TC 20 - Aircraft and space vehicles
Items to be displayed:
Standards and projects under the direct responsibility of TC 20 Secretariat and its SCs
| Standard and/or project | ICS | TC | |
|---|---|---|---|
| ISO 11:1987 Aircraft -- Ground pressure testing connections for pressure cabins | 90.60 | 49.100 49.080 | TC 20/SC 10 |
| ISO 12:1987 Aerospace -- Pipelines -- Identification | 90.60 | 49.080 | TC 20/SC 10 |
| ISO 43:1976 Aircraft -- Jacking pads | 90.60 | 49.100 | TC 20 |
| ISO 44:1975 Aerospace -- Lever-operated, two-position, ON/OFF switches -- Directions of operation | 90.92 | 49.060 | TC 20 |
| ISO 45:1990 Aircraft -- Pressure refuelling connections | 90.60 | 49.050 49.100 49.080 | TC 20/SC 10 |
| ISO 46:1973 Aircraft -- Fuel nozzle grounding plugs and sockets | 90.60 | 49.100 | TC 20 |
| ISO 102:1990 Aircraft -- Gravity filling orifices | 90.60 | 49.080 49.100 | TC 20/SC 10 |
| ISO/TR 224:1998 Aircraft -- Declaration of design and performance for aircraft equipment -- Standard form | 60.60 | 49.020 | TC 20 |
| ISO 244:1979 Aircraft -- Sealing wire | 90.60 | 49.030.99 | TC 20 |
| ISO 245:1998 Aerospace -- Lockwire -- Diameters | 90.60 | 49.030.50 | TC 20/SC 4 |
| ISO 268:1980 Aircraft -- Mechanical and electromechanical indicators -- General requirements | 90.60 | 49.090 | TC 20 |
| ISO 413:1974 Aircraft -- Heads of lubricating nipples | 90.60 | 49.035 49.100 | TC 20 |
| ISO 451:1976 Aircraft -- Pressure re-oiling connection | 90.60 | 49.100 49.080 | TC 20/SC 10 |
| ISO 461-1:2003 Aircraft -- Connectors for ground electrical supplies -- Part 1: Design, performance and test requirements | 90.93 | 49.100 49.060 | TC 20/SC 1 |
| ISO 461-2:1985 Aircraft -- Connectors for ground electrical supplies -- Part 2: Dimensions | 90.60 | 49.100 49.060 | TC 20/SC 1 |
| ISO 482:1977 Aircraft -- Propulsion units and components -- Methods of numbering and describing direction of rotation | 90.60 | 49.050 | TC 20 |
| ISO 485:1973 Aircraft water-methanol pressure connections | 90.60 | 49.100 49.080 | TC 20/SC 10 |
| ISO 493:1975 Aircraft -- Dimensions for single-hole mounting (Class 1 and Class 2) lever-operated manual switches | 90.93 | 49.060 | TC 20/SC 1 |
| ISO 530:1975 Aircraft -- General purpose push-pull single-pole circuit-breakers -- Dimensions | 90.93 | 49.060 | TC 20/SC 1 |
| ISO 1002:1983 Rolling bearings -- Airframe bearings -- Characteristics, boundary dimensions, tolerances, static load ratings | 90.93 | 49.035 | TC 20/SC 15 |
| ISO 1021:1980 Aircraft -- Engine nacelle fire extinguisher apertures and doors | 90.60 | 49.100 | TC 20 |
| ISO 1022:1988 Aerospace -- Gaseous oxygen replenishment connection for use in fluid systems (old type) -- Dimensions (Inch series) (Not valid for new designs) | 90.60 | 49.100 49.080 | TC 20/SC 10 |
| ISO 1023:1974 Aircraft -- High pressure air charging valves | 90.93 | 49.100 49.080 | TC 20/SC 10 |
| ISO 1033:1975 Aircraft -- Dimensions for general purpose push-pull three-pole circuit-breakers | 90.93 | 49.060 | TC 20/SC 1 |
| ISO 1034:1973 Aircraft -- Ground air-conditioning connections | 90.60 | 49.100 49.080 | TC 20/SC 10 |
| ISO 1151-1:1988 Flight dynamics -- Concepts, quantities and symbols -- Part 1: Aircraft motion relative to the air | 90.60 | 01.060 49.020 | TC 20 |
| ISO 1151-2:1985 Flight dynamics -- Concepts, quantities and symbols -- Part 2: Motions of the aircraft and the atmosphere relative to the Earth | 90.60 | 01.060 49.020 | TC 20 |
| ISO 1151-2:1985/Add 1:1987 | 60.60 | 01.060 49.020 | TC 20 |
| ISO 1151-3:1989 Flight dynamics -- Concepts, quantities and symbols -- Part 3: Derivatives of forces, moments and their coefficients | 90.60 | 01.060 49.020 | TC 20 |
| ISO 1151-3:1989/Cor 1:1996 | 60.60 | 01.060 49.020 | TC 20 |
| ISO 1151-4:1994 Flight dynamics -- Concepts, quantities, and symbols -- Part 4: Concepts and quantities used in the study of aircraft stability and control | 90.20 | 01.060 49.020 | TC 20 |
| ISO 1151-5:1987 Flight dynamics -- Concepts, quantities and symbols -- Part 5: Quantities used in measurements | 90.60 | 01.060 49.020 | TC 20 |
| ISO 1151-6:1982 Terms and symbols for flight dynamics -- Part 6: Aircraft geometry | 90.60 | 01.060 49.020 | TC 20 |
| ISO 1151-6:1982/Amd 1:1984 | 60.60 | 01.060 49.020 | TC 20 |
| ISO 1151-7:1985 Flight dynamics -- Concepts, quantities and symbols -- Part 7: Flight points and flight envelopes | 90.60 | 49.020 01.060 | TC 20 |
| ISO 1151-8:1992 Flight dynamics -- Concepts, quantities and symbols -- Part 8: Concepts and quantities used in the study of the dynamic behaviour of the aircraft | 90.60 | 01.060 49.020 | TC 20 |
| ISO 1151-9:1993 Flight dynamics -- Concepts, quantities and symbols -- Part 9: Models of atmospheric motions along the trajectory of the aircraft | 90.60 | 01.060 49.020 | TC 20 |
| ISO 1151-9:1993/Amd 1:1998 Turbulence | 60.60 | 01.060 49.020 | TC 20 |
| ISO 1198:1972 Sealed-beam landing lamps for aircraft -- Dimensions | 90.93 | 49.060 | TC 20/SC 1 |
| ISO 1464:1985 Aerospace -- Tripod jacks -- Clearance dimensions | 90.93 | 49.100 | TC 20/SC 9 |
| ISO 1465:1989 Aircraft -- Liquid oxygen replenishment couplings -- Mating dimensions | 90.20 | 49.100 49.080 | TC 20/SC 10 |
| ISO 1466:1973 Lever-operated manual switches for aircraft -- Performance requirements | 90.60 | 49.060 | TC 20/SC 1 |
| ISO 1467:1973 General purpose push-pull single-pole circuit-breakers for aircraft -- Performance requirements | 90.60 | 49.060 | TC 20/SC 1 |
| ISO 1509:1973 General purpose push-pull three-pole circuit-breakers for aircraft -- Performance requirements | 90.60 | 49.060 | TC 20/SC 1 |
| ISO 1540:2006 Aerospace -- Characteristics of aircraft electrical systems | 90.60 | 49.060 | TC 20/SC 1 |
| ISO 1547:1975 Aircraft -- Precision fuse-links -- General requirements | 90.93 | 49.060 | TC 20/SC 1 |
| ISO 1548:1976 Aircraft -- Precision fuse-links -- Type A | 90.93 | 49.060 | TC 20/SC 1 |
| ISO 1549:1976 Aircraft -- Precision fuse-links -- Type B | 90.93 | 49.060 | TC 20/SC 1 |
