|
ISO 13597 |
Aerospace - Inserts, Self-Locking, with MJ Threads, Open Type, in Metallic Material, Coated or Uncoated - Dimensions-First Edition |
|
ISO 13599 |
Aerospace - Inserts, with Clearance Hole, in Metallic Material, Coated or Uncoated - Dimensions-First Edition |
|
ISO 13764 |
Space Data and Information Transfer Systems - Standard Formatted Data Units - Control Authority Procedures-First Edition |
|
ISO 13921 |
Aerospace - Screws, 100 Degrees Reduced Countersunk Head, Internal Offset Cruciform Ribbed or Unribbed Drive, Normal Shank, Short or Medium Length MJ Threads, Metallic Material, Coated or Uncoated, Strength Classes Less Than or Equal to 1 100 MPa - Dimensions First Edition |
|
ISO 14191 |
Aerospace - Airframe Spherical Roller Bearings, Single-Row, Self-Aligning, Diameter Series 3 and 4 - Metric Series-First Edition |
|
ISO 14192 |
Aerospace - Airframe Spherical Roller Bearings, Single-Row, Self-Aligning, Shielded, Intermediate Duty - Metric Series-First Edition |
|
ISO 14193 |
Aerospace - Airframe Spherical Roller Bearings, Single-Row, Self-Aligning, Sealed, Extended Inner Ring, Intermediate Duty - Inch Series-First Edition |
|
ISO 14197 |
Aerospace - Airframe Spherical Roller Bearings, Single-Row, Self-Aligning, Sealed, Intermediate Duty - Inch Series-First Edition |
|
ISO 14201 |
Aerospace - Airframe Ball Bearings, Double-Row, Self-Aligning, Diameter Series 2 - Metric Series-First Edition |
|
ISO 14202 |
Aerospace - Airframe Ball Bearings, Single-Row, Rigid, Diameter Series 0 and 2 - Metric Series-First Edition |
|
ISO 14203 |
Aerospace - Airframe Ball Bearings, Single-Row, Rigid, Diameter Series 8 and 9 - Metric Series-First Edition |
|
ISO 14204 |
Aerospace - Airframe Ball Bearings, Double-Row, Rigid, Diameter Series 0 - Metric Series-First Edition |
|
ISO 14209 |
Aerospace - Airframe Ball Bearings, Single-Row, Rigid, Precision, Sealed, Intermediate Duty - Inch Series-First Edition |
|
ISO 14211 |
Aerospace - Airframe Ball Bearings, Single-Row, Rigid, Precision, Sealed Torque Tube Design, Light Duty - Inch Series-First Edition |
|
ISO 14212 |
Aerospace - Airframe Ball Bearings, Single-Row, Rigid, Sealed, Torque Tube Design, Extra-Light Duty - Inch Series-First Edition |
|
ISO 14213 |
Aerospace - Airframe Ball Bearings, Single-Row, Rigid, Precision, Sealed, Torque Tube Design, Extra-Light Duty - Inch Series-First Edition |
|
ISO 14215 |
Aerospace - Airframe Ball Bearings, Double-Row, Rigid, Precision, Sealed, Heavy Duty - Inch Series-First Edition |
|
ISO 14216 |
Aerospace - Airframe Ball Bearings, Double-Row, Self-Aligning, Sealed, Heavy Duty - Inch Series-First Edition |
|
ISO 14217 |
Aerospace - Airframe Ball Bearings, Double-Row, Self-Aligning, Precision, Sealed, Heavy Duty - Inch Series-First Edition |
|
ISO 14218 |
Aerospace - Airframe Ball Bearings, Single-Row, Self-Aligning, Sealed, Heavy Duty - Inch Series-First Edition |
|
ISO 14219 |
Aerospace - Airframe Ball Bearings, Single-Row, Self-Aligning, Precision, Sealed, Heavy Duty - Inch Series-First Edition |
|
ISO 14276 |
Aerospace - Drives, Internal, Offset Cruciform - Metric Series-First Edition |
|
ISO 14277 |
Aerospace Drivers, Ribbed, for Internal Offset Cruciform Ribbed or Unribbed Drives Metric Series-First Edition |
|
ISO 14278 |
Aerospace Gauges, for Internal Offset Cruciform Ribbed or Unribbed Drives Metric Series-First Edition |
|
ISO 14279 |
Aerospace Drives, Internal, Cruciform Metric Series-First Edition |
|
ISO 14280 |
Aerospace Drivers, Ribbed, for Internal Cruciform Ribbed or Unribbed Drives Metric Series-First Edition |
|
ISO 14281 |
