated, High Formability - UNS A92024 |
| 172 | SAE AMS4444D-2006 | 2006-10-01(R 2000) | English | Magnesium Alloy Castings, Sand 6.0Zn - 0.80Zr (ZK61A-T5) Precipitation Heat Treated |
| 173 | SAE AMS4800E-2006 | 2006-10-01(R 2000) | English | Bearings, Babbitt 91Sn - 4.5Sb - 4.5Cu
DoD Adopted |
| 174 | SAE AMS5905B-2006 | 2006-10-01 | English | Steel, Corrosion Resistant, Sheet and Strip 18Cr - 9.0Ni (SAE 30302) Cold Rolled, 3/4 Hard, 175 ksi (1207 MPa) Tensile Strength - UNS S30200
DoD Adopted |
| 175 | SAE AS5643A-2006 | 2006-10-01 | English | IEEE -1394b Interface Requirements for Military and Aerospace Vehicle Applications |
| 176 | SAE AMS4300C-2006 | 2006-10-01 | English | Boron-Aluminum Composite Sheet 50 v/o 5.6B, 6061-0, For Diffusion Bonding
DoD Adopted |
| 177 | SAE J2665-2006 | 2006-10-01 | English | Test Procedure to Measure the Fuel Permeability of Materials by the Cup Weight Loss Method |
| 178 | SAE AMS5682E-2006 | 2006-10-01 | English | (R) Nickel Alloy, Corrosion and Heat-Resistant, Welding Wire 78Ni - 20Cr
DoD Adopted |
| 179 | SAE J1113-1-2006 | 2006-10-01 | English | Electromagnetic Compatibility Measurement Procedures and Limits for Components of Vehicles, Boats (up to 15 m), and Machines (Except Aircraft) (16.6 Hz to 18 GHz) |
| 180 | SAE AS25435A-2006 | 2006-10-01 | English | TERMINAL-LUG, CRIMP STYLE, STRAIGHT TYPE, FOR ALUMINUM AIRCRAFT WIRE, CLASS 1 - FSC 5940 |
| 181 | SAE AMS4008K-2006 | 2006-10-01 | English | Aluminum Alloy, Sheet and Plate 1.25Mn - 0.12Cu (3003-H14) Strain Hardened - UNS A93003 |
| 182 | SAE ARP5151-2006 | 2006-10-01 | English | Safety Assessment of General Aviation Airplanes and Rotorcraft in Commercial Service |
| 183 | SAE AMS4010C-2006 | 2006-10-01 | English | Aluminum Alloy Foil 1.2Mn - 0.12Cu (3003-H18) - UNS A93003
DoD Adopted |
| 184 | SAE AMS4297A-2006 | 2006-10-01 | English | Aluminum Alloy Sheet 4.4Cu - 1.5Mg - 0.60Mn (2024; -T4 Flat Sheet) Solution Heat Treated, High Formability - UNS A92024 |
| 185 | SAE AMS4422P-2006 | 2006-10-01 | English | Magnesium Alloy Castings, Sand 6.0Al - 3.0Zn (AZ63 - T4) Solution Heat Treated |
| 186 | SAE AMS5903B-2006 | 2006-10-01 | English | Steel, Corrosion Resistant, Sheet, Strip, and Plate 18Cr - 9.0Ni (SAE 30302) Cold Rolled, 1/4 Hard, 125 ksi (862 MPa) Tensile Strength - UNS S30200
DoD Adopted |
| 187 | SAE AMS4420N-2006 | 2006-10-01 | English | Magnesium Alloy Castings, Sand 6Al - 3Zn (AZ63A-F) as Cast - UNS M11630 |
| 188 | SAE J1105-2006 | 2006-10-01 | English | (R) HornForward WarningElectricPerformance, Test, and Application |
| 189 | SAE AMS5904B-2006 | 2006-10-01 | English | Steel, Corrosion Resistant, Sheet and Strip 18Cr - 9.0Ni (SAE 30302) Cold Rolled, 1/2 Hard, 150 ksi (1034 MPa) Tensile Strength - UNS S30200
DoD Adopted |
| 190 | SAE AS70991A-2006 | 2006-10-01 | English | Terminals: Lug and Splice, Crimp Style, Aluminum, For Aluminum Aircraft Wire - FSC 5940
DoD Adopted |
| 191 | SAE AMS4816D-2006 | 2006-10-01 | English | Bearings, Silver-Clad Steel Strip - FSC 3120 |
| 192 | SAE AMS6485H-2006 | 2006-10-01 | English | Steel Bars and Forgings 5.0Cr - 1.3Mo - 0.50V (0.38 - 0.43C) |
| 193 | SAE J2776-2006 | 2006-10-01 | English | Refrigerant Purity and Container Requirements for New HFC-134a 1,1,1,2Tetrafluoroethane Refrigerant Used in Mobile Air-Conditioning Systems |
| 194 | SAE AMS5635F-2006 | 2006-10-01 | English | Steel, Corrosion-Resistant, Bars, Wire, and Forgings 18Cr - 9Ni - 0.21Pb (303Pb) Free-Machining, Solution Heat Treated - UNS S30360
DoD Adopted |
| 195 | SAE AMS4036K-2006 | 2006-10-01 | English | Aluminum Alloy Sheet and Plate, Alclad One Side 4.4Cu - 1.5Mg - 0.60Mn Alclad One Side 2024 and 1-1/2% Alclad One Side 2024-T3 Sheet 1-1/2% Alclad One Side 2024-T351 Plate - UNS A82024
DoD Adopted |
| 196 | SAE J2748-2006 | 2006-10-01 | English | VHDL-AMS Statistical Analysis Packages |
| 197 | SAE AMS4384J-2006 | 2006-10-01 | English | Magnesium Alloy, Sheet and Plate 3.2Th - 0.70Zr Annealed Recrystallized - UNS M13310 |
| 198 | SAE AMS2644E-2006 | 2006-10-01 | English | Inspection Material, Penetrant
DoD Adopted |
| 199 | SAE AMS4383F-2006 | 2006-10-01 | English | Magnesium Alloy, Sheet and Plate 2.0Th - 0.78Mn Solution Heat Treated, Cold Worked, and Precipitation Heat Treated - UNS M13210 |
| 200 | SAE AMS4385K-2006 | 2006-10-01 | English | Magnesium Alloy, Sheet and Plate 3.2Th - 0.70Zr Cold Rolled and Partially Annealed - UNS M13310 |
| 201 | SAE AS25439A-2006 | 2006-10-01 | English | SPLICE-PERMANENT CRIMP STYLE, 2 WAY TYPE FOR ALUMINUM AIRCRAFT WIRE, CLASS 1 - FSC 5940 |
| 202 | SAE J1752-1-2006 | 2006-10-01 | English | (R) Electromagnetic Compatibility Measurement Procedures for Integrated Circuits - Integrated Circuit EMC Measurement Procedures - General and Definitions |
| 203 | SAE AS25436A-2006 | 2006-10-01 | English | TERMINAL-LUG, CRIMP STYLE, 90掳 UPRIGHT TYPE, FOR ALUMINUM AIRCRAFT WIRE, CLASS 1 - FSC 5940 |
| 204 | SAE AMS7488E-2006 | 2006-10-01 | English | Rings, Flash Welded Aluminum and Aluminum Alloys
DoD Adopted |
| 205 | SAE AMS4967J-2006 | 2006-10-01 | English | Titanium Alloy, Bars, Wire, Forgings, and Rings 6.0Al - 4.0V Annealed, Heat Treatable - UNS R56400
DoD Adopted |
| 206 | SAE/TP 2006-01-3177-2006 | 2006-09-12 | English | A Comparison between Indoor GPS versus Laser Tracking Metrology for Robotic Drilling |
| 207 | SAE/TP 2006-01-3138-2006 | 2006-09-12 | English | High Speed Tow Placement System for Complex Surfaces with Cut / Clamp / & Restart Capabilities at 85 m/min (3350 IPM) |
| 208 | SAE/TP 2006-01-3179-2006 | 2006-09-12 | English | Advances in Testing and Analytical Simulation Methodologies to Support Design and Structural Integrity Assessment of Large Monolithic Parts |
| 209 | SAE/TP 2006-01-3178-2006 | 2006-09-12 | English | Developments in Bond Assisted Single Step Assembly |
| 210 | SAE/TP 2006-01-3125-2006 | 2006-09-12 | English | Various Types of RRJ Aircraft Joints and Associated Features of Their Performance |
| 211 | SAE/TP 2006-01-3137-2006 | 2006-09-12 | English | Portable Automation for Feeding and Installing Fasteners |
| 212 | SAE/TP 2006-01-3141-2006 | 2006-09-12 | English | Snake-Arm Robots: A New Approach to Aircraft Assembly |
| 213 | SAE/TP 2006-01-3124-2006 | 2006-09-12 | English | Full Flexible Multi Task Robot Cell for Complex 360° Aircraft Structures |