| ISO 1749:1973 Aircraft -- Elastomeric sealing rings -- Packaging and identification | 90.20 | 83.140.50 49.080 | TC 20/SC 10 |
| ISO 1949:1987 Aircraft -- Electrical connectors -- Design requirements | 90.92 | 49.060 | TC 20/SC 1 |
| ISO 1950:1974 Aircraft -- Identification of servicing, maintenance, ground handling and safety/hazard points | 90.93 | 49.100 | TC 20/SC 9 |
| ISO 1965:1973 Aluminium terminal ends for crimping to aircraft aluminium electrical cables | 90.93 | 49.060 | TC 20/SC 1 |
| ISO 1966:1973 Crimped joints for aircraft electrical cables | 90.93 | 49.060 | TC 20/SC 1 |
| ISO 1967:1974 Aircraft -- Fire-resisting electrical cables -- Dimensions, conductor resistance and mass | 90.60 | 49.060 | TC 20/SC 1 |
| ISO 1971:1975 Aircraft -- Accessory drives and mounting pads | 90.60 | 49.035 | TC 20 |
| ISO 2020-1:1997 Aerospace -- Preformed flexible steel wire rope for aircraft controls -- Part 1: Dimensions and loads | 90.60 | 49.035 | TC 20 |
| ISO 2020-2:1997 Aerospace -- Preformed flexible steel wire rope for aircraft controls -- Part 2: Technical specification | 90.60 | 49.035 | TC 20 |
| ISO 2026:1974 Aircraft -- Connections for starting engines by air | 90.60 | 49.100 49.080 | TC 20/SC 10 |
| ISO 2032:1973 Heat-resisting equipment wires for aircraft | 90.93 | 49.060 | TC 20/SC 1 |
| ISO 2042:1973 Aircraft electrical circuit diagrams | 90.60 | 49.060 | TC 20/SC 1 |
| ISO 2046:1973 Gaseous breathing oxygen supplies for aircraft | 90.60 | 49.100 | TC 20/SC 10 |
| ISO 2100:1987 Aircraft -- Electrical connectors -- Tests | 90.93 | 49.060 | TC 20/SC 1 |
| ISO 2155:1974 Aircraft -- Fire-resisting electrical cables -- Performance requirements | 90.60 | 49.060 | TC 20/SC 1 |
| ISO 2156:1974 Aircraft -- Fire-resisting electrical cables -- Methods of test | 90.60 | 49.060 | TC 20/SC 1 |
| ISO 2277:1973 Static invertors for aircraft | 90.93 | 49.060 | TC 20/SC 1 |
| ISO 2315:1980 Aircraft -- Two- and four-pole sealed electromagnetic relays, 2 A and 3 A -- Clearance and fixing dimensions | 90.93 | 49.060 | TC 20/SC 1 |
| ISO 2434:1973 Compressed non-breathing air for use in aircraft | 90.60 | 49.100 | TC 20/SC 10 |
| ISO 2435:1973 Nitrogen for use in aircraft | 90.60 | 49.100 | TC 20/SC 10 |
| ISO 2436:1973 Heat-resisting equipment wires for aircraft -- Methods of test | 90.93 | 49.060 | TC 20/SC 1 |
| ISO 2533:1975 Standard Atmosphere | 90.60 | 07.060 19.020 17.020 49.020 | TC 20/SC 6 |
| ISO 2533:1975/Add 1:1985 Hypsometrical tables | 60.60 | 07.060 19.020 17.020 49.020 | TC 20/SC 6 |
| ISO 2533:1975/Add 2:1997 Extension to - 5000 m and standard atmosphere as a function of altitude in feet | 60.60 | 07.060 19.020 17.020 49.020 | TC 20/SC 6 |
| ISO 2563:2009 Aircraft ducting and piping -- Profile dimensions for flanges of V-band couplings | 60.60 | 49.080 | TC 20/SC 10 |
| ISO 2574:1994 Aircraft -- Electrical cables -- Identification marking | 90.93 | 49.060 01.070 | TC 20/SC 1 |
| ISO 2635:2003 Aircraft -- Conductors for general purpose aircraft electrical cables and aerospace applications -- Dimensions and characteristics | 90.93 | 49.060 | TC 20/SC 1 |
| ISO 2669:1995 Environmental tests for aircraft equipment -- Steady-state acceleration | 90.60 | 49.020 | TC 20 |
| ISO 2671:1982 Environmental tests for aircraft equipment -- Part 3.4 : Acoustic vibration | 90.60 | 49.020 17.140.30 | TC 20 |
| ISO 2678:1985 Environmental tests for aircraft equipment -- Insulation resistance and high voltage tests for electrical equipment | 90.93 | 49.060 | TC 20/SC 1 |
| ISO 2685:1998 Aircraft -- Environmental test procedure for airborne equipment -- Resistance to fire in designated fire zones | 90.60 | 49.020 | TC 20 |
| ISO 2964:1985 Aerospace -- Tubing -- Outside diameters and thicknesses -- Metric dimensions | 90.60 | 49.080 | TC 20/SC 10 |
| ISO 3161:1999 Aerospace -- UNJ threads -- General requirements and limit dimensions | 90.20 | 49.030.10 | TC 20/SC 4 |
| ISO 3168:1998 Aerospace -- Nuts, anchor, self-locking, fixed, single lug, with counterbore, with MJ threads, classifications: 1 100 MPa (at ambient temperature )/235 degrees C, 1 100 MPa (at ambient temperature )/315 degrees C and 1 100 MPa (at ambient temperature)/425 degrees C -- Dimensions | 90.60 | 49.030.30 | TC 20/SC 4 |
| ISO 3174:1994 Aircraft -- Connections for checking hydraulic systems by ground appliances -- Threaded type | 90.20 | 49.080 49.100 | TC 20/SC 10 |
| ISO 3185:2008 Aerospace -- Bolts, normal bihexagonal head, normal shank, short or medium length MJ threads, metallic material, coated or uncoated, strength classes less than or equal to 1 100 MPa -- Dimensions | 60.60 | 49.030.20 | TC 20/SC 4 |
| ISO 3186:2008 Aerospace -- Bolts, large bihexagonal head, normal shank, short or medium length MJ threads, metallic material, coated or uncoated, strength classes 1 250 MPa to 1 800 MPa -- Dimensions | 60.60 | 49.030.20 | TC 20/SC 4 |
| ISO 3191:1998 Aerospace -- Nuts, anchor, self-locking, fixed, single lug, reduced series, with counterbore, with MJ threads, classifications: 1 100 MPa (at ambient temperature)/235 degrees C, 1 100 MPa (at ambient temperature)/315 degrees C and 1 100 MPa (at ambient temperature)/425 degrees C -- Dimensions | 90.60 | 49.030.30 | TC 20/SC 4 |
| ISO 3193:2008 Aerospace -- Bolts, normal hexagonal head, normal shank, short or medium length MJ threads, metallic material, coated or uncoated, strength classes less than or equal to 1 100 MPa -- Dimensions | 60.60 | 49.030.20 | TC 20/SC 4 |
| ISO 3202:1997 Aerospace -- Screws, pan head, internal offset cruciform ribbed or unribbed drive, threaded to head, MJ threads, metallic material, coated or uncoated, strength classes less than or equal to 1 100 MPa -- Dimensions | 90.60 | 49.030.20 | TC 20/SC 4 |
| ISO 3203:1993 Aerospace -- Bolts, normal bihexagonal 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 | 90.20 | 49.030.20 | TC 20/SC 4 |