Aerospace Gauges, for Internal Cruciform Ribbed or Unribbed Drives Metric Series-Frist Edition |
|
ISO 14302 |
Space systems - Electromagnetic compatibility requirements-First Edition |
|
ISO 14619 |
Space systems Space experiments General requirements-First Edition |
|
ISO 14624-7 |
Space systems Safety and compatibility of materials Part 7: Determination of permeability and penetration of materials to aerospace fluids-First Edition |
|
ISO 1465 |
Aircraft - Liquid Oxygen Replenishment Couplings - Mating Dimensions-Second Edition |
|
ISO 1467 |
General Purpose Push-Pull Single-Pole Circuit-Breakers for Aircraft - Performance Requirements-First Edition |
|
ISO 14711 |
Space Systems - Unmanned Mission Operations Concepts - Guidelines for Defining and Assessing Concept Products-First Edition |
|
ISO 14951-11 |
Space Systems - Fluid Characteristics - Part 11: Ammonia-First Edition |
|
ISO 14951-12 |
Space Systems - Fluid Characteristics - Part 12: Carbon Dioxide-First Edition |
|
ISO 14951-2 |
Space Systems - Fluid Characteristics - Part 2: Hydrogen Propellant-First Edition |
|
ISO 14951-4 |
Space Systems - Fluid Characteristics - Part 4: Helium-First Edition; Corrigendum 1: 06/01/2000 |
|
ISO 14951-9 |
Space Systems - Fluid Characteristics - Part 9: Argon-First Edition; Corrigendum 1: 4/15/2000 |
|
ISO 15387 |
Space systems Single-junction solar cells Measurement and calibration procedures-First edition |
|
ISO 15395 |
Space Data and Information Transfer Systems - Standard Formatted Data Units - Control Authority Data Structures-First Edition |
|
ISO 1548 |
Aircraft - Precision Fuse-Links - Type A-First Edition |
|
ISO 15859-1 |
Space systems Fluid characteristics, sampling and test methods Part 1: Oxygen-First Edition |
|
ISO 15859-10 |
Space systems Fluid characteristics, sampling and test methods Part 10: Water-First Edition |
|
ISO 15859-11 |
Space systems Fluid characteristics, sampling and test methods Part 11: Ammonia-First Edition |
|
ISO 15859-12 |
Space systems Fluid characteristics, sampling test methods Part 12: Carbon dioxide-First Edition |
|
ISO 15859-13 |
Space systems Fluid characteristics, sampling and test methods Part 13: Breathing air-First Edition |
|
ISO 15859-4 |
Space systems Fluid characteristics, sampling and test methods Part 4: Helium-First Edition |
|
ISO 15859-8 |
Space systems Fluid characteristics, sampling and test methods Part 8: Kerosine propellant-First Edition |
|
ISO 15887 |
Space Data and Information Transfer Systems - Data Systems - Lossless Data Compression-First Edition |
|
ISO 15888 |
Space Data and Information Transfer Systems - Standard Formatted Data Units - Referencing Environment-First Edition |
|
ISO 15889 |
Space data and information transfer systems - Data description language - EAST specification-Second Edition |
|
ISO 15891 |
Space Data and Information Transfer Systems - Protocol Specification for Space Communications - Network Protocol-First Edition |
|
ISO 15892 |
Space Data and Information Transfer Systems - Protocol Specification for Space Communications - Security Protocol-First Edition |
|
ISO 16091 |
Space Systems - Integrated Logistic Support-First Edition |
|
ISO 16412 |
Air cargo equipment Air cargo pallets Utilization guidelines-First edition |
|
ISO 16458 |
Space systems Unmanned spacecraft transportation General requirements-First Edition |
|
ISO 17057 |
Aerospace - Rivets, Solid - Test Method-First Edition |
|
ISO 17775 |
Aircraft Ground-service connections Potable water, toilet-flush water and toilet drain-First Edition |
|
ISO 1965 |