| 214 | SAE/TP 2006-01-3173-2006 | 2006-09-12 | English | Edge Trimming of CFRP with Diamond Interlocking Tools |
| 215 | SAE/TP 2006-01-3123-2006 | 2006-09-12 | English | Join Cell for the G150 Aircraft |
| 216 | SAE/TP 2006-01-3121-2006 | 2006-09-12 | English | The Application of Lean Six Sigma at Brush Wellman Inc. |
| 217 | SAE/TP 2006-01-3175-2006 | 2006-09-12 | English | New Concept of Artificial Vision System Applicability to Measure and Control the Quality of Automated Fastening |
| 218 | SAE/TP 2006-01-3176-2006 | 2006-09-12 | English | Dual Electric Spindle Retrofit for Wing Riveters |
| 219 | SAE/TP 2006-01-3172-2006 | 2006-09-12 | English | Drilling of Thick Composite Structures State of the Art |
| 220 | SAE/TP 2006-01-3171-2006 | 2006-09-12 | English | Residual Stress Prediction for Part Distortion Modeling |
| 221 | SAE/TP 2006-01-3155-2006 | 2006-09-12 | English | Effects of Coating Tribology on Fastener Single and Double Shear Strength |
| 222 | SAE/TP 2006-01-3174-2006 | 2006-09-12 | English | A New Approach for Best Fit Assembly Based on the Behaviour of Components |
| 223 | SAE/TP 2006-01-3130-2006 | 2006-09-12 | English | “RoHS” Compliant Chrome – Free Conversion Coating for Aerospace Manufacturing |
| 224 | SAE/TP 2006-01-3156-2006 | 2006-09-12 | English | SLAM, A Fast High Volume Additive Manufacturing Concept by Impact Welding; Application to Ti6Al4V Alloy |
| 225 | SAE/TP 2006-01-3169-2006 | 2006-09-12 | English | Evaluation of Alternatives to Electrodeposited Cadmium for Threaded Fastener Applications |
| 226 | SAE/TP 2006-01-3160-2006 | 2006-09-12 | English | Optimizing Semi-automated Threaded Fastener Installation with Remote Data Collection |
| 227 | SAE/TP 2006-01-3120-2006 | 2006-09-12 | English | A Superior Method of Installing Aircraft Fittings and Hardware |
| 228 | SAE/TP 2006-01-3132-2006 | 2006-09-12 | English | A Win-Win Approach to Supplier Management in Manufacturing |
| 229 | SAE/TP 2006-01-3170-2006 | 2006-09-12 | English | True Offset Fastening |
| 230 | SAE/TP 2006-01-3143-2006 | 2006-09-12 | English | Automation for the Assembly of the Bottom Wing Panels on Stringers for the A320 |
| 231 | SAE/TP 2006-01-3167-2006 | 2006-09-12 | English | A Novel Means of Software Compensation for Robots and Machine Tools |
| 232 | SAE/TP 2006-01-3153-2006 | 2006-09-12 | English | CVD Diamond Coated Rotating Tools for Composite Machining |
| 233 | SAE/TP 2006-01-3129-2006 | 2006-09-12 | English | Effect of Surface Processes on High-Cycle Fatigue Life of Titanium Alloys |
| 234 | SAE/TP 2006-01-3142-2006 | 2006-09-12 | English | An Automated Fuselage Panel Assembly and Riveting Cell – Validation and Testing |
| 235 | SAE/TP 2006-01-3133-2006 | 2006-09-12 | English | Deployment of a Global Kanban System |
| 236 | SAE/TP 2006-01-3131-2006 | 2006-09-12 | English | Studying the Effect of Pad Contact Surface on the Frictional Behavior and Acoustic Noise Response for Heavy Duty Vehicle Brakes Using FAST Machine |
| 237 | SAE/TP 2006-01-3165-2006 | 2006-09-12 | English | The Advanced Thread Locking Mechanism |
| 238 | SAE/TP 2006-01-3154-2006 | 2006-09-12 | English | Development of Metal-Matrix Nano-Composite Materials for Advanced Aerospace Fastener Technology |
| 239 | SAE/TP 2006-01-3164-2006 | 2006-09-12 | English | Out of Autoclave Processable Prepregs and Resin Films — An Overview of Recent Developments and Shared Databases |
| 240 | SAE/TP 2006-01-3152-2006 | 2006-09-12 | English | Development and Deployment of Orbital Drilling at Boeing |
| 241 | SAE/TP 2006-01-3151-2006 | 2006-09-12 | English | Non-Metallic Fastener Technology Developed for the Temporary Assembly of Composite Structure |
| 242 | SAE/TP 2006-01-3127-2006 | 2006-09-12 | English | Simply Supported Retractable Top Beam for Wing Major Assembly Jig |
| 243 | SAE/TP 2006-01-3150-2006 | 2006-09-12 | English | Simulation at the Heart of an Automated Aerospace Manufacturing Process |
| 244 | SAE/TP 2006-01-3162-2006 | 2006-09-12 | English | Composite Automatic Wing Drilling Equipment (CAWDE) |
| 245 | SAE/TP 2006-01-3144-2006 | 2006-09-12 | English | The Key to Aerospace Automation |
| 246 | SAE/TP 2006-01-3126-2006 | 2006-09-12 | English | IFAC (Integrated Fuselage Assembly Cell) |
| 247 | SAE/TP 2006-01-3163-2006 | 2006-09-12 | English | Laser Consolidation – A One-Step Manufacturing Process for Making Net-Shaped Functional Aerospace Components |
| 248 | SAE/TP 2006-01-3136-2006 | 2006-09-12 | English | AMEC SPIE’s High Dynamics Automatic Drilling and Riveting General Purpose System |
| 249 | SAE AMS5399D-2006 | 2006-09-01(R 2018) | English | Nickel Alloy, Corrosion and Heat-Resistant, Investment Castings 52Ni - 19Cr - 11Co - 9.8Mo - 3.2Ti - 1.6Al - 0.006B Vacuum-Melted, Vacuum-Cast, Solution Heat Treated - UNS N07041 |
| 250 | SAE AMS5547H-2006 | 2006-09-01(R 2018) | English | Steel, Corrosion and Heat-Resistant, Sheet and Strip 15.5Cr - 4.5Ni - 2.9Mo - 0.10N Solution Heat Treated - UNS S35500 |
| 251 | SAE AMS5837G-2006 | 2006-09-01(R 2018) | English | Nickel Alloy, Corrosion and Heat-Resistant, Welding Wire 62Ni - 21.5Cr - 9.0Mo - 3.7Cb(Nb) - UNS N06625 |
| 252 | SAE AMS5732J-2006 | 2006-09-01(R 2018) | English | Steel, Corrosion and Heat-Resistant, Bars, Wire, Forgings, Tubing, and Rings 15Cr - 25.5Ni - 1.2Mo - 2.1Ti - 0.006B - 0.30V Consumable Electrode Melted 1800 °F (982 °C) Solution and Precipitation Heat Treated - UNS S66286 |
| 253 | SAE AS1791D-2006 | 2006-09-01(R 2015) | English | WIRE, RETAINER - TUBE COUPLING NUT(DoD Adopted) |
| 254 | SAE AS5830-2006 | 2006-09-01(R 2013) | English | Coupling Assembly, Threadless, Flexible, Fixed Cavity, Current Carrying, Self-Bonding, Procurement Specification |
| 255 | SAE AS5831-2006 | 2006-09-01(R 2013) | English | ASSEMBLED COUPLING, THREADLESS-FLEXIBLE, FIXED CAVITY, CURRENT CARRYING, SELF BONDING, ENVELOPE DIMENSIONS |
| 256 | SAE AS5832-2006 | 2006-09-01(R 2013) | English | ASSEMBLED COUPLING COMPONENTS, THREADLESS-FLEXIBLE, FIXED CAVITY, CURRENT CARRYING, SELF BONDING |
| 257 | SAE AS5833-2006 | 2006-09-01(R 2013) | English | MALE FERRULE, THREADLESS-FLEXIBLE, FIXED CAVITY, CURRENT CARRYING, SELF BONDING, SWAGED |
| 258 | SAE AS5834-2006 | 2006-09-01(R 2013) | English | SLEEVE, THREADLESS-FLEXIBLE, FIXED CAVITY, CURRENT CARRYING, SELF BONDING |
| 259 | SAE AS5835-2006 | 2006-09-01(R 2013) | English | COUPLING BODY, THREADLESS-FLEXIBLE, FIXED CAVITY, CURRENT CARRYING, SELF BONDING |