| ISO 3209:1998 Aerospace -- Nuts, anchor, self-locking, floating, two lug, with counterbore, with MJ threads, classifications: 1 100 MPa (at ambient temperature )/235 degrees C, 1 100 MPa (at ambient temperature )/315 degrees C and 1 100 MPa (at ambient temperature)/425 degrees C -- Dimensions | 90.60 | 49.030.30 | TC 20/SC 4 |
| ISO 3221:1998 Aerospace -- Nuts, anchor, self-locking, fixed, 90 degrees corner, with counterbore, with MJ threads, classifications: 1 100 MPa (at ambient temperature)/235 degrees C, 1 100 MPa (at ambient temperature)/315 degrees C and 1 100 MPa (at ambient temperature)/425 degrees C -- Dimensions | 90.60 | 49.030.30 | TC 20/SC 4 |
| ISO 3222:1998 Aerospace -- Nuts, anchor, self-locking, fixed, closed corner, reduced series, with counterbore, with MJ threads, classifications: 1 100 MPa (at ambient temperature)/235 degrees C, 1 100 MPa (at ambient temperature)/315 degrees C and 1 100 MPa (at ambient temperature)/425 degrees C -- Dimensions | 90.60 | 49.030.30 | TC 20/SC 4 |
| ISO 3223:1998 Aerospace -- Nuts, anchor, self-locking, fixed, two lug, with counterbore, with MJ threads, classifications: 1 100 MPa (at ambient temperature )/235 degrees C, 1 100 MPa (at ambient temperature )/315 degrees C and 1 100 MPa (at ambient temperature)/425 degrees C -- Dimensions | 90.60 | 49.030.30 | TC 20/SC 4 |
| ISO 3224:1998 Aerospace -- Nuts, anchor, self-locking, floating, single lug, with counterbore, with MJ threads, classifications: 1 100 MPa (at ambient temperature )/235 degrees C, 1 100 MPa (at ambient temperature )/315 degrees C and 1 100 MPa (at ambient temperature)/425 degrees C -- Dimensions | 90.60 | 49.030.30 | TC 20/SC 4 |
| ISO 3225:1998 Aerospace -- Nuts, anchor, self-locking, fixed, two lug, reduced series, with counterbore, with MJ threads, classifications: 1 100 MPa (at ambient temperature)/235 degrees C, 1 100 MPa (at ambient temperature)/315 degrees C and 1 100 MPa (at ambient temperature)/425 degrees C -- Dimensions | 90.60 | 49.030.30 | TC 20/SC 4 |
| ISO 3230:1998 Aerospace -- Rivets, solid, 100 degrees normal countersunk head with dome, metallic material, with or without surface treatment -- Dimensions | 90.60 | 49.030.60 | TC 20/SC 4 |
| ISO 3282:1976 Aircraft -- Dimensions for single-hole and triple-hole mounting (Class 3) lever-operated manual switches | 90.93 | 49.060 | TC 20/SC 1 |
| ISO 3323:1987 Aircraft -- Hydraulic components -- Marking to indicate fluid for which component is approved | 90.60 | 49.080 | TC 20/SC 10 |
| ISO 3353-1:2002 Aerospace -- Lead and runout threads -- Part 1: Rolled external threads | 90.60 | 49.030.10 | TC 20/SC 4 |
| ISO 3353-2:2002 Aerospace -- Lead and runout threads -- Part 2: Internal threads | 90.60 | 49.030.10 | TC 20/SC 4 |
| ISO 3456:1975 Aircraft -- Lever-operated manual switches (Class 3) -- Performance requirements | 90.93 | 49.060 | TC 20/SC 1 |
| ISO 4084:1977 Aircraft -- Repairable contactors (not hermetically sealed) -- Performance requirements | 90.60 | 49.060 | TC 20/SC 1 |
| ISO 4095:1998 Aerospace -- Bihexagonal drives -- Wrenching configuration -- Metric series | 90.60 | 49.030.20 | TC 20/SC 4 |
| ISO 4115:1997 Air cargo equipment -- Air/land pallet nets | 90.93 | 55.180.30 | TC 20/SC 9 |
| ISO 4116:1986 Air cargo equipment -- Ground equipment requirements for compatibility with aircraft unit load devices | 90.93 | 49.120 49.100 | TC 20/SC 9 |
| ISO 4117:1993 Air and air/land cargo pallets -- Specification and testing | 90.93 | 55.180.30 | TC 20/SC 9 |
| ISO 4118:2005 Air cargo -- Non-certified containers for the lower deck of large-capacity aircraft -- Specification and testing | 90.60 | 55.180.30 | TC 20/SC 9 |
| ISO 4128:1985 Aircraft -- Air mode modular containers | 90.93 | 55.180.30 | TC 20/SC 9 |
| ISO 4147:1997 Aerospace -- Nuts, hexagonal, slotted (castellated), normal height, normal across flats, with MJ threads, classifications: 600 MPa (at ambient temperature)/120 degrees C, 600 MPa (at ambient temperature)/235 degrees C, 900 MPa (at ambient temperature)/425 degrees C, 1 100 MPa (at ambient temperature)/235 degrees C, 1 100 MPa (at ambient temperature)/315 degrees C, 1 100 MPa (at ambient temperature)/650 degrees C, 1 210 MPa (at ambient temperature)/730 degrees C, 1 250 MPa (at ambient temperature)/235 degrees C and 1 550 MPa (at ambient temperature)/600 degrees C -- Dimensions | 90.60 | 49.030.30 | TC 20/SC 4 |
| ISO 4153:1981 Aircraft -- Pressure fuel dispensing system -- Test procedure and limit value for shut-off surge pressure | 90.60 | 49.100 49.050 | TC 20 |
| ISO 4170:1995 Air cargo equipment -- Interline pallet nets | 90.93 | 55.180.30 | TC 20/SC 9 |
| ISO 4171:1993 Air cargo equipment -- Interline pallets | 90.93 | 55.180.30 | TC 20/SC 9 |
| ISO 5065-1:1986 Aircraft -- Magnetic indicators -- Part 1: Characteristics | 90.60 | 49.090 | TC 20/SC 1 |
| ISO 5065-2:1986 Aircraft -- Magnetic indicators -- Part 2: Tests | 90.93 | 49.090 | TC 20/SC 1 |
| ISO 5066-1:1986 Aircraft -- Hermetically sealed monostable electrical relays, 2A and 3A -- Part 1: Operating characteristics and test conditions | 90.93 | 49.060 | TC 20/SC 1 |
| ISO 5066-2:1986 Aircraft -- Hermetically sealed monostable electrical relays, 2A and 3A -- Part 2: Type approval tests | 90.93 | 49.060 | TC 20/SC 1 |
| ISO 5843-1:1985 Aerospace construction -- List of equivalent terms -- Part 1: Aerospace electrical equipment | 90.60 | 01.040.49 49.060 | TC 20/SC 8 |
| ISO 5843-2:1990 Aerospace -- List of equivalent terms -- Part 2: Aerospace rivets | 90.60 | 01.040.49 49.030.60 | TC 20/SC 8 |
| ISO 5843-3:1997 Aerospace -- List of equivalent terms -- Part 3: Aerospace bolts and nuts | 90.60 | 01.040.49 49.030.30 49.030.20 | TC 20/SC 8 |
| ISO 5843-4:1990 Aerospace -- List of equivalent terms -- Part 4: Flight dynamics | 90.60 | 01.040.49 49.020 | TC 20/SC 8 |
| ISO 5843-5:1990 Aerospace -- List of equivalent terms -- Part 5: Environmental and operating conditions for aircraft equipment | 90.60 | 01.040.49 49.020 | TC 20/SC 8 |
| ISO 5843-6:1985 Aerospace -- List of equivalent terms -- Part 6: Standard atmosphere | 90.60 | 01.040.49 49.020 | TC 20/SC 8 |