Aluminium Terminal Ends for Crimping to Aircraft Aluminium Electrical Cables-First Edition |
|
ISO 1971 |
Aircraft - Accessory Drives and Mounting Pads-First Edition |
|
ISO 2026 |
Aircraft - Connections for Starting Engines by Air-First Edition |
|
ISO 2032 |
Heat-Resisting Equipment Wires for Aircraft-First Edition |
|
ISO 20652 |
Space data and information transfer systems Producer–archive interface Methodology abstract standard-First Edition |
|
ISO 20683-1 |
Aircraft ground equipment Design, test and maintenance for towbarless towing vehicles (TLTV) interfaced with nose-landing gear Part 1: Main-line aircraft-First Edition |
|
ISO 20683-2 |
Aircraft ground equipment Design, test and maintenance for towbarless towing vehicles (TLTV) interfaced with noselanding gear Part 2: Regional aircraft-First Edition |
|
ISO 21348 |
Space environment (natural and artificial) Process for determining solar irradiances-First Edition |
|
ISO 21349 |
Space systems Project reviews-First Edition |
|
ISO 21459 |
Space data and information transfer systems Proximity-1 space link protocol Coding and synchronization sublayer-First Edition |
|
ISO 21460 |
Space data and information transfer systems Proximity-1 space link protocol Physical layer-Second Edition |
|
ISO 21961 |
Space Data and Information Transfer Systems - Data Entity Dictionary Specification Language (DEDSL) - Abstract Sytax-First Edition |
|
ISO 21962 |
Space Data and Information Transfer Systems - Data Entity Dictionary Specification Language (DEDSL) - PVL Syntax-First Edition |
|
ISO 22072 |
Aerospace Electrohydrostatic actuator (EHA) Characteristics to be defined in procurement specifications-First edition |
|
ISO 22641 |
Space data and information transfer systems - TM (telemetry) synchronization and channel coding-First Edition |
|
ISO 22642 CORR 1 |
Space data and information transfer systems TC (telecommand) synchronization and channel coding TECHNICAL CORRIGENDUM 1-First Edition |
|
ISO 22643 |
Space Data and Information Transfer Systems - Data Entity Dictionary Specification Language (DEDSL) - XML/DTD Syntax-First Edition |
|
ISO 22645 |
Space data and information transfer systems - TM (telemetry) space data link protocol-First Edition |
|
ISO 22646 |
Space data and information transfer systems Space packet protocol-First Edition |
|
ISO 22647 |
Space data and information transfer systems Space link identifiers-First Edition |
|
ISO 22663 |
Space data and information transfer systems Proximity-1 space link protocol Data link layer-Second Edition |
|
ISO 22664 |
Space data and information transfer systems - TC (telecommand) space data link protocol-First Edition |
|
ISO 22666 |
Space data and information transfer systems AOS (advanced orbiting systems) space data link protocol-Second Edition |
|
ISO 22667 |
Space data and information transfer systems - Communication operations Procedure-1-First Edition |
|
ISO 22671 |
Space data and information transfer systems Space link extension (SLE) Forward communications link transmission unit (CLTU) service-Second edition |
|
ISO 22672 |
Space data and information transfer systems Space link extension (SLE) Forward space packet service-First Edition |
|
ISO 2277 |
Static Invertors for Aircraft-First Edition; Erratum-1973 |
|
ISO 2315 |
Aircraft - Two- and Four-Pole Sealed Electromagnetic Relays, 2 A and 3 A - Clearance and Fixing Dimensions-Second Edition |
|
ISO 23933 |
Aerospace Aramid reinforced lightweight polytetrafluoroethylene (PTFE) hose assemblies, classification 135 °C/20 684 kPa (275 °F/3 000 psi) and 135 °C/21 000 kPa (275 °F/3 046 psi) Procurement specification-First Edition |