| 260 | SAE AS5836-2006 | 2006-09-01(R 2013) | English | FITTING END, THREADLESS-FLEXIBLE, FIXED CAVITY, CURRENT CARRYING, SELF BONDING MALE AND FEMALE DESIGN STANDARD |
| 261 | SAE AS5837-2006 | 2006-09-01(R 2013) | English | MALE FERRULE, THREADLESS-FLEXIBLE, FIXED CAVITY, CURRENT CARRYING, SELF BONDING, BUTT WELDED |
| 262 | SAE AS5838-2006 | 2006-09-01(R 2013) | English | FEMALE FERRULE, THREADLESS-FLEXIBLE, FIXED CAVITY, CURRENT CARRYING, SELF BONDING, SWAGED |
| 263 | SAE AS5839-2006 | 2006-09-01(R 2013) | English | FEMALE FERRULE, THREADLESS-FLEXIBLE, FIXED CAVITY, CURRENT CARRYING, SELF BONDING, BUTT WELDED |
| 264 | SAE AMS3846D-2006 | 2006-09-01(R 2013) | English | Cloth, Quarts Finished for Resin Laminates |
| 265 | SAE AMS5611F-2006 | 2006-09-01(R 2013) | English | Steel, Corrosion and Heat Resistant, Bars, Wire, Forgings, Tubing, and Rings 12Cr Ferrite Controlled, Consumable Electrode Melted - UNS S41001 |
| 266 | SAE AMS2251H-2006 | 2006-09-01(R 2013) | English | Tolerances Low-Alloy Steel Bars(DoD Adopted) |
| 267 | SAE AIR5696-2006 | 2006-09-01(R 2013) | English | Aerospace Fluid Power - FAA Regulatory History - Transport Airplane Hydraulic Systems |
| 268 | SAE ARP5056-2006 | 2006-09-01(R 2013) | English | Flight Crew Interface Considerations in the Flight Deck Design Process for Part 25 Aircraft |
| 269 | SAE AS87132-2006 | 2006-09-01(R 2012) | English | Lubricant, Cetyl Alcohol, 1-Hexadecanol, Application to Fasteners |
| 270 | SAE AMS4402-2006 | 2006-09-01(R 2012) | English | Aluminum Alloy, Extruded Profiles (2024-T432) 4.4Cu - 1.5Mg - 0.6Mn Annealed, Stretch Formed, Solution Heat Treated and Stress Relieved by Stretching - UNS A92027 |
| 271 | SAE AMS5650F-2006 | 2006-09-01(R 2012) | English | Steel, Corrosion and Heat-Resistant, Bars, Wire, Forgings, Tubing, and Rings 23Cr - 13.5Ni (SAE 30309S) Solution Heat Treated - UNS S30908
DoD Adopted |
| 272 | SAE AMS5631E-2006 | 2006-09-01(R 2012) | English | Steel, Corrosion-Resistant, Bars and Forgings 17Cr (0.60 - 0.75C) (SAE 51440A) - UNS S44002 |
| 273 | SAE AMS5620G-2006 | 2006-09-01(R 2012) | English | Steel, Corrosion and Heat-Resistant, Bars, Wire, and Forgings 13Cr (0.30 - 0.40C) (SAE 51420F, 51420FSe) Free-Machining Grade - UNS S42020 (Type 2); S42023 (Type 1)
DoD Adopted |
| 274 | SAE AMS5910B-2006 | 2006-09-01(R 2012) | English | Steel, Corrosion-Resistant, Sheet, Strip, and Plate 19Cr - 9.2Ni (SAE 30304) Cold Rolled, 125 ksi (862 MPa) Tensile Strength - UNS S30400
DoD Adopted |
| 275 | SAE AMS5837G-2006 | 2006-09-01(R 2012) | English | Nickel Alloy, Corrosion and Heat-Resistant, Welding Wire 62Ni - 21.5Cr - 9.0Mo - 3.7Cb(Nb) - UNS N06625
DoD Adopted |
| 276 | SAE AMS5547H-2006 | 2006-09-01(R 2012) | English | Steel, Corrosion and Heat-Resistant, Sheet and Strip 15.5Cr - 4.5Ni - 2.9Mo - 0.10N Solution Heat Treated - UNS S35500
DoD Adopted |
| 277 | SAE AMS5399D-2006 | 2006-09-01(R 2012) | English | Nickel Alloy, Corrosion and Heat-Resistant, Investment Castings 52Ni - 19Cr - 11Co - 9.8Mo - 3.2Ti - 1.6Al - 0.006B Vacuum-Melted, Vacuum-Cast, Solution Heat Treated - UNS N07041
DoD Adopted |
| 278 | SAE AMS5907B-2006 | 2006-09-01(R 2012) | English | Steel, Corrosion and Heat Resistant, Sheet, Strip, and Plate 17Cr - 12Ni - 2.5Mo (SAE 30316) Cold Rolled, 1/4 Hard, 125 ksi (862 MPa) Tensile Strength - UNS S31600
DoD Adopted |
| 279 | SAE AMS4016L-2006 | 2006-09-01(R 2012) | English | Aluminum Alloy, Sheet and Plate 2.5Mg - 0.25Cr (5052-H32) Strain Hardened, Quarter-Hard, and Stabilized - UNS A95052 |
| 280 | SAE AMS7735D-2006 | 2006-09-01(R 2012) | English | Alloy Wire, Round 35Pd - 30Ag - 14Cu - 10Au - 10Pt - 0.85Zn Solution Heat Treated - UNS P03300 |
| 281 | SAE AMS5906B-2006 | 2006-09-01(R 2012) | English | Steel, Corrosion Resistant, Sheet Strip 18Cr - 9.0Ni (SAE 30302) Cold Rolled, Full Hard, 185 ksi (1276 MPa) Tensile Strength - UNS S30200
DoD Adopted |
| 282 | SAE AMS5719D-2006 | 2006-09-01(R 2012) | English | Steel Bars, Wire, Forgings, Tubing, Rings, and Extrusions, Corrosion-Resistant 11.8Cr - 2.5Ni - 1.8Mo - 0.33V (0.08 - 0.15C) Annealed, Vacuum Arc or Electroslag Remelted - UNS S64152
DoD Adopted |
| 283 | SAE ARP5674-2006 | 2006-09-01(R 2012) | English | Safety Considerations for Aircraft-Mounted Lasers Projected Into the Navigable Airspace |
| 284 | SAE AMS5532G-2006 | 2006-09-01(R 2012) | English | Iron Alloy, Corrosion and Heat Resistant, Sheet, Strip, and Plate 30Fe - 21Cr - 20Ni - 20Co - 3.0Mo - 2.5W - 1.0Cb - 0.15N Solution Heat Treated - UNS R30155 |
| 285 | SAE AMS4340E-2006 | 2006-09-01(R 2011) | English | Aluminum Alloy, Extrusions 6.2Zn - 2.3Cu - 2.2Mg - 0.12Zr (7050-T76511) Solution Heat Treated, Stress Relieved, Straightened, and Overaged - UNS A97050 |
| 286 | SAE AMS4349D-2006 | 2006-09-01(R 2011) | English | Core, Honeycomb, Aluminum Alloy, Corrosion Inhibited For Sandwich Construction 5056, 350 (177) |
| 287 | SAE AMS4341E-2006 | 2006-09-01(R 2011) | English | Aluminum Alloy, Extrusions 6.2Zn - 2.3Cu - 2.2Mg - 0.12Zr (7050-T73511) Solution Heat Treated, Stress Relieved by Stretching, Straightened, and Overaged - UNS A97050 |
| 288 | SAE AMS2615F-2006 | 2006-09-01(R 2011) | English | Pressure Testing, Hydraulic Pressure as Specified |
| 289 | SAE AMS4337A-2006 | 2006-09-01(R 2011) | English | Aluminum Alloy, Extruded Profiles (7055-T77511) 8.0Zn - 2.3Cu - 2.0Mg - 0.16Zr Solution Heat Treated, Stress Relieved, and Overaged - UNS A97055 |
| 290 | SAE AMS4348D-2006 | 2006-09-01(R 2011) | English | Core, Honeycomb, Aluminum Alloy, Corrosion Inhibited For Sandwich Construction 5052, 350 (177) |
| 291 | SAE AMS5110J-2006 | 2006-09-01(R 2011) | English | Carbon Steel, Wire and Springs 0.75 - 0.88C (SAE 1080) Spring Temper, Cold Drawn - UNS G10800
DoD Adopted |
| 292 | SAE AMS7713B-2006 | 2006-09-01(R 2011) | English | Iron, Electrical, Bar and Strip Cold Finished, Annealed |
| 293 | SAE AMS4177D-2006 | 2006-09-01(R 2011) | English | Core, Flexible Honeycomb, Aluminum Alloy For Sandwich Construction 5056, 350 (177) |
| 294 | SAE AMS4254B-2006 | 2006-09-01(R 2000) | English | Aluminum Alloy, Aramid Fiber Reinforced, Laminated Sheet 4.4Cu - 1.5Mg - 0.6Mn (2024-T3) 3, 5, 7, or 9 Ply |
| 295 | SAE AMS4258A-2006 | 2006-09-01(R 2000) | English | Laminated Sheet, Aluminum Alloy, Aramid Fiber Reinforced 5.7Zn - 2.2Mg - 1.6Cu - 0.22Cr (Alclad, One Side 7475- T761) 5 or 7 Ply |