| ISO 5843-8:1988 Aerospace -- List of equivalent terms -- Part 8: Aircraft reliability | 90.60 | 01.040.49 49.020 | TC 20/SC 8 |
| ISO 5843-9:1988 Aerospace -- List of equivalent terms -- Part 9: Aircraft | 90.60 | 01.040.49 49.020 | TC 20/SC 8 |
| ISO 5843-10:1988 Aerospace -- List of equivalent terms -- Part 10: Aircraft structure | 90.60 | 01.040.49 49.045 | TC 20/SC 8 |
| ISO 5855-1:1999 Aerospace -- MJ threads -- Part 1: General requirements | 90.20 | 49.030.10 | TC 20/SC 4 |
| ISO 5855-2:1999 Aerospace -- MJ threads -- Part 2: Limit dimensions for bolts and nuts | 90.20 | 49.030.10 | TC 20/SC 4 |
| ISO 5855-3:1999 Aerospace -- MJ threads -- Part 3: Limit dimensions for fittings for fluid systems | 90.20 | 49.030.10 | TC 20/SC 4 |
| ISO 5856:2008 Aerospace -- Screws, 100 degrees normal 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 | 60.60 | 49.030.20 | TC 20/SC 4 |
| ISO 5857:2008 Aerospace -- Bolts, with MJ threads, made of alloy steel, strength class 1 250 MPa -- Procurement specification | 60.60 | 49.030.20 | TC 20/SC 4 |
| ISO 5858:1999 Aerospace -- Nuts, self-locking, with maximum operating temperature less than or equal to 425 degrees C -- Procurement specification | 90.20 | 49.030.30 | TC 20/SC 4 |
| ISO 5859:1991 Aerospace -- Graphic symbols for schematic drawings of hydraulic and pneumatic systems and components | 90.60 | 49.080 01.080.30 | TC 20/SC 10 |
| ISO 5866:1983 Aircraft -- 2 and 3A plug-in base change-over relays, Type II, with crimped connections -- Clearance and fixing dimensions | 90.93 | 49.060 | TC 20/SC 1 |
| ISO 5867-1:1996 Aircraft -- Electromagnetic relays and contactors -- Part 1: General requirements | 90.93 | 49.060 | TC 20/SC 1 |
| ISO 5878:1982 Reference atmospheres for aerospace use | 90.60 | 49.020 | TC 20/SC 6 |
| ISO 5878:1982/Add 1:1983 Wind supplement | 60.60 | 49.020 | TC 20/SC 6 |
| ISO 5878:1982/Amd 1:1990 | 60.60 | 49.020 | TC 20/SC 6 |
| ISO 5878:1982/Add 2:1983 Air humidity in the Northern Hemisphere | 60.60 | 49.020 | TC 20/SC 6 |
| ISO 5884:1987 Aerospace -- Fluid systems and components -- Methods for system sampling and measuring the solid particle contamination of hydraulic fluids | 90.60 | 49.080 | TC 20/SC 10 |
| ISO 5887:1981 Aircraft -- Joints for connecting crew members' regulator masks to oxygen sources | 90.60 | 49.080 | TC 20/SC 10 |
| ISO 6517:1992 Air cargo equipment -- Base-restrained certified containers exclusively for the lower deck of high-capacity aircraft | 90.92 | 55.180.30 | TC 20/SC 9 |
| ISO 6702-1:1991 Aircraft -- Requirements for on-board weight and balance systems -- Part 1: General | 90.93 | 49.120 49.090 | TC 20/SC 9 |
| ISO 6702-2:1991 Aircraft -- Requirements for on-board weight and balance systems -- Part 2: Design, performance and interface characteristics | 90.93 | 49.120 49.090 | TC 20/SC 9 |
| ISO 6771:2007 Aerospace -- Fluid systems and components -- Pressure and temperature classifications | 60.60 | 49.080 | TC 20/SC 10 |
| ISO 6772:1988 Aerospace -- Fluid systems -- Impulse testing of hydraulic hose, tubing and fitting assemblies | 90.92 | 83.140.40 49.080 | TC 20/SC 10 |
| ISO 6773:1994 Aerospace -- Fluid systems -- Thermal shock testing of piping and fittings | 90.20 | 49.080 | TC 20/SC 10 |
| ISO 6858:1982 Aircraft -- Ground support electrical supplies -- General requirements | 90.93 | 49.100 49.060 | TC 20/SC 1 |
| ISO 6859-1:1982 Aircraft -- Proximity switches -- Part 1: General requirements | 90.60 | 49.060 | TC 20/SC 1 |
| ISO 6965:1982 Aircraft -- Self-propelled gantry for lifting air cargo containers and outsize cargoes -- Functional requirements | 90.92 | 49.120 49.100 | TC 20/SC 9 |
| ISO 6966-1:2005 Aircraft ground equipment -- Basic requirements -- Part 1: General design requirements | 90.60 | 49.120 49.100 | TC 20/SC 9 |
| ISO 6966-2:2005 Aircraft ground equipment -- Basic requirements -- Part 2: Safety requirements | 90.60 | 49.100 49.120 | TC 20/SC 9 |
| ISO 6967:2006 Aircraft ground equipment -- Main deck loader -- Functional requirements | 90.60 | 49.120 49.100 | TC 20/SC 9 |
| ISO 6968:2005 Aircraft ground equipment -- Lower deck loader -- Functional requirements | 90.60 | 49.120 49.100 | TC 20/SC 9 |
| ISO 7137:1995 Aircraft -- Environmental conditions and test procedures for airborne equipment | 90.60 | 49.020 | TC 20 |
| ISO 7166:1985 Aircraft -- Rail and stud configuration for passenger equipment and cargo restraint | 90.93 | 49.120 | TC 20/SC 9 |
| ISO 7169:2007 Aerospace -- Separable tube fittings for fluid systems, for 24 degree cones, for pressures up to 3 000 psi or 21 000 kPa -- Procurement specification, inch/metric | 60.60 | 49.080 | TC 20/SC 10 |
| ISO 7257:1983 Aircraft -- Hydraulic tubing joints and fittings -- Rotary flexure test | 90.60 | 49.080 | TC 20/SC 10 |
| ISO 7258:1984 Polytetrafluoroethylene (PTFE) tubing for aerospace applications -- Methods for the determination of the density and relative density | 90.20 | 83.140.40 49.080 | TC 20/SC 10 |
| ISO 7313:1984 Aircraft -- High temperature convoluted hose assemblies in polytetrafluoroethylene (PTFE) | 90.60 | 49.080 83.140.40 | TC 20/SC 10 |
| ISO 7314:2002 Aerospace -- Fluid systems -- Metal hose assemblies | 90.60 | 49.080 | TC 20/SC 10 |
| ISO 7315:1988 Aerospace -- "P" clamps (loop clamps) for fluid systems -- Envelope dimensions | 90.60 | 49.080 | TC 20/SC 10 |
| ISO 7319:1992 Aerospace -- Fluid systems -- Interface of 24 degree cone metric couplings | 90.60 | 49.080 | TC 20/SC 10 |
| ISO 7320:1992 Aerospace -- Couplings, threaded and sealed, for fluid systems -- Dimensions | 90.60 | 49.080 | TC 20/SC 10 |
| ISO 7332:1998 Aerospace -- Nuts, anchor, self-locking, floating, two lug, reduced series, with counterbore, with MJ threads, classifications: 1 100 MPa (at ambient temperature)/235 degrees C, 1 100 MPa (at ambient temperature)/315 degrees C and 1 100 MPa (at ambient temperature)/425 degrees C -- Dimensions | 90.60 | 49.030.30 | TC 20/SC 4 |