|
ISO 23935 |
Aircraft Environmental test procedures for airborne fluid system components Resistance to fire in designated fire zones-First Edition |
|
ISO 2436 |
Heat-Resisting Equipment Wires for Aircraft - Methods of Test-First Edition |
|
ISO 244 |
Aircraft - Sealing Wire-First Edition |
|
ISO 2574 |
Aircraft - Electrical Cables - Identification Marking-Second Edition |
|
ISO 26143 |
Space data and information transfer systems Space link extension (SLE) Return operational control fields service-First Edition |
|
ISO 3168 |
Aerospace - Nuts, Anchor, Self-Locking, Fixed, Single Lug with Counterbore, with MJ Threads, Classifications: 1 100 MPa (at Ambient Temperature)/235 Degrees Celsius, 1 100 MPa (at Ambient Temperature/315 Degrees Celsius and 1 100 MPa (at Ambient Temperature)/425 Degrees Celsius - Dimensions-Second Edition |
|
ISO 3174 |
Aircraft - Connections for Checking Hydraulic Systems by Ground Appliances - Threaded Type Second Edition |
|
ISO 3221 |
Aerospace - Nuts, Anchor, Self-Locking, Fixed, 90 Degree Corner, with Counterbore, with MJ Threads, Classifications: 1 100 MPa (at Ambient Temperature)/235 Degrees Celsius, 1 100 MPa (at Ambient Temperature)/315 Degrees Celsius and 1 100 MPa (at Ambient Temperature)/425 Degrees Celsius - Dimensions-Second Edition |
|
ISO 3222 |
Aerospace - Nuts, Anchor, Self-Locking, Fixed, Closed Corner, Reduced Series, with Counterbore, with MJ Threads, Classifications: 1 100 MPa (at Ambient Temperature)/235 Degrees Celsius, 1 100 MPa (at Ambient Temperature)/315 Degrees Celsius and 1 100 MPa (at Ambient Temperature)/425 Degrees Celsius - Dimensions-Second Edition |
|
ISO 3223 |
Aerospace - Nuts, Anchor, Self-Locking, Fixed, Two Lug, with Counterbore, with MJ Threads, Classifications: 1 100 MPa (at Ambient Temperature)/235 Degrees Celsius, 1 100 MPa (at Ambient Temperature)/315 Degrees Celsius and 1 100 MPa (at Ambient Temperature)/425 Degrees Celsius - Dimensions-Second Edition |
|
ISO 3224 |
Aerospace - Nuts, Anchor, Self-Locking, Floating, Single Lug, with Counterbore, with MJ Threads, Classifications: 1 100 MPa (at Ambient Temperature)/235 Degrees Celsius, 1 100 MPa (at Ambient Temperature)/315 Degrees Celsius and 1 100 MPa (at Ambient Temperature)/425 degrees Celsius - Dimensions-Second Edition |
|
ISO 3282 |
Aircraft - Dimensions for Single-Hole and Triple-Hole Mounting (Class 3) Lever-Operated Manual Switches First Edition |
|
ISO 3323 |
Aircraft - Hydraulic Components - Marking to Indicate Fluid for Which Component is Approved Second Edition |
|
ISO 3389 |
Aircraft - Radio Frequency Flexible Coaxial Cables - Dimensions and Electrical Characteristics First Edition |
|
ISO 3456 |
Aircraft - Lever-Operated Manual Switches (Class 3) - Performance Requirements First Edition |
|
ISO 4084 |
Aircraft - Repairable Contactors (Not Hermetically Sealed) - Performance Requirements First Edition |
|
ISO 4115 |
Air Cargo Equipment - Air/Land Pallet Nets-Third Edition |
|
ISO 413 |
Aircraft - Heads of Lubricating Nipples-First Edition |
|
ISO 451 |
Aircraft - Pressure Re-Oiling Connection-First Edition; Erratum-1980 |
|
ISO 461-1 |
Aircraft - Connectors for Ground Electrical Supplies - Part 1: Design, Performance and Test Requirements-Second Edition |
|
ISO 461-2 |
Aircraft - Connectors for Ground Electrical Supplies - Part 2: Dimensions-First Edition |
|
ISO 493 |
Aircraft - Dimensions for Single-Hole Mounting (Class 1 and Class 2) Lever-Operated Manual Switches-First Edition |
|
ISO 5065-1 |
Aircraft - Magnetic Indicators - Part 1: Characteristics First Edition |