| 296 | SAE AMS4302B-2006 | 2006-09-01(R 2000) | English | Aluminum Alloy, Laminated Sheet, Aramid Fiber Reinforced 5.7Zn - 2.2Mg - 1.6Cu - 0.22Cr (7475-T761) 3, 5, 7, or 9 Ply |
| 297 | SAE J551-4-2006 | 2006-09-01(R 2000) | English | Test Limits and Methods of Measurement of Radio Disturbance Characteristics of Vehicles and Devices, Broadband and Narrowband, 150 kHz to 1000 MHz |
| 298 | SAE AMS4238E-2006 | 2006-09-01(R 1995) | English | Aluminum Alloy Castings, Sand 6.8Mg - 0.18Ti - 0.18Mn (535.0-F) as Cast |
| 299 | SAE AMS7510/1B-2006 | 2006-09-01 | English | Magnets, Rare-Earth/Cobalt, Permanent Samarium-Cobalt, 33/67 - 15 (119) 250 |
| 300 | SAE AMS5906B-2006 | 2006-09-01 | English | Steel, Corrosion Resistant, Sheet Strip 18Cr - 9.0Ni (SAE 30302) Cold Rolled, Full Hard, 185 ksi (1276 MPa) Tensile Strength - UNS S30200
DoD Adopted |
| 301 | SAE AMS5907B-2006 | 2006-09-01 | English | Steel, Corrosion and Heat Resistant, Sheet, Strip, and Plate 17Cr - 12Ni - 2.5Mo (SAE 30316) Cold Rolled, 1/4 Hard, 125 ksi (862 MPa) Tensile Strength - UNS S31600
DoD Adopted |
| 302 | SAE AMS5910B-2006 | 2006-09-01 | English | Steel, Corrosion Resistant, Sheet, Strip, and Plate 19Cr - 9.2Ni (SAE 30304) Cold Rolled, 125 ksi (862 MPa) Tensile Strength - UNS S30400
DoD Adopted |
| 303 | SAE AMS6356F-2006 | 2006-09-01 | English | Steel, Sheet, Strip, and Plate 0.95Cr - 0.20Mo - (0.30 - 0.35C)(SAE 4132) - UNS G41300
DoD Adopted |
| 304 | SAE AMS6464G-2006 | 2006-09-01 | English | Welding Electrodes, Covered, Steel 1.05Mo - 0.20V (0.06 - 0.12C) - UNS W10013 |
| 305 | SAE AMS6543D-2006 | 2006-09-01 | English | Steel, Bars and Forgings, Maraging 2.0Cr - 10Ni - 8.0Co - 1.0Mo (0.10 - 0.14C)(HY-180) Double Vacuum Melted, Solution Heat Treated - UNS K91970
DoD Adopted |
| 306 | SAE AMS7713B-2006 | 2006-09-01 | English | Iron, Electrical, Bar and Strip Cold Finished, Annealed |
| 307 | SAE AMS7735D-2006 | 2006-09-01 | English | Alloy Wire, Round 35Pd - 30Ag - 14Cu - 10Au - 10Pt - 0.85Zn Solution Heat Treated - UNS P03300 |
| 308 | SAE AMS5605E-2006 | 2006-09-01 | English | Nickel Alloy, Corrosion and Heat Resistant, Sheet, Strip, and Plate 41.5Ni - 16Cr - 37Fe - 2.9Cb - 1.8Ti Consumable Electrode or Vacuum Induction Melted 1800 Degrees F (982 Degrees C) Solution Heat Treated - UNS N09706 |
| 309 | SAE AMS5523F-2006 | 2006-09-01 | English | Steel, Corrosion and Heat-Resistant, Sheet, Strip, and Plate 23Cr - 13.5Ni (SAE 30309S) Solution Heat Treated - UNS S30908
DoD Adopted |
| 310 | SAE AMS5521H-2006 | 2006-09-01 | English | Steel, Corrosion and Heat Resistant, Sheet, Strip, and Plate 25Cr - 20Ni (SAE 30310S) Solution Heat Treated - UNS S31008
DoD Adopted |
| 311 | SAE AMS5442-2006 | 2006-09-01 | English | Nickel Alloy, Corrosion and Heat-Resistant, Bars, Forgings, and Rings Ni - 18Cr - 2.8Mo - 5.5Cb(Nb) - 0.70Ti - 1.50Al - 10Fe - 9Co - 1W Consumable Electrode Remelted or Vacuum Induction Melted 1775 degrees F (968 degrees C) Solution and Precipitation Heat Treated - UNS N07818 |
| 312 | SAE ARP4087B-2006 | 2006-09-01 | English | Wing Inspection Lights - Design Criteria |
| 313 | SAE ARP5056-2006 | 2006-09-01 | English | Flight Crew Interface Considerations in the Flight Deck Design Process for Part 25 Aircraft |
| 314 | SAE AMS4930F-2006 | 2006-09-01 | English | Titanium Alloy Bars, Wire, Forgings, and Rings 6Al - 4V, Extra Low Interstitial Annealed - UNS R56401
DoD Adopted |
| 315 | SAE EIA-STD-656B-2006 | 2006-09-01 | English | I/O Buffer Information Specification (IBIS) Version 4.2 - Formerly TechAmerica EIA-STD-656-B |
| 316 | SAE J1472-2006 | 2006-09-01 | English | Braking Performance - Rollers |
| 317 | SAE AS81935/7-2006 | 2006-09-01 | English | BEARING, PLAIN ROD END, SELF-ALIGNING, SELFLUBRICATING, WIDE, INTERNALLY THREADED, STEEL, CORROSION RESISTANT (CRES) -65 TO +325 掳F |
| 318 | SAE AS87132-2006 | 2006-09-01 | English | Lubricant, Cetyl Alcohol, 1-Hexadecanol, Application to Fasteners |
| 319 | SAE J551-2-2006 | 2006-09-01 | English | Test Limits and Methods of Measurement of Radio Disturbance Characteristics of Vehicles, Motorboats, and Spark-Ignited Engine-Driven Devices |
| 320 | SAE AIR5696-2006 | 2006-09-01 | English | Aerospace Fluid Power - FAA Regulatory History - Transport Airplane Hydraulic Systems |
| 321 | SAE AMS4239D-2006 | 2006-09-01 | English | Aluminum Alloy Castings, Sand 6.8Mg - 0.18Ti - 0.18Mn (535.0-0) Annealed |
| 322 | SAE AMS3644G-2006 | 2006-09-01 | English | Plastic: Polyimide For Molded Rod, Bar, and Tube, Plaque, and Formed Parts |
| 323 | SAE AS5832-2006 | 2006-09-01 | English | ASSEMBLED COUPLING COMPONENTS, THREADLESS-FLEXIBLE, FIXED CAVITY, CURRENT CARRYING, SELF BONDING |
| 324 | SAE AMS2280B-2006 | 2006-09-01 | English | Trace Element Control Nickel Alloy Castings |
| 325 | SAE AMS5719D-2006 | 2006-09-01 | English | Steel Bars, Wire, Forgings, Tubing, Rings, and Extrusions, Corrosion Resistant 11.8 Cr - 2.5Ni - 1.8Mo - 0.33V (0.08 - 0.15C) Annealed, Vacuum Arc or Electroslag Remelted - UNS S64152
DoD Adopted |
| 326 | SAE AMS5399D-2006 | 2006-09-01 | English | Nickel Alloy, Corrosion and Heat Resistant, Investment Castings 52Ni - 19Cr - 11Co - 9.8Mo - 3.2Ti - 1.6Al - 0.006B Vacuum-Melted, Vacuum-Cast, Solution Heat Treated - UNS N07041
DoD Adopted |
| 327 | SAE AMS5441-2006 | 2006-09-01 | English | Nickel Alloy, Corrosion and Heat-Resistant, Bars, Forgings, and Rings Ni - 18Cr - 2.8Mo - 5.5Cb(Nb) - 0.70Ti - 1.50Al - 10Fe - 9Co - 1W Consumable Electrode Remelted or Vacuum Induction Melted 1775 degrees F (968 degrees C) Solution Heat Treated, Precipitation-Hardenable - UNS N07818 |
| 328 | SAE AMS2615F-2006 | 2006-09-01 | English | Pressure Testing, Hydraulic Pressure as Specified |
| 329 | SAE AMS5712J-2006 | 2006-09-01 | English | Nickel Alloy, Corrosion and Heat Resistant, Bars, Forgings, and Rings 53Ni - 19Cr - 11Co - 9.8Mo - 3.2Ti - 1.6Al - 0.006B Vacuum Melted, Solution Heat Treated Precipitation Hardenable - UNS N07041
DoD Adopted |
| 330 | SAE AMS5703D-2006 | 2006-09-01 | English | Nickel Alloy, Corrosion and Heat Resistant, Bars, Forgings, and Rings 41.5Ni - 16Cr - 37Fe - 2.9Cb - 1.8Ti Consumable Electrode or Vacuum Induction Melted 1750 Degrees F (954 Degrees C) Solution, Stabilization, and Precipitation Heat Treated - UNS N09706
DoD Adopted |