| ISO 7403:1998 Aerospace -- Spline drives -- Wrenching configuration -- Metric series | 90.60 | 49.030.20 | TC 20/SC 4 |
| ISO 7481:2000 Aerospace -- Nuts, self-locking, with maximum operating temperature less than or equal to 425 degrees C -- Test methods | 90.60 | 49.030.30 | TC 20/SC 4 |
| ISO 7661:1984 Aerospace -- Fluid systems -- Clamp blocks for tube lines having axial alignment -- Design standard and qualification testing -- Metric series | 90.20 | 49.080 | TC 20/SC 10 |
| ISO 7689:2008 Aerospace -- Bolts, with MJ threads, made of alloy steel, strength class 1 100 MPa -- Procurement specification | 60.60 | 49.030.20 | TC 20/SC 4 |
| ISO 7715:1985 Air cargo equipment -- Ground handling and transport systems for unit load devices -- Minimum requirements | 90.93 | 49.120 | TC 20/SC 9 |
| ISO 7716:1985 Air cargo equipment -- Unit load devices transport vehicle (UTV) -- Functional requirements | 90.93 | 49.100 49.120 | TC 20/SC 9 |
| ISO 7717:1985 Aircraft -- Four-wheel-drive tow tractors -- Performance requirements factors for design | 90.93 | 49.100 | TC 20/SC 9 |
| ISO 7718-1:2009 Aircraft -- Passenger doors interface requirements for connection of passenger boarding bridge -- Part 1: Main deck doors | 60.60 | 49.100 | TC 20/SC 9 |
| ISO 7718-2:2009 Aircraft -- Passenger doors interface requirements for connection of passenger boarding bridge -- Part 2: Upper deck doors | 60.60 | 49.100 | TC 20/SC 9 |
| ISO 7913:1994 Aerospace -- Bolts and screws, metric -- Tolerances of form and position | 90.60 | 49.030.20 | TC 20/SC 4 |
| ISO 7938:1986 Aircraft -- Ball bearings for control cable pulleys -- Dimensions and loads | 90.93 | 49.035 | TC 20/SC 15 |
| ISO 7939:1988 Aircraft -- Non-metallic pulleys with ball bearings for control cables -- Dimensions and loads | 90.60 | 49.035 | TC 20 |
| ISO 7961:1994 Aerospace -- Bolts -- Test methods | 90.60 | 49.030.20 | TC 20/SC 4 |
| ISO 7995:2002 Aerospace -- Nuts, hexagonal, self-locking, with MJ threads, classifications: 1 100 MPa (at ambient temperature)/235 degrees C, 1 100 MPa (at ambient temperature)/315 degrees C and 1 100 MPa (at ambient temperature)/425 degrees C -- Dimensions | 90.60 | 49.030.30 | TC 20/SC 4 |
| ISO 8056-1:1985 Aircraft -- Nickel-chromium and nickel-aluminium thermocouple extension cables -- Part 1: Conductors -- General requirements and tests | 90.93 | 49.060 | TC 20/SC 1 |
| ISO 8056-2:1988 Aircraft -- Nickel-chromium and nickel-aluminium thermocouple extension cables -- Part 2: Terminations -- General requirements and tests | 90.60 | 49.060 | TC 20/SC 1 |
| ISO 8056-3:1987 Aircraft -- Nickel-chromium and nickel-aluminium thermocouple extension cables -- Part 3: Crimp-type ring terminal ends -- Dimensions | 90.60 | 49.060 | TC 20/SC 1 |
| ISO 8056-4:1987 Aircraft -- Nickel-chromium and nickel-aluminium thermocouple extension cables -- Part 4: Crimp-type butt connectors -- Dimensions | 90.60 | 49.060 | TC 20/SC 1 |
| ISO 8058:1999 Air cargo -- Insulated container -- Thermal efficiency requirements | 90.93 | 55.180.30 | TC 20/SC 9 |
| ISO 8074:1985 Aerospace -- Surface treatment of austenitic stainless steel parts | 90.60 | 49.040 | TC 20 |
| ISO 8075:1985 Aerospace -- Surface treatment of hardenable stainless steel parts | 90.60 | 49.040 | TC 20 |
| ISO 8078:1984 Aerospace process -- Anodic treatment of aluminium alloys -- Sulfuric acid process, undyed coating | 90.20 | 49.040 | TC 20 |
| ISO 8079:1984 Aerospace process -- Anodic treatment of aluminium alloys -- Sulfuric acid process, dyed coating | 90.20 | 49.040 | TC 20 |
| ISO 8080:1985 Aerospace -- Anodic treatment of titanium and titanium alloys -- Sulfuric acid process | 90.60 | 49.040 | TC 20 |
| ISO 8081:1985 Aerospace process -- Chemical conversion coating for aluminium alloys -- General purpose | 90.60 | 49.040 | TC 20 |
| ISO 8097:2001 Aircraft -- Minimum airworthiness requirements and test conditions for certified air cargo unit load devices | 90.93 | 55.180.30 | TC 20/SC 9 |
| ISO 8153-1:2009 Aerospace fluid systems and components -- Vocabulary -- Part 1: Hose assemblies | 60.60 | 01.040.83 83.140.40 01.040.49 49.080 | TC 20/SC 10 |
| ISO 8168:2008 Aerospace -- Bolts, with MJ threads, made of heat and corrosion resisting steel, strength class 1 100 MPa -- Procurement specification | 60.60 | 49.030.20 | TC 20/SC 4 |
| ISO 8177:1986 Aerospace -- Omega clamps (saddle clamps) for fluid systems -- Dimensions | 90.60 | 49.080 | TC 20/SC 10 |
| ISO 8267-1:2005 Aircraft -- Tow bar attachment fittings interface requirements -- Part 1: Main line aircraft | 90.60 | 49.100 | TC 20/SC 9 |
| ISO 8267-2:2005 Aircraft -- Tow bar attachment fittings interface requirements -- Part 2: Regional aircraft | 90.60 | 49.100 | TC 20/SC 9 |
| ISO 8268:1987 Air cargo equipment -- Automobile transport devices -- Basic requirements | 90.93 | 49.120 | TC 20/SC 9 |
| ISO 8278:1986 Aerospace -- Hydraulic, pressure compensated, variable delivery pumps -- General requirements | 90.60 | 49.080 | TC 20/SC 10 |
| ISO 8279:2008 Aerospace -- Nuts, hexagonal, plain, normal height, normal across flats, with MJ threads, classifications: 600 MPa (at ambient temperature)/120 degrees C, 600 MPa (at ambient temperature)/235 degrees C, 900 MPa (at ambient temperature)/425 degrees C, 1 100 MPa (at ambient temperature)/235 degrees C, 1 100 MPa (at ambient temperature)/315 degrees C, 1 100 MPa (at ambient temperature)/650 degrees C, 1 210 MPa (at ambient temperature)/730 degrees C, 1 250 MPa (at ambient temperature)/235 degrees C and 1 550 MPa (at ambient temperature)/600 degrees C -- Dimensions | 60.60 | 49.030.30 | TC 20/SC 4 |
| ISO 8280:1993 Aerospace -- Rivets, solid, universal head, metallic material, with or without surface treatment -- Dimensions | 90.20 | 49.030.60 | TC 20/SC 4 |
| ISO 8323:1985 Freight containers -- Air/surface (intermodal) general purpose containers -- Specification and tests | 90.93 | 55.180.10 | TC 20/SC 9 |
| ISO 8399-1:1998 Aerospace -- Accessory drives and mounting flanges (Metric series) -- Part 1: Design criteria | 90.60 | 49.035 | TC 20 |