|
ISO 5065-2 |
Aircraft - Magnetic Indicators - Part 2: Tests First Edition |
|
ISO 5066-1 |
Aircraft - Hermetically Sealed Monostable Electrical Relays, 2A and 3A - Part 1: Operating Characteristics and Test Conditions First Edition |
|
ISO 5066-2 |
Aircraft - Hermetically Sealed Monostable Electrical Relays, 2A and 3A - Part 2: Type Approval Tests First Edition |
|
ISO 530 |
Aircraft - General Purpose Push-Pull Single-Pole Circuit-Breakers - Dimensions-First Edition |
|
ISO 5843-2 |
Aerospace - List of Equivalent Terms - Part 2: Aerospace Rivets Second Edition |
|
ISO 5843-4 |
Aerospace - List of Equivalent Terms - Part 4: Flight Dynamics Second Edition |
|
ISO 5843-5 |
Aerospace - List of Equivalent Terms - Part 5: Environmental and Operating Conditions for Aircraft Equipment First Edition |
|
ISO 5843-9 |
Aerospace - List of Equivalent Terms - Part 9: Aircraft First Edition |
|
ISO 5866 |
Aircraft - 2 and 3A Plug-In Base Change-Over Relays, Type II, with Crimped Connections - Clearance and Fixing Dimensions First Edition |
|
ISO 5867-1 |
Aircraft - Electromagnetic Relays and Contactors - Part 1: General Requirements First Edition |
|
ISO 5878 |
Reference Atmospheres for Aerospace Use-First Edition; Addendum 1: 1983, Addendum 2: 1983, Amendment 1: 1990 |
|
ISO 6702-1 |
Aircraft - Requirements for On-Board Weight and Balance Systems - Part 1: General First Edition; |
|
ISO 6771 |
Aerospace Fluid systems and components Pressure and temperature classifications-Third Edition |
|
ISO 6773 |
Aerospace Fluid Systems - Thermal Shock Testing of Piping and Fittings Second Edition |
|
ISO 6859-1 |
Aircraft - Proximity Switches - Part 1: General Requirements First Edition |
|
ISO 6965 |
Aircraft - Self-Propelled Gantry for Lifting Air Cargo Containers and Outside Cargoes - Functional Requirements First Edition |
|
ISO 6968 |
Aircraft ground equipment Lower deck loader Functional requirements-Third Edition |
|
ISO 7258 |
Polytetrafluoroethylene (PTFE) Tubing for Aerospace Applications - Methods for the Determination of the Density and Relative Density First Edition |
|
ISO 7313 |
Aircraft - High Temperature Convoluted Hose Assemblies in Polytetrafluoroethylene (PTFE) First Edition |
|
ISO 7315 |
Aerospace - |
|
ISO 7319 |
Aerospace - Fluid Systems - Interface of 24 Degree Cone Metric Couplings Second Edition |
|
ISO 7320 |
Aerospace - Couplings, Threaded and Sealed, for Fluid Systems - Dimensions Second Edition |
|
ISO 7332 |
Aerospace - Nuts, Anchor, Self-Locking, Floating, Two Lug, Reduced Series, with Counterbore, with MJ Threads, ClassificationS: 1 100 MPa (at Ambient Temperature)/235 Degrees Celsius, 1 100 MPa (at Ambient Temperature)/315 Degrees Celsius and 1 100 MPa (at Ambient Temperature)/425 Degrees Celsius - Dimensions-Second Edition |
|
ISO 7717 |
Aircraft - Four-Wheel-Drive Tow Tractors - Performance Requirements Factors for Design First Edition |
|
ISO 7718 |
Aircraft Main-deck passenger doors Interface requirements for connection with passenger-boarding bridge or transfer vehicle-Second Edition |
|
ISO 7913 |
Aerospace - Bolts and Screws, Metric - Tolerances of Form and Position Second Edition |
|
ISO 7961 |
Aerospace - Bolts - Test Methods First Edition |
|
ISO 8056-1 |
Aircraft - Nickel-Chromium and Nickel-Aluminium Thermocouple Extension Cables - Part 1: Conductors - General Requirements and Tests First Edition |
|
ISO 8056-3 |
Aircraft - Nickel-Chromium and Nickel-Aluminium Thermocouple Extension Cables - Part 3: Crimp-Type Ring Terminal Ends - Dimensions First Edition |
|
ISO 8056-4 |