| 331 | SAE J1270-2006 | 2006-09-01 | English | Measurement of Passenger Car, Light Truck, and Highway Truck and Bus Tire Rolling Resistance |
| 332 | SAE AMS2615F-2006 | 2006-09-01 | English | Pressure Testing, Hydraulic Pressure as Specified |
| 333 | SAE AS85049/138-2006 | 2006-09-01 | English | CONNECTOR ACCESSORIES, ELECTRICAL, CAP, DUST, PLASTIC, CATEGORY 9 |
| 334 | SAE AS87132-2006 | 2006-09-01 | English | Lubricant, Cetyl Alcohol, 1-Hexadecanol, Application to Fasteners |
| 335 | SAE AMS5631E-2006 | 2006-09-01 | English | Steel, Corrosion Resistant, Bars and Forgings 17Cr (0.60 - 0.75C) - UNS S44002 |
| 336 | SAE AMS5620G-2006 | 2006-09-01 | English | Steel, Corrosion and Heat Resistant, Bars, Wire,and Forgings 13Cr (0.30 - 0.40C) (SAE 51420F, 51420Se) Free-Machining Grade - UNS S42020 (Type 2); S42023 (Type 1)
DoD Adopted |
| 337 | SAE AS115851 THRU AS115900A-2006 | 2006-09-01 | English | (R) SCREW - FLAT FILLISTER, DRILLED HEAD, CADMIUM PLATED, STEEL UNS G87400, 125 KSI MIN .2500-20 UNC - 3A
DoD Adopted |
| 338 | SAE AMS5611F-2006 | 2006-09-01 | English | Steel, Corrosion and Heat Resistant, Bars, Wire, Forgings, Tubing, and Rings 12Cr Ferrite Controlled, Consumable Electrode Melted - UNS S41001 |
| 339 | SAE AMS5571H-2006 | 2006-09-01 | English | Steel, Corrosion and Heat Resistant, Seamless Tubing 18Cr - 10.5Ni - 0.70Cb (SAE 30347) Solution Heat Treated - UNS S34700
DoD Adopted |
| 340 | SAE AS5838-2006 | 2006-09-01 | English | FEMALE FERRULE, THREADLESS-FLEXIBLE, FIXED CAVITY, CURRENT CARRYING, SELF BONDING, SWAGED |
| 341 | SAE AS5837-2006 | 2006-09-01 | English | MALE FERRULE, THREADLESS-FLEXIBLE, FIXED CAVITY, CURRENT CARRYING, SELF BONDING, BUTT WELDED |
| 342 | SAE AS5836-2006 | 2006-09-01 | English | FITTING END, THREADLESS-FLEXIBLE, FIXED CAVITY, CURRENT CARRYING, SELF BONDING MALE AND FEMALE DESIGN STANDARD |
| 343 | SAE AMS4349D-2006 | 2006-09-01 | English | Core, Honeycomb, Aluminum Alloy, Corrosion Inhibited for Sandwich Construction, 5056, 350 (177) |
| 344 | SAE AMS4348D-2006 | 2006-09-01 | English | Core, Honeycomb, Aluminum Alloy, Corrosion Inhibited for Sandwich Construction 5052, 350 (177) |
| 345 | SAE AS5839-2006 | 2006-09-01 | English | FEMALE FERRULE, THREADLESS-FLEXIBLE, FIXED CAVITY, CURRENT CARRYING, SELF BONDING, BUTT WELDED |
| 346 | SAE AMS4344C-2006 | 2006-09-01 | English | Aluminum Alloy, Extrusions 5.6Zn - 2.5Mg - 1.6Cu - 0.23Cr (7175-T73511) Solution Heat Treated, Stress Relieved by Stretching, Staightened,, and Overaged - UNS A97175 |
| 347 | SAE AMS7510B-2006 | 2006-09-01 | English | Magnets, Rare-Earth/ Cobalt, Permanent Powder-Metallurgy Product |
| 348 | SAE AMS4341E-2006 | 2006-09-01 | English | Aluminum Alloy, Extrusions 6.2Zn - 2.3Cu - 2.2Mg - 0.12Zr (7050-T73511) Solution Heat Treated, Stress Relieved by Stretching, Straightened, and Overaged - UNS A97050
DoD Adopted |
| 349 | SAE AS5835-2006 | 2006-09-01 | English | COUPLING BODY, THREADLESS-FLEXIBLE, FIXED CAVITY, CURRENT CARRYING, SELF BONDING |
| 350 | SAE ARP1315D-2006 | 2006-09-01 | English | (R) Safety Considerations for Airplane Lavatories |
| 351 | SAE AMS4340E-2006 | 2006-09-01 | English | Aluminum Alloy, Extrusions 6.2Zn - 2.3Cu - 2.2Mg - 0.12Zr (7050-T76511) Solution Heat Treated, Stress Relieved, Straightened, and Overaged - UNS A97050
DoD Adopted |
| 352 | SAE ARP5674-2006 | 2006-09-01 | English | Safety Considerations for Aircraft-Mounted Lasers Projected Into the Navigable Airspace |
| 353 | SAE J1269-2006 | 2006-09-01 | English | Rolling Resistance Measurement Procedure for Passenger Car, Light Truck, and Highway Truck and Bus Tires |
| 354 | SAE AS5834-2006 | 2006-09-01 | English | SLEEVE, THREADLESS-FLEXIBLE, FIXED CAVITY, CURRENT CARRYING, SELF BONDING |
| 355 | SAE AMS4337A-2006 | 2006-09-01 | English | Aluminum Alloy, Extruded Profiles (7055-T77511) 8.0Zn - 2.3Cu - 2.0Mg - 0.16Zr Solution Heat Treated, Stress Relieved, and Overaged - UNS A97055 |
| 356 | SAE AMS3644G-2006 | 2006-09-01 | English | Plastic: Polyimide For Molded Rod, Bar, and Tube, Plaque, and Formed Parts |
| 357 | SAE AMS7510/2B-2006 | 2006-09-01 | English | Magnets, Rare-Earth/ Cobalt, Permanent Samarium-Cobalt, 33/67 - 18 (143) 250 |
| 358 | SAE AS5833-2006 | 2006-09-01 | English | MALE FERRULE, THREADLESS-FLEXIBLE, FIXED CAVITY, CURRENT CARRYING, SELF BONDING, SWAGED |
| 359 | SAE AS5831-2006 | 2006-09-01 | English | ASSEMBLED COUPLING, THREADLESS-FLEXIBLE, FIXED CAVITY, CURRENT CARRYING, SELF BONDING, ENVELOPE DIMENSIONS |
| 360 | SAE AS1791D-2006 | 2006-09-01 | English | WIRE, RETAINER - TUBE COUPLING NUT
DoD Adopted |
| 361 | SAE AMS4253B-2006 | 2006-09-01 | English | Aluminum Alloy-Aramid Fiber Reinforced-Laminated Sheet 5.7Zn - 2.2Mg - 1.6Cu - 0.22Cr (7475-T61) 3, 5, 7, or 9 Ply |
| 362 | SAE AMS4248B-2006 | 2006-09-01 | English | Aluminum Alloy Hand Forgings and Rolled Rings 1.0Mg - 0.60Si - 0.28Cu - 0.20Cr (6061-T652) Solution Heat Treated, Stress Relief Compressed, and Precipitation Heat Treated - UNS A96061
DoD Adopted |
| 363 | SAE J2503-2006 | 2006-09-01 | English | Drawbar Pull Performance Criteria |
| 364 | SAE AS5830-2006 | 2006-09-01 | English | Coupling Assembly, Threadless, Flexible, Fixed Cavity, Current Carrying, Self-Bonding, Procurement Specification |
| 365 | SAE AMS4086N-2006 | 2006-09-01 | English | Aluminum Alloy, Drawn, Round, Seamless Hydraulic Tubing 4.4Cu - 1.5Mg - 0.60Mn (2024-T3) Solution Heat Treated, Cold Worked, and Naturally Aged - UNS A92024 |
| 366 | SAE AMS4138B-2006 | 2006-09-01 | English | Aluminum Alloy Forgings 4.3Zn - 3.3Mg - 0.60Cu - 0.20Mn - 0.18Cr (7079- T6) |
| 367 | SAE AMS4892C-2006 | 2006-09-01 | English | Alloy Castings, Corrosion and Heat Resistant 66Ni - 29Cu - 4.0Si as Cast - UNS N04019
DoD Adopted |
| 368 | SAE AMS4893C-2006 | 2006-09-01 | English | Alloy Castings, Corrosion and Heat Resistant 66Ni - 29Cu - 4.0Si Solution Treated - UNS N04019 |
| 369 | SAE AMS5732J-2006 | 2006-09-01 | English | Steel, Corrosion and Heat-Resistant, Bars, Wire, Forgings, Tubing, and Rings 15Cr - 25.5Ni - 1.2Mo - 2.1Ti - 0.006B - 0.30V Consumable Electrode Melted 1800 °F (982 °C) Solution and Precipitation Heat Treated - UNS S66286 |
| 370 | SAE AMS5872E-2006 | 2006-09-01 | English | Nickel Alloy, Corrosion and Heat Resistant, Sheet, Strip, and Plate 48Ni - 20Cr - 20Co - 5.9Mo - 2.2Ti - 0.45Al Consumable Electrode or Vacuum Induction Melted Solution Heat Treated - UNS N07263 |