| ISO 8399-2:1998 Aerospace -- Accessory drives and mounting flanges (Metric series) -- Part 2: Dimensions | 90.60 | 49.035 | TC 20 |
| ISO 8479:1986 Aerospace -- "Q" clamps (centre-mounted clamps) for fluid systems -- Dimensions | 90.60 | 49.080 | TC 20/SC 10 |
| ISO 8538:1999 Aerospace -- Nuts, hexagonal, self-locking, with counterbore and captive washer, with MJ threads, classifications: 1 100 MPa (at ambient temperature)/235 degrees C, 1 100 MPa (at ambient temperature)/315 degrees C and 1 100 MPa (at ambient temperature)/425 degrees C -- Dimensions | 90.20 | 49.030.30 | TC 20/SC 4 |
| ISO 8574:2004 Aerospace -- Hydraulic system tubing -- Qualification tests for bent tubes | 90.60 | 49.080 | TC 20/SC 10 |
| ISO 8575:1990 Aerospace -- Fluid systems -- Hydraulic system tubing | 90.92 | 49.080 | TC 20/SC 10 |
| ISO 8591-1:1989 Aerospace -- Wrought aluminium and aluminium alloys -- Inspection, testing and supply requirements -- Part 1: General requirements | 90.20 | 49.025.20 | TC 20 |
| ISO 8625-1:1993 Aerospace -- Fluid systems -- Vocabulary -- Part 1: General terms and definitions related to pressure | 90.60 | 49.080 01.040.49 | TC 20/SC 10 |
| ISO 8625-2:1991 Aerospace -- Fluid systems -- Vocabulary -- Part 2: General terms and definitions relating to flow | 90.60 | 49.080 01.040.49 | TC 20/SC 10 |
| ISO 8625-3:1991 Aerospace -- Fluid systems -- Vocabulary -- Part 3: General terms and definitions relating to temperature | 90.60 | 01.040.49 49.080 | TC 20/SC 10 |
| ISO 8641:2008 Aerospace -- Self-locking nuts with maximum operating temperature greater than 425 degrees C -- Procurement specification | 60.60 | 49.030.30 | TC 20/SC 4 |
| ISO 8642:2008 Aerospace -- Self-locking nuts with maximum operating temperature greater than 425 degrees C -- Test methods | 60.60 | 49.030.30 | TC 20/SC 4 |
| ISO/TR 8647:1990 Environmental degradation of textiles used in air cargo restraint equipment | 90.93 | 49.120 | TC 20/SC 9 |
| ISO 8668-1:1986 Aircraft -- Terminal junction systems -- Part 1: Characteristics | 90.93 | 49.060 | TC 20/SC 1 |
| ISO 8668-2:1986 Aircraft -- Terminal junction systems -- Part 2: Tests | 90.93 | 49.060 | TC 20/SC 1 |
| ISO 8668-3:1994 Aircraft -- Terminal junction systems -- Part 3: Detail specification for type 1 system | 90.20 | 49.060 | TC 20/SC 1 |
| ISO 8668-4:1993 Aircraft -- Terminal junction systems -- Part 4: Detail specification for type 2 system | 90.93 | 49.060 | TC 20/SC 1 |
| ISO 8668-5:1992 Aircraft -- Terminal junction systems -- Part 5: Detail specification for type 3 system | 90.93 | 49.060 | TC 20/SC 1 |
| ISO 8668-6:1994 Aircraft -- Terminal junction systems -- Part 6: Detail specification for type 4 system | 90.20 | 49.060 | TC 20/SC 1 |
| ISO 8775:1988 Aerospace -- Gaseous oxygen replenishment connection for use in fluid systems (new type) -- Dimensions (Inch series) | 90.60 | 49.100 49.080 | TC 20/SC 10 |
| ISO 8788:2000 Aerospace -- Nuts, metric -- Tolerances of form and position | 90.60 | 49.030.30 | TC 20/SC 4 |
| ISO 8815:1994 Aircraft -- Electrical cables and cable harnesses -- Vocabulary | 90.20 | 49.060 01.040.49 | TC 20/SC 1 |
| ISO 8816:1993 Aircraft -- Solid-state remote power controllers -- General requirements | 90.60 | 49.060 | TC 20/SC 1 |
| ISO 8829-1:2009 Aerospace -- Test methods for polytetrafluoroethylene (PTFE) inner-tube hose assemblies -- Part 1: Metallic (stainless steel) braid | 60.60 | 49.080 83.140.40 | TC 20/SC 10 |
| ISO 8829-2:2006 Aerospace -- Test methods for polytetrafluoroethylene (PTFE) inner-tube hose assemblies -- Part 2: Non-metallic braid | 90.20 | 49.080 83.140.40 | TC 20/SC 10 |
| ISO 8843:2005 Aircraft -- Crimp-removable contacts for electrical connectors -- Identification system | 90.60 | 49.060 01.070 | TC 20/SC 1 |
| ISO 8913:2006 Aerospace -- Lightweight polytetrafluoroethylene (PTFE) hose assemblies, classification 400 degrees F/3 000 psi (204 degrees C/20 684 kPa) and 204 degrees C/21 000 kPa (400 degrees F/3 046 psi) -- Procurement specification | 90.20 | 83.140.40 49.080 | TC 20/SC 10 |
| ISO 8940:2002 Aerospace -- Nuts, anchor, self-locking, sealing, floating, two-lug, with counterbore, with MJ threads, classifications: 900 MPa (at ambient temperature)/120 degrees C, 900 MPa (at ambient temperature)/175 degrees C and 900 MPa (at ambient temperature)/235 degrees C -- Dimensions | 90.60 | 49.030.30 | TC 20/SC 4 |
| ISO 9031:1987 Air cargo equipment -- Handling systems for unit load devices (ULDs) -- Symbols for pictorial representation | 90.93 | 01.080.20 49.120 | TC 20/SC 9 |
| ISO 9139:1998 Aerospace -- Nuts, plain or slotted (castellated) -- Procurement specification | 90.60 | 49.030.30 | TC 20/SC 4 |
| ISO 9140:1998 Aerospace -- Nuts, plain or slotted (castellated) -- Test methods | 90.60 | 49.030.30 | TC 20/SC 4 |
| ISO 9152:1998 Aerospace -- Bolts, with MJ threads, in titanium alloys, strength class 1 100 MPa -- Procurement specification | 90.60 | 49.030.20 | TC 20/SC 4 |
| ISO 9154:1999 Aerospace -- Bolts, with MJ threads, made of heat-resistant nickel-based alloy, strength class 1 550 MPa -- Procurement specification | 90.20 | 49.030.20 | TC 20/SC 4 |
| ISO 9156:1998 Aerospace -- Nuts, anchor, self-locking, fixed, 90 degrees corner, reduced series, with counterbore, with MJ threads, classifications: 1 100 MPa (at ambient temperature)/235 degrees C, 1 100 MPa (at ambient temperature)/315 degrees C and 1 100 MPa (at ambient temperature)/425 degrees C -- Dimensions | 90.60 | 49.030.30 | TC 20/SC 4 |
| ISO 9157:2002 Aerospace -- Nuts, spline-drive, self-locking, with MJ threads, classifications: 1 100 MPa (at ambient temperature)/425 degrees C, 1 100 MPa (at ambient temperature)/650 degrees C, 1 210 MPa (at ambient temperature)/425 degrees C, 1 210 MPa (at ambient temperature)/730 degrees C, 1 550 MPa (at ambient temperature)/235 degrees C, 1 550 MPa (at ambient temperature)/425 degrees C and 1 550 MPa (at ambient temperature)/600 degrees C -- Dimensions | 90.60 | 49.030.30 | TC 20/SC 4 |