Aircraft - Nickel-Chromium and Nickel-Aluminium Thermocouple Extension Cables - Part 4: Crimp-Type Butt Connectors - Dimensions First Edition |
|
ISO 8079 |
Aerospace Process - Anodic Treatment of Aluminium Alloys - Sulfuric Acid Process, Dyed Coating First Edition |
|
ISO 8168 |
Aerospace - Corrosion- and Heat-Resisting Steel Bolts with Strength Classification 1 100 MPa and MJ Threads - Procurement Specification First Edition |
|
ISO 8177 |
Aerospace - Omega Clamps (Saddle Clamps) for Fluid Systems - Dimensions Second Edition |
|
ISO 8267-2 |
Aircraft Tow bar attachment fittings interface requirements Part 2: Regional aircraft-First Edition; Supersedes ISO 8267:1997 |
|
ISO 8278 |
Aerospace - Hydraulic, Pressure Compensated, Variable Delivery Pumps - General Requirements First Edition |
|
ISO 8280 |
Aerospace - Rivets, Solid, Universal Head, Metallic Material, with or without Surface Treatment - Dimensions First Edition |
|
ISO 8479 |
Aerospace - |
|
ISO 8625-1 |
Aerospace - Fluid Systems - Vocabulary - Part 1: General Terms and Definitions Relating to Pressure First Edition |
|
ISO 8625-3 |
Aerospace - Fluid Systems - Vocabulary - Part 3: General Terms and Definitions Relating to Temperature First Edition |
|
ISO 8641 |
Aerospace - Self-Locking Nuts with Maximum Operating Temperature Greater Than 425 Degrees Celsius - Procurement Specification First Edition |
|
ISO 8668-1 |
Aircraft - Terminal Junction Systems - Part 1: Characteristics First Edition |
|
ISO 8668-2 |
Aircraft - Terminal Junction Systems - Part 2: Tests First Edition |
|
ISO 8668-3 |
Aircraft - Terminal Junction Systems - Part 3: Detail Specification for Type 1 System First Edition |
|
ISO 8668-4 |
Aircraft - Terminal Junction Systems - Part 4: Detail Specification for Type 2 System First Edition |
|
ISO 8668-5 |
Aircraft - Terminal Junction Systems - Part 5: Detail Specification for Type 3 System First Edition |
|
ISO 8668-6 |
Aircraft - Terminal Junction Systems - Part 6: Detail Specification for Type 4 System First Edition |
|
ISO 8775 |
Aerospace - Gaseous Oxygen Replenishment Connection for Use in Fluid Systems (New Type) - Dimensions (Inch Series) First Edition |
|
ISO 8816 |
Aircraft - Solid-State Remote Power Controllers - General Requirements First Edition |
|
ISO 9140 |
Aerospace - Nuts, Plain or Slotted (Castellated) - Test Methods-First Edition |
|
ISO 9156 |
Aerospace - Nuts, Anchor, Self-Locking, Fixed, 90 Degree Corner, Reduced Series, with Counterbore, with MJ Threads, Classifications: 1 100 MPa (at Ambient Temperature)/235 Degrees Celsius, 1 100 MPa (at Ambient Temperature)/315 Degrees Celsius and 1 100 MPa (at Ambient Temperature)/425 Degrees Celsius - Dimensions-Second Edition |
|
ISO 9216 |
Aerospace - Nuts, hexagonal, slotted (castellated), for pulleys, in alloy steel and cadmium plated or in corrosion-resistant steel and passivated - Dimensions and masses-First Edition |
|
ISO 9219 |
Aerospace - Bolts, thin hexagonal head, for pulleys, close tolerance shank, short thread, in alloy steel and cadmium plated or in titanium alloy and MoS2 lubricated or in corrosion-resistant steel and passivated - Dimensions and masses-First Edition |
|
ISO 9256 |
Aerospace - Bolts, Large Hexagonal Head, Normal or Pitch Diameter Shank, Long Length MJ Threads, Metallic Material, Coated or Uncoated, Strength Classes Less Than or Equal to 1 100 MPa - Dimensions First Edition |
|
ISO 9418 |
Aerospace - Rivets, Solid, in Aluminium or Aluminium Alloys - Procurement Specification-First Edition |
|
ISO 9528 |