| 371 | SAE AMS5110J-2006 | 2006-09-01 | English | Carbon Steel, Wire and Springs 0.75 - 0.88C (SAE 1080) Spring Temper, Cold Drawn - UNS G10800
DoD Adopted |
| 372 | SAE AMS4016L-2006 | 2006-09-01 | English | Aluminum Alloy, Sheet and Plate 2.5Mg - 0.25Cr (5052-H32) Strain Hardened, Quarter-Hard, and Stabilized - UNS A95052 |
| 373 | SAE AMS5862H-2006 | 2006-09-01 | English | Steel, Corrosion-Resistant, Sheet, Strip, and Plate 15Cr - 4.5Ni - 0.30Cb (Nb) - 3.5Cu Consumable Electrode Remelted, Solution Heat Treated Precipitation-Hardenable - UNS S15500
DoD Adopted |
| 374 | SAE AS85049/5A-2006 | 2006-09-01 | English | (R) Connector Accessories, Electrical, Backshell, Cable Sealing, Straight, Step-Down, Category 1A (for MIL-C-22992 Connectors, Classes C, J, and R) - FSC 5935
DoD Adopted |
| 375 | SAE AMS5650F-2006 | 2006-09-01 | English | Steel, Corrosion and Heat Resistant, Bars, Wire, Forgings, Tubing, and Rings 23Cr - 13.5Ni (SAE 30309S) Solution Heat Treated - UNS S30908
DoD Adopted |
| 376 | SAE AMS4177D-2006 | 2006-09-01 | English | Core, Flexible Honeycomb, Aluminum Alloy For Sandwich Construction 5056, 350 (177) |
| 377 | SAE AMS4674G-2006 | 2006-09-01 | English | Nickel - Copper Alloy, Corrosion Resistant Bars and Forgings 67Ni - 30Cu - 0.04S Free Machining - UNS N04405 |
| 378 | SAE AMS5837G-2006 | 2006-09-01 | English | Nickel Alloy, Corrosion and Heat Resistant, Welding Wire 62Ni - 21.5Cr - 9.0Mo - 3.7Cb(Nb) - UNS N06625
DoD Adopted |
| 379 | SAE AMS6437G-2006 | 2006-09-01 | English | Steel, Sheet, Strip, and Plate 5.0Cr - 1.3Mo - 0.50V (0.38 - 0.43C) (H-11) - UNS T20811
DoD Adopted |
| 380 | SAE AMS5554E-2006 | 2006-09-01 | English | Steel, Corrosion and Heat Resistant, Seamless Tubing 16.5Cr - 4.5Ni - 2.9Mo - 0.10N Annealed - UNS S35000
DoD Adopted |
| 381 | SAE AMS-QQ-A-250/6A-2006 | 2006-09-01 | English | Aluminum Alloy 5083, Plate and Sheet - UNS A95083
DoD Adopted |
| 382 | SAE J1269-2006 | 2006-09-01 | English | Rolling Resistance Measurement Procedure for Passenger Car, Light Truck, and Highway Truck and Bus Tires |
| 383 | SAE AMS5872E-2006 | 2006-09-01 | English | Nickel Alloy, Corrosion and Heat-Resistant, Sheet, Strip, and Plate 48Ni - 20Cr - 20Co - 5.9Mo - 2.2Ti - 0.45Al Consumable Electrode or Vacuum Induction Melted Solution Heat Treated - UNS N07263 |
| 384 | SAE AMS5547H-2006 | 2006-09-01 | English | Steel, Corrosion and Heat Resistant, Sheet and Strip 15.5 Cr - 4.5Ni - 2.9Mo - 0.10N Solution Heat Treated - UNS S35500
DoD Adopted |
| 385 | SAE AMS5536M-2006 | 2006-09-01 | English | Nickel Alloy, Corrosion and Heat Resistant, Sheet, Strip, and Plate 47.5Ni - 22Cr - 1.5Co - 9.0Mo - 0.60W - 18.5Fe Solution Heat Treated - UNS N06002
DoD Adopted |
| 386 | SAE AMS5532G-2006 | 2006-09-01 | English | Iron Alloy, Corrosion and Heat Resistant, Sheet, Strip, and Plate 30Fe - 21Cr - 20Ni - 20Co - 3.0Mo - 2.5W - 1.0Cb - 0.15N Solution Heat Treated - UNS R30155
DoD Adopted |
| 387 | SAE AMS2251H-2006 | 2006-09-01 | English | Tolerances Low-Alloy Steel Bars
DoD Adopted |
| 388 | SAE AMS4086N-2006 | 2006-09-01 | English | Aluminum Alloy, Drawn, Round, Seamless Hydraulic Tubing 4.4Cu - 1.5Mg - 0.60Mn (2024-T3) Solution Heat Treated, Cold Worked, and Naturally Aged |
| 389 | SAE AMS4087H-2006 | 2006-09-01 | English | Aluminum Alloy Tubing, Seamless, Drawn (2024-0) Reinstate Composition Annealed |
| 390 | SAE AS21220B-2006 | 2006-09-01 | English | BEARING, ROLLER, ROD END, INTERNAL THREAD, SELF-ALIGNING, ANTI-FRICTION, AIRFRAME, HEAVY DUTY, TYPE II, -67 TO 350 掳F, SEALED
DoD Adopted |
| 391 | SAE J1270-2006 | 2006-09-01 | English | Measurement of Passenger Car, Light Truck, and Highway Truck and Bus Tire Rolling Resistance |
| 392 | SAE AS81935/9-2006 | 2006-09-01 | English | BEARING, PLAIN, ROD END, SELF-ALIGNING, SELFLUBRICATING, NARROW, INTERNALLY THREADED, CORROSION RESISTANT (CRES) -65 TO +325 掳F |
| 393 | SAE AMS2447C-2006 | 2006-09-01 | English | Coating, Thermal Spray High Velocity Oxygen/Fuel Process |
| 394 | SAE AMS7254A-2006 | 2006-09-01 | English | Perfluoroether Elastomer |
| 395 | SAE AS81935/2A-2006 | 2006-09-01 | English | (R) BEARING, PLAIN ROD END, SELF-ALIGNING, SELF-LUBRICATING, WIDE, INTERNALLY THREADED, -65 TO +325 掳F
DoD Adopted |
| 396 | SAE J1939-11-2006 | 2006-09-01 | English | Physical Layer, 250K bits/s, Twisted Shielded Pair |
| 397 | SAE AMS4402-2006 | 2006-09-01 | English | Aluminum Alloy, Extruded Profiles (2024-T432) 4.4Cu - 1.5Mg - 0.6Mn Annealed, Stretch Formed, Solution Heat Treated and Stress Relieved by Stretching - UNS A92027 |
| 398 | SAE AMS-QQ-A-250/9A-2006 | 2006-09-01 | English | Aluminum Alloy 5456, Plate and Sheet - UNS A95456
DoD Adopted |
| 399 | SAE AMS5732J-2006 | 2006-09-01 | English | Steel, Corrosion and Heat Resistant, Bars, Wire, Forgings, Tubing, and Rings 15Cr - 25.5Ni - 1.2Mo - 2.1Ti - 0.006B - 0.30V Consumable Electrode Melted 1800 Degrees F (982 Degrees C) Solution and Precipitation Heat Treated - UNS S66286
DoD Adopted |
| 400 | SAE J1121-2006 | 2006-09-01 | English | Helical Compression and Extension Spring Terminology |
| 401 | SAE AMS3846D-2006 | 2006-09-01 | English | Cloth, Quartz Finished for Resin Laminates
DoD Adopted |
| 402 | SAE AMS6444K-2006 | 2006-09-01 | English | Steel, Bars, Forgings, and Tubing 1.45Cr (0.93 - 1.05C) (SAE 52100) Premium Aircraft-Quality, Consumable Electrode Vacuum Remelted - UNS G52986
DoD Adopted |
| 403 | SAE AMS5382J-2006 | 2006-09-01 | English | Cobalt Alloy, Corrosion and Heat Resistant, Investment Castings 54Co - 25.5Cr - 10.5Ni - 7.5W as Cast - UNS R30031
DoD Adopted |
| 404 | SAE ARP4835-2006 | 2006-09-01 | English | Aerospace Fluid Power-Hydraulic Thermal Expansion Relief Valves |
| 405 | SAE/TP 2006-01-2385-2006 | 2006-08-29 | English | Analyzing a NACA 23012 Airfoil Composed of a Double-Slotted Fowler Flap and a Leading-Edge Handley-Page Slat with the Use of Computational Fluid Dynamics |
| 406 | SAE/TP 2006-01-2387-2006 | 2006-08-29 | English | The Channel Wing Revisited |
| 407 | SAE/TP 2006-01-2386-2006 | 2006-08-29 | English | Experimental and CFD Analysis of Aerial Refueling System |
| 408 | SAE/TP 2006-01-2447-2006 | 2006-08-29 | English | Studying Flammability in a Commercial Transport Fuel Tank with Inerting |
| 409 | SAE/TP 2006-01-2446-2006 | 2006-08-29 | English | Limiting Oxygen Concentration of Aviation Fuels |