| ISO 9199:1998 Aerospace -- Nuts, bihexagonal, self-locking, MJ threads, classifications: 1 100 MPa (at ambient temperature)/425 degrees C, 1 100 MPa (at ambient temperature)/650 degrees C, 1 210 MPa (at ambient temperature)/425 degrees C, 1 210 MPa (at ambient temperature)/730 degrees C, 1 550 MPa (at ambient temperature)/235 degrees C, 1 550 MPa (at ambient temperature)/425 degrees C and 1 550 MPa (at ambient temperature)/600 degrees C -- Dimensions | 90.60 | 49.030.30 | TC 20/SC 4 |
| ISO 9206:1990 Aerospace -- Constant displacement hydraulic motors -- General specifications | 90.60 | 49.080 | TC 20/SC 10 |
| ISO 9216:2002 Aerospace -- Nuts, hexagonal, slotted (castellated), for pulleys, in alloy steel and cadmium plated or in corrosion-resistant steel and passivated -- Dimensions and masses | 90.60 | 49.030.30 | TC 20 |
| ISO 9217:2002 Aerospace -- Washers, chamfered, with counterbore, for pulleys, in alloy steel and cadmium plated or in corrosion-resistant steel and passivated -- Dimensions and masses | 90.60 | 49.030.50 | TC 20 |
| ISO 9218:2002 Aerospace -- Washers, flat, for pulleys, in alloy steel and cadmium plated or in corrosion-resistant steel and passivated -- Dimensions and masses | 90.60 | 49.030.50 | TC 20 |
| ISO 9219:2002 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 | 90.60 | 49.030.20 | TC 20 |
| ISO 9254:1993 Aerospace -- Bolt, normal spline 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 | 90.20 | 49.030.20 | TC 20/SC 4 |
| ISO 9255:2008 Aerospace -- Bolts, normal spline head, normal shank, short or medium length MJ threads, metallic material, coated or uncoated, strength classes less than or equal to 1 100 MPa -- Dimensions | 60.60 | 49.030.20 | TC 20/SC 4 |
| ISO 9256:1993 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 | 90.20 | 49.030.20 | TC 20/SC 4 |
| ISO 9418:1998 Aerospace -- Rivets, solid, in aluminium or aluminium alloys -- Procurement specification | 90.60 | 49.030.60 | TC 20/SC 4 |
| ISO 9469:1991 Air cargo equipment -- Unit load devices for transportation of horses | 90.93 | 55.180.30 | TC 20/SC 9 |
| ISO 9528:1994 Aerospace -- Standard-weight polytetrafluoroethylene (PTFE) hose assemblies, classification 204 degrees C/21 000 kPa -- Procurement specification | 90.20 | 83.140.40 49.080 | TC 20/SC 10 |
| ISO 9538:1996 Aerospace -- Hydraulic tubing joints and fittings -- Planar flexure test | 90.60 | 49.080 | TC 20/SC 10 |
| ISO 9609:1996 Aerospace -- Nuts, hexagonal, plain, reduced height, normal across flats, with MJ threads, classifications: 450 MPa (at ambient temperature) /120 degrees C, 450 MPa (at ambient temperature) /235 degrees C, 600 MPa (at ambient temperature) /425 degrees C, 900 MPa (at ambient temperature) /235 degrees C, 900 MPa (at ambient temperature) /315 degrees C, 900 MPa (at ambient temperature) /650 degrees C, 1 100 MPa (at ambient temperature) /235 degrees C, 1 100 MPa (at ambient temperature) /730 degrees C and 1 250 MPa (at ambient temperature)/600 degrees C -- Dimensions | 90.60 | 49.030.30 | TC 20/SC 4 |
| ISO 9618:1996 Aerospace -- Nuts, hexagonal, slotted (castellated), reduced height, normal across flats, with MJ threads, classifications: 450 MPa (at ambient temperature)/120 degrees C, 450 MPa (at ambient temperature)/235 degrees C, 600 MPa (at ambient temperature)/425 degrees C, 900 MPa (at ambient temperature)/235 degrees C, 900 MPa (at ambient temperature)/315 degrees C, 900 MPa (at ambient temperature)/650 degrees C, 1 100 MPa (at ambient temperature)/235 degrees C, 1 100 MPa (at ambient temperature)/730 degrees C and 1 250 MPa (at ambient temperature)/600 degrees C -- Dimensions | 90.60 | 49.030.30 | TC 20/SC 4 |
| ISO 9634:1994 Aerospace -- Fluid systems -- Dimensions of plastic protective caps and plugs | 90.20 | 49.080 | TC 20/SC 10 |
| ISO 9662:1994 Aircraft equipment -- Environmental and operating conditions for airborne equipment -- Humidity, temperature and pressure tests | 90.20 | 49.020 | TC 20 |
| ISO 9666:1993 Aircraft -- Self-propelled lavatory-servicing vehicle -- Functional requirements | 90.93 | 43.160 49.100 | TC 20/SC 9 |
| ISO 9667:1998 Aircraft ground support equipment -- Tow bars | 90.93 | 49.100 | TC 20/SC 9 |
| ISO 9678:1991 Aircraft -- Self-propelled potable-water vehicle | 90.93 | 49.100 | TC 20/SC 9 |
| ISO 9679:2006 Aerospace -- Clamps for fluid systems -- Test methods | 90.20 | 49.080 | TC 20/SC 10 |
| ISO 9736:2000 Aerospace -- Eye-ends, in steel, threaded, for aircraft control wire rope -- Dimensions and loads | 90.60 | 49.035 | TC 20 |
| ISO 9737:2000 Aerospace -- Eye-ends, in corrosion-resistant steel, swaged on aircraft control wire rope -- Dimensions and loads | 90.60 | 49.035 | TC 20 |
| ISO 9738:2000 Aerospace -- Turnbarrels, for aircraft control wire rope -- Dimensions and loads | 90.60 | 49.035 | TC 20 |
| ISO 9747:2000 Aerospace -- Double-shank ball-ends, in corrosion-resistiant steel, swaged on aircraft control wire rope -- Dimensions and loads | 90.60 | 49.035 | TC 20 |
| ISO 9748:2000 Aerospace -- Ball-ends, in corrosion-resistant steel, swaged on aircraft control wire rope -- Dimensions and loads | 90.60 | 49.035 | TC 20 |
| ISO 9749:2000 Aerospace -- Stud-ends, in corrosion-resistant steel, swaged on aircraft control wire rope -- Dimensions and loads | 90.60 | 49.035 | TC 20 |
| ISO 9757:2000 Aerospace -- Fork-ends, in steel, threaded, for aircraft control wire rope turnbarrels -- Dimensions and loads | 90.60 | 49.035 | TC 20 |
| ISO 9758:2000 Aerospace -- Fork-ends, in steel, threaded, for rolling bearings, for aircraft control wire rope -- Dimensions and loads | 90.60 | 49.035 | TC 20 |
| ISO 9759:2000 Aerospace -- Fork-ends, in corrosion-resistiant steel, swaged on aircraft control wire rope -- Dimensions and loads | 90.60 | 49.035 | TC 20 |
| ISO 9760:2000 Aerospace -- Fork-ends, in corrosion-resistant steel, swaged on aircraft control wire rope for rolling bearings -- Dimensions and loads | 90.60 | 49.035 | TC 20 |