Aerospace - Standard-Weight Polytetrafluoroethylene (PTFE) Hose Assemblies, Classification 204 Degrees Celsius/21 000 kPa - Procurement Specification Second Edition |
|
ISO 9538 |
Aerospace - Hydraulic Tubing Joints and Fittings - Planar Flexure Test First Edition |
|
ISO 9609 |
Aerospace - Nuts, Hexagonal, Plain, Reduced Height, Normal Across Flats, with MJ Threads, Classifications: 450 MPa (at Ambient Temp.)/120 Deg. C, 450 MPa (at Ambient Temp.)/235 Deg. C, 600 MPa (at Ambient Temp.)/425 Deg. C, 900 MPa (at Ambient Temp.)/235 Deg. C, 900 MPa (at Ambient Temp.)/315 Deg. C, 900 MPa (at Ambient Temp.)/650 Deg. C, 1 100 MPa (at Ambient Temp.)/235 Deg. C, 1 100 MPa (at-Ambient Temp.)/730 Deg. C and 1250 MPa (at Ambient Temp.)/600 Deg. C - Dimensions First Edition |
|
ISO 9634 |
Aerospace - Fluid Systems - Dimensions of Plastic Protective Caps and Plugs First Edition |
|
ISO 9666 |
Aircraft - Self-Propelled Lavatory-Servicing Vehicle - Functional Requirements First Edition |
|
ISO 9679 |
Aerospace Clamps for fluid systems Test methods-First Edition |
|
ISO 9736 |
Aerospace - Eye-Ends, in Steel, Threaded, for Aircraft Control Wire Rope - Dimensions and Loads-First Edition |
|
ISO 9738 |
Aerospace - Turnbarrels, for Aircraft Control Wire Rope - Dimensions and Loads-First Edition |
|
ISO 9747 |
Aerospace - Double-Shank Ball-Ends, in Corrosion-Resistant Steel, Swaged on Aircraft Control Wire Rope - Dimensions and Loads-First Edition |
|
ISO 9748 |
Aerospace - Ball-Ends, in corrosion-Resistant Steel, Swaged on Aircraft Control Wire Rope - Dimensions and Loads-First Edition |
|
ISO 9749 |
Aerospace - Stud-Ends, in Corrosion-Resistant Steel, Swaged on Aircraft Control Wire Rope - Dimensions and Loads-First Edition |
|
ISO 9758 |
Aerospace - Fork-Ends, in Steel, Threaded, for Rolling Bearings, for Aircraft Control Wire Rope - Dimensions and Loads-First Edition |
|
ISO 9759 |
Aerospace - Fork-Ends, in Corrosion-Resistant Steel, Swaged on Aircraft Control Wire Rope - Dimensions and Loads-First Edition |
|
ISO 9761 |
Aerospace - Locking Clips, in Corrosion-Resistant Steel, for Aircraft Control Wire Rope Turnbuckles - Dimensions-First Edition |
|
ISO 9938 |
Aerospace - Polytetrafluoroethylene (PTFE) Hose Assemblies, Classification 204 Degrees Celsius/28 000 kPa - Procurement Specification Second Edition |
|
ISO 9939 |
Aerospace - Pressure Re-Oiling Connection (New Type) First Edition |
|
ISO TR 10201 |
Aerospace - Standards for Electronic Instruments and Systems-Fourth Edition |
|
ISO TR 12198 |
Aerospace - Rivets, Solid - Materials-First Edition |
|
ISO TR 14618 |
Middle Atmosphere - Global Model at Altitudes Between 30 km and 120 km, and Wind Model at Altitudes Above 30 km First Edition |
|
ISO TR 8647 |
Environmental Degradation of Textiles Used in Air Cargo Restraint Equipment First Edition |
|
ISO 16454 |
Space systems Structural design Stress analysis requirements-First Edition |
|
ISO 21350 |
Space systems Off-the-shelf item utilization-First Edition |
|
ISO 22010 |
Space systems Mass properties control-First Edition |
|
ISO 22538-1 |
Space systems - Oxygen safety - Part 1: Design of oxygen systems and components-First Edition |
|
ISO 22538-2 |
Space systems Oxygen safety Part 2: Selection of metallic materials for oxygen systems and components-First Edition |
|
ISO 22538-3 |
Space systems Oxygen safety Part 3: Selection of non-metallic materials for oxygen systems and components-First Edition |
|
ISO 22538-4 |
Space systems - Oxygen safety - Part 4: Hazards analyses for oxygen systems and components-First Edition |
|
ISO 23041 |
Space systems Unmanned spacecraft operational procedures Documentation-First edition |