| 410 | SAE/TP 2006-01-2445-2006 | 2006-08-29 | English | Vaporization of JP-8 Jet Fuel in a Simulated Aircraft Fuel Tank Under Varying Ambient Conditions |
| 411 | SAE/TP 2006-01-2444-2006 | 2006-08-29 | English | An Approximate Graph Matching Technique for Integrity Monitoring in Integrated Intelligent Flight Deck Applications |
| 412 | SAE/TP 2006-01-2442-2006 | 2006-08-29 | English | Intrinsically Safe Current Limit Study for Aircraft Fuel Tank Electronics |
| 413 | SAE/TP 2006-01-2438-2006 | 2006-08-29 | English | As9100 Registration Difficulties and Organizational Benefits: A Supplier Satisfaction Survey |
| 414 | SAE/TP 2006-01-2436-2006 | 2006-08-29 | English | Quiet, Clean, and Efficient, but Heavy – Concerns for Future Fuel Cell Powered Personal Air Vehicles |
| 415 | SAE/TP 2006-01-2435-2006 | 2006-08-29 | English | A Comparative Study of a Multi-Gas Generator Fan to aTurbofan Engine on a Vertical Takeoff and Landing Personal Air Vehicle |
| 416 | SAE/TP 2006-01-2434-2006 | 2006-08-29 | English | A System Dynamics Approach for Dynamic Uncertainty Assessment in a PAV Design Environment |
| 417 | SAE/TP 2006-01-2431-2006 | 2006-08-29 | English | The Successful Person Air Vehicle: Business Case Risk Reduction |
| 418 | SAE/TP 2006-01-2429-2006 | 2006-08-29 | English | The Third Wave of Aeronautics: On-Demand Mobility |
| 419 | SAE/TP 2006-01-2425-2006 | 2006-08-29 | English | Simulation and Visualization Environment for Nonlinear Helicopter Flight Dynamics |
| 420 | SAE/TP 2006-01-2423-2006 | 2006-08-29 | English | Flow Characteristics of Straight and Slanted Entry Nozzle Run by a Supersonic Stream |
| 421 | SAE/TP 2006-01-2422-2006 | 2006-08-29 | English | Flight Without Fuel – Regenerative Soaring Feasibility Study |
| 422 | SAE/TP 2006-01-2421-2006 | 2006-08-29 | English | An Improved Method of Accelerated Crankshaft Fatigue Testing for Reciprocating Aircraft Engines |
| 423 | SAE/TP 2006-01-2420-2006 | 2006-08-29 | English | Optimization of a Light Aircraft Spark-Ignition Engine |
| 424 | SAE/TP 2006-01-2419-2006 | 2006-08-29 | English | Arc Fault Protection, Application Techniques for Aircraft Circuit Breakers |
| 425 | SAE/TP 2006-01-2418-2006 | 2006-08-29 | English | Aeronautical Applications of High Power Solid State Lighting |
| 426 | SAE/TP 2006-01-2416-2006 | 2006-08-29 | English | Non-Linear Adaptive Attitude Control of Rigid Body in Space |
| 427 | SAE/TP 2006-01-2415-2006 | 2006-08-29 | English | Fault Detection and Isolation in Attitude and Heading Reference Systems For Fly-By-Wire Control System For General Aviation Aircraft |
| 428 | SAE/TP 2006-01-2414-2006 | 2006-08-29 | English | Laboratory and Preliminary In-Flight Tests of Electromechanical Actuators |
| 429 | SAE/TP 2006-01-2413-2006 | 2006-08-29 | English | NASA Personal Air Transportation Technologies |
| 430 | SAE/TP 2006-01-2412-2006 | 2006-08-29 | English | Test Approach for the Mechanical Qualification of a Micro-Satellite Structure and Subsystems |
| 431 | SAE/TP 2006-01-2411-2006 | 2006-08-29 | English | Stress Concentrations and Structural Analysis |
| 432 | SAE/TP 2006-01-2410-2006 | 2006-08-29 | English | Wiring Assessment of Aging Commuter Class Aircraft |
| 433 | SAE/TP 2006-01-2409-2006 | 2006-08-29 | English | Destructive Evaluation of Aging General Aviation Airplanes |
| 434 | SAE/TP 2006-01-2406-2006 | 2006-08-29 | English | Unsteady Stalling Characteristics of Flapping Wing Micro Aerial Vehicle |
| 435 | SAE/TP 2006-01-2403-2006 | 2006-08-29 | English | A Knowledge-Based Design Framework for Aircraft Conceptual and Preliminary Design |
| 436 | SAE/TP 2006-01-2402-2006 | 2006-08-29 | English | AMRaven – An Integrated Air Vehicle Design and Analysis Environment |
| 437 | SAE/TP 2006-01-2397-2006 | 2006-08-29 | English | Comparison Plusher and Tractor Propulsion for Micro Air Vehicle Applications |
| 438 | SAE/TP 2006-01-2396-2006 | 2006-08-29 | English | Continued Computational Investigation into Circulation Control for the V-22 Osprey Download Reduction; Blowing Slot Optimization |
| 439 | SAE/TP 2006-01-2394-2006 | 2006-08-29 | English | Preliminary Design of a Tandem Seater Light Sport Airplane |
| 440 | SAE/TP 2006-01-2388-2006 | 2006-08-29 | English | Prediction of Variation in Dimensional Tolerance Due to Sheet Metal Hydroforming using Finite Element Analysis |
| 441 | SAE/TP 2006-01-2389-2006 | 2006-08-29 | English | Managing Value Stream Risk |
| 442 | SAE/TP 2006-01-2393-2006 | 2006-08-29 | English | The Design of an Uninhabited Air Vehicle for Use in Polar Research |
| 443 | SAE/TP 2006-01-2430-2006 | 2006-08-29 | English | Next Generation NASA GA Advanced Concept |
| 444 | SAE/TP 2006-01-2443-2006 | 2006-08-29 | English | Characterization of the Effect of Material Configuration and Impact Parameters on Damage Tolerance of Sandwich Composites |
| 445 | SAE AS5530-2006 | 2006-08-20(R 2013) | English | UNION, FLARELESS TUBE FITTING, INTERNALLY SWAGED |
| 446 | SAE AS5530-2006 | 2006-08-20 | English | UNION, FLARELESS TUBE FITTING, INTERNALLY SWAGED |
| 447 | SAE AMS5793B-2006 | 2006-08-01(R 2018) | English | Powder, Plasma Spray 95Ni - 5Al |
| 448 | SAE AMS5792B-2006 | 2006-08-01(R 2018) | English | Powder, Plasma Spray 50 (88WC - 12Co) + 35 (70Ni - 16.5Cr - 4Fe - 4Si - 3.8B) + 15 (80Ni - 20A1) Three-Component Mixture |
| 449 | SAE AS5529-2006 | 2006-08-01(R 2013) | English | FITTING ASSEMBLY, CROSS, AXIALLY SWAGED, HYDRAULIC, 5080 PSI |
| 450 | SAE AS1714D-2006 | 2006-08-01(R 2013) | English | NUT ASSEMBLY, COUPLING, FLEXIBLE, VARIABLE CAVITY, THREADED, FERRULE TYPE TUBE ENDS |
| 451 | SAE AS1716D-2006 | 2006-08-01(R 2013) | English | FERRULE, COUPLING, FLEXIBLE, VARIABLE CAVITY, THREADED, FERRULE TUBE END |
| 452 | SAE AS1717D-2006 | 2006-08-01(R 2013) | English | RETAINER, COUPLING, FLEXIBLE, VARIABLE CAVITY, THREADED FERRULE TYPE TUBE ENDS |
| 453 | SAE AS1718D-2006 | 2006-08-01(R 2013) | English | COUPLING BODY, FLEXIBLE, VARIABLE CAVITY, THREADED FERRULE TYPE TUBE ENDS |
| 454 | SAE AS5952B-2006 | 2006-08-01(R 2013) | English | HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, PARA ARAMID REINFORCED, 275 °F, 5080 PSI, FLARELESS, TITANIUM FITTINGS, STRAIGHT TO STRAIGHT |
| 455 | SAE AS5955B-2006 | 2006-08-01(R 2013) | English | HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, PARA ARAMID REINFORCED, 275 °F, 5080 PSI, FLARELESS, TITANIUM FITTINGS, 45° TO 45° |
| 456 | SAE AS5957B-2006 | 2006-08-01(R 2013) | English | HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, PARA ARAMID REINFORCED, 275 °F, 5080 PSI, FLARELESS, TITANIUM FITTINGS, 90° TO 90° |
| 457 | SAE AS5791-2006 | 2006-08-01(R 2013) | English | FITTING ASSEMBLY, ADAPTER, BULKHEAD FLARELESS, AXIALLY SWAGED, HYDRAULIC |
| 458 | SAE AS1712C-2006 | 2006-08-01(R 2013) | English | COUPLING SUBASSEMBLY, FLEXIBLE, VARIABLE CAVITY, THREADED, FERRULE TYPE TUBE ENDS |
| 459 | SAE AS1713C-2006 | 2006-08-01(R 2013) | English | HALF COUPLING SUBASSEMBLY, FLEXIBLE, VARIABLE CAVITY, THREADED FERRULE TYPE TUBE ENDS |
| 460 | SAE AS5531-2006 | 2006-08-01(R 2013) | English | UNION, SHORT FLARELESS TUBE FITTING, INTERNALLY SWAGED |
| 461 | SAE J2730-2006 | 2006-08-01(R 2013) | English | Dynamic Cleat Test with Perpendicular and Inclined Cleats |
| 462 | SAE AS123451 THRU AS123600B-2006 | 2006-08-01(R 2012) | English | RIVET, SOLID, 100° FLUSH HEAD, HIGH TEMPERATURE, 347 CRES, UNS S34700 |
| 463 | SAE AS9318A-2006 | 2006-08-01(R 2012) | English | RIVET, SOLID - 100° FLUSH HEAD, MONEL UNS N04400 |
| 464 | SAE AS123151 THRU AS123300A-2006 | 2006-08-01(R 2012) | English | RIVET, UNIVERSAL HEAD, HIGH TEMPERATURE, 347 CRES UNS S34700 |
| 465 | SAE AS9319A-2006 | 2006-08-01(R 2012) | English | RIVET, SOLID - UNIVERSAL HEAD, MONEL UNS N04400 |
| 466 | SAE AMS5925A-2006 | 2006-08-01(R 2012) | English | Steel, Corrosion-Resistant, Bars, Wire, and Forgings 15.5Cr - 1.8Mo - 0.20N (0.37 - 0.45C) Electroslag Remelted - UNS S42025 |
| 467 | SAE AMS5792B-2006 | 2006-08-01(R 2012) | English | Powder, Plasma Spray 50 (88WC - 12Co) + 35 (70Ni - 16.5Cr - 4Fe - 4Si - 3.8B) + 15 (80Ni - 20A1) Three-Component Mixture |
| 468 | SAE AMS5793B-2006 | 2006-08-01(R 2012) | English | Powder, Plasma Spray 95Ni - 5Al
DoD Adopted |
| 469 | SAE AMS5022N-2006 | 2006-08-01(R 2011) | English | Steel, Bars, Forgings, and Tubing, Free-Cutting 0.14 - 0.20C (SAE 1117) - UNS G11170
DoD Adopted |
| 470 | SAE ARP1048B-2006 | 2006-08-01(R 2011) | English | (R) Instrument and Cockpit Illumination for General Aviation Aircraft |
| 471 | SAE J2305-2006 | 2006-08-01(R 2011) | English | Hazard Reduction for Horizontal Earthboring Machines |
| 472 | SAE ARP378C-2006 | 2006-08-01(R 2011) | English | Passenger Reading Lights |
| 473 | SAE AMS5024H-2006 | 2006-08-01(R 2011) | English | Steel, Bars, Forgings, and Tubing, Free-Cutting 1.5Mn (0.32 - 0.39C) (SAE 1137) - UNS G11370
DoD Adopted |
| 474 | SAE AMS4403-2006 | 2006-08-01(R 2011) | English | Aluminum Alloy, Die Forgings 7.5Zn - 1.6Cu - 1.5Mg - 0.12Zr (7085-T7452) Solution Heat Treated, Compression Stress-Relieved, and Overaged - UNS A97085 |
| 475 | SAE ARP4252A-2006 | 2006-08-01(R 2011) | English | Instrumental Methods of Determining Surface Cleanliness |
| 476 | SAE AMS2800D-2006 | 2006-08-01(R 2011) | English | Identification Finished Parts
DoD Adopted |
| 477 | SAE AMS3415D-2006 | 2006-08-01(R 2011) | English | Flux, Aluminum Dip Brazing 1030 °F (554 °C) or Lower Liquidus
DoD Adopted |
| 478 | SAE AS123151 THRU AS123300A-2006 | 2006-08-01(R 2005) | English | (R) RIVET, UNIVERSAL HEAD, HIGH TEMPERATURE, 347 CRES UNS S34700
DoD Adopted |
| 479 | SAE AS9318A-2006 | 2006-08-01(R 2004) | English | (R) RIVET, SOLID - 100 DEGREE FLUSH HEAD, MONEL UNS N04400 - FSC 5320
DoD Adopted |
| 480 | SAE AS8023A-2006 | 2006-08-01(R 1993) | English | (R) Minimum Performance Standards for Static Electric Power Inverters |
| 481 | SAE AS9319A-2006 | 2006-08-01 | English | (R) RIVET, SOLID - UNIVERSAL HEAD, MONEL UNS N04400
DoD Adopted |
| 482 | SAE ARP4721 PART 1-2006 | 2006-08-01 | English | Monitoring Aircraft Noise and Operations in the Vicinity of Airports: System Description, Acquisition, and Operation |
| 483 | SAE AS5952B-2006 | 2006-08-01 | English | HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, PARA ARAMID REINFORCED, 275 掳F, 5080 PSI, FLARELESS, TITANIUM FITTINGS, STRAIGHT TO STRAIGHT |
| 484 | SAE AS5955B-2006 | 2006-08-01 | English | HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, PARA ARAMID REINFORCED, 275 掳F, 5080 PSI, FLARELESS, TITANIUM FITTINGS, 45掳 TO 45掳 |
| 485 | SAE AS5957B-2006 | 2006-08-01 | English | HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, PARA ARAMID REINFORCED, 275 掳F, 5080 PSI, FLARELESS, TITANIUM FITTINGS, 90掳 TO 90掳 |
| 486 | SAE ARP378C-2006 | 2006-08-01 | English | Passenger Reading Lights |
| 487 | SAE AS5550A-2006 | 2006-08-01 | English | FITTING ASSEMBLY, RING LOCKED, ADAPTER, FLARELESS TO PORT, EXTRA FINE THREADS, 5080 PSI |
| 488 | SAE J1113-12-2006 | 2006-08-01 | English | Electrical Interference by Conduction and CouplingCapacitive and Inductive Coupling via Lines Other than Supply Lines |
| 489 | SAE AS123451 THRU AS123600B-2006 | 2006-08-01 | English | (R) RIVET, SOLID, 100 DEGREES FLUSH HEAD, HIGH TEMPERATURE, 347 CRES, UNS S34700
DoD Adopted |
| 490 | SAE AS5529-2006 | 2006-08-01 | English | SLEEVE, FLARELESS TUBE FITTING, INTERNALLY SWAGED |
| 491 | SAE AMS5792B-2006 | 2006-08-01 | English | Powder, Plasma Spray 50 (88WC - 12Co) + 35 (70Ni - 16.5Cr - 4Fe - 4Si - 3.8B) + 15 (80Ni - 20A1) Three-Component Mixture |
| 492 | SAE AIR5690-2006 | 2006-08-01 | English | Considerations for the Carriage and Use of Visual Distress Signals in Airline Overwater Survival Kits |
| 493 | SAE AS150501 THRU AS150800A-2006 | 2006-08-01 | English | (R) STUD, STEPPED, 1.5 DIA ENGAGEMENT, CADMIUM PLATED, STEEL UNS G87400, .2500-20 UNS X .1900-32 UNF-3A
DoD Adopted |
| 494 | SAE ARP1048B-2006 | 2006-08-01 | English | (R) Instrument and Cockpit Illumination for General Aviation Aircraft |
| 495 | SAE AMS5793B-2006 | 2006-08-01 | English | Powder, Plasma Spray 95Ni - 5Al
DoD Adopted |
| 496 | SAE ARP4721 PART 2-2006 | 2006-08-01 | English | Monitoring Aircraft Noise and Operations in the Vicinity of Airports: System Validation |
| 497 | SAE AMS4825D-2006 | 2006-08-01 | English | Bearings, Leaded Bronze 74Cu - 15.5Pb - 10Sn Steel Back |
| 498 | SAE AS5531-2006 | 2006-08-01 | English | UNION, SHORT FLARELESS TUBE FITTING, INTERNALLY SWAGED |
| 499 | SAE AS4914B-2006 | 2006-08-01 | English | (R) Aircraft Fluorescent Lighting Ballast/Fixture Safety Standard |
| 500 | SAE AMS6395F-2006 | 2006-08-01 | English | Steel Sheet, Strip, and Plate 0.95Cr - 0.20Mo (0.38 - 0.43C) (SAE 4140) - UNS G41400
DoD Adopted |
|