| ISO 9761:2000 Aerospace -- Locking clips, in corrosion-resistant steel, for aircraft control wire rope turnbuckles -- Dimensions | 90.60 | 49.035 | TC 20 |
| ISO 9762:2000 Aerospace -- Aircraft control wire rope assemblies -- Dimensions and end-fitting combinations | 90.60 | 49.035 | TC 20 |
| ISO 9763:1999 Aerospace -- Aircraft control wire rope assemblies -- Technical specification | 90.20 | 49.035 | TC 20 |
| ISO 9788:1990 Air cargo equipment -- Cast components of double stud fitting assembly with a load capacity of 22 250 N (5 000 lbf), for aircraft cargo restraint | 90.60 | 49.120 | TC 20/SC 9 |
| ISO 9938:1994 Aerospace -- Polytetrafluoroethylene (PTFE) hose assemblies, classification 204 degrees C/28 000 kPa -- Procurement specification | 90.20 | 83.140.40 49.080 | TC 20/SC 10 |
| ISO 9939:1994 Aerospace -- Pressure re-oiling connection (new type) | 90.20 | 49.080 49.100 | TC 20/SC 10 |
| ISO 10046:1996 Aircraft -- Methodology of calculating cargo compartment volumes | 90.93 | 49.045 | TC 20/SC 9 |
| ISO 10096:1997 Aerospace -- Nuts, hexagonal, slotted (castellated), reduced height, reduced across flats, with MJ threads, classifications: 450 MPa (at ambient temperature)/425 degrees C, 600 MPa (at ambient temperature)/235 degrees C, 600 MPa (at ambient temperature)/315 degrees C, 600 MPa (at ambient temperature)/650 degrees C, 900 MPa (at ambient temperature)/235 degrees C, 900 MPa (at ambient temperature)/730 degrees C and 1 100 MPa (at ambient temperature)/600 degrees C -- Dimensions | 90.60 | 49.030.30 | TC 20/SC 4 |
| ISO/TR 10201:2001 Aerospace -- Standards for electronic instruments and systems | 60.60 | 49.090 | TC 20 |
| ISO 10254:1995 Air cargo and ground equipment -- Vocabulary | 90.92 | 01.040.49 49.100 49.120 | TC 20/SC 9 |
| ISO 10296:1992 Aircraft -- Hybrid remote power controllers -- General requirements | 90.93 | 49.060 | TC 20/SC 1 |
| ISO 10299:2000 Aerospace -- Rivets, solid -- Material and metric series identification | 90.60 | 49.030.60 | TC 20/SC 4 |
| ISO 10327:1995 Aircraft -- Certified aircraft container for air cargo -- Specification and testing | 90.92 | 55.180.30 | TC 20/SC 9 |
| ISO 10502:1992 Aerospace -- Hose assemblies in polytetrafluoroethylene (PTFE) for use up to 232 degrees C and 10 500 kPa -- Procurement specification | 90.92 | 83.140.40 49.080 | TC 20/SC 10 |
| ISO 10583:1993 Aerospace fluid systems -- Test methods for tube/fitting assemblies | 90.60 | 49.080 | TC 20/SC 10 |
| ISO 10792-1:1995 Aerospace -- Airframe spherical plain bearings in corrosion-resisting steel with self-lubricating liner -- Part 1: Metric series | 90.60 | 49.035 | TC 20/SC 15 |
| ISO 10792-2:1995 Aerospace -- Airframe spherical plain bearings in corrosion-resisting steel with self-lubricating liner -- Part 2: Inch series | 90.60 | 49.035 | TC 20/SC 15 |
| ISO 10792-3:1995 Aerospace -- Airframe spherical plain bearings in corrosion-resisting steel with self-lubricating liner -- Part 3: Technical specification | 90.60 | 49.035 | TC 20/SC 15 |
| ISO 10841:1996 Aircraft -- Catering vehicle for large capacity aircraft -- Functional requirements | 90.60 | 49.100 | TC 20/SC 9 |
| ISO 10842:2006 Aircraft -- Ground service connections -- Locations and types | 90.20 | 49.100 | TC 20/SC 9 |
| ISO 10955:1999 Aerospace -- End-fittings and turnbarrels for aircraft control wire rope -- Technical specification | 90.20 | 49.035 | TC 20 |
| ISO 10959:2000 Aerospace -- MJ threads -- Gauging | 90.60 | 49.030.10 | TC 20/SC 4 |
| ISO 11075:2007 Aircraft -- De-icing/anti-icing fluids -- ISO type I | 60.60 | 49.100 | TC 20/SC 9 |
| ISO 11076:2006 Aircraft -- Ground-based de-icing/anti-icing methods with fluids | 90.92 | 49.100 | TC 20/SC 9 |
| ISO 11077:1993 Aerospace -- Self-propelled de-icing/anti-icing vehicles -- Functional requirements | 90.60 | 49.100 | TC 20/SC 9 |
| ISO 11078:2007 Aircraft -- De-icing/anti-icing fluids -- ISO types II, III and IV | 60.60 | 49.100 | TC 20/SC 9 |
| ISO 11104:2003 Space data and information transfer systems -- Time code formats | 90.60 | 49.140 | TC 20/SC 13 |
| ISO 11217:1993 Aerospace -- Hydraulic system fluid contamination -- Location of sampling points and criteria for sampling | 90.92 | 49.080 49.100 | TC 20/SC 10 |
| ISO 11218:1993 Aerospace -- Cleanliness classification for hydraulic fluids | 90.92 | 49.080 | TC 20/SC 10 |
| ISO 11241:1994 Aircraft -- Aircraft engine transport devices | 90.93 | 49.100 | TC 20/SC 9 |
| ISO 11242:1996 Aircraft -- Pressure equalization requirements for cargo containers | 90.93 | 55.180.30 | TC 20/SC 9 |
| ISO 11995:1996 Aircraft -- Stability requirements for loading and servicing equipment | 90.60 | 49.100 49.120 | TC 20/SC 9 |
| ISO 12056:1996 Aircraft -- Self-propelled passenger stairs for large capacity aircraft -- Functional requirements | 90.60 | 49.100 | TC 20/SC 9 |
| ISO 12118:1995 Air cargo equipment -- Identification of double-stud tie-down fittings having an omnidirectional rated load capacity of 22 250 N (5 000 lbf) or above | 90.93 | 49.120 | TC 20/SC 9 |
| ISO 12175:1994 Space data and information transfer systems -- Standard formatted data units -- Structure and construction rules | 90.20 | 49.140 | TC 20/SC 13 |
| ISO/TR 12198:1998 Aerospace -- Rivets, solid -- Materials | 60.60 | 49.030.60 | TC 20/SC 4 |
| ISO 12256:2002 Aerospace -- Drives, internal, cruciform, ribbed -- Metric series | 90.60 | 49.030.20 | TC 20/SC 4 |
| ISO 12256:2002/Cor 1:2009 | 60.60 | 49.030.20 | TC 20/SC 4 |
| ISO 12257:2008 Aerospace -- Internal six-lobe drives -- Metric series | 60.60 | 49.030.20 | TC 20/SC 4 |
| ISO 12258:1998 Aerospace -- Bolts, reduced bihexagonal head, normal or pitch diameter shank, long length MJ threads, metallic material, coated or uncoated, strength classes less than or equal to 1 275 MPa -- Dimensions | 90.60 | 49.030.30 | TC 20/SC 4 |
| ISO 12260:1996 Aerospace -- Screws, pan head, internal offset cruciform ribbed or unribbed drive, stepped shank, short or medium length MJ threads, metallic material, coated or uncoated, strength classes less than or equal to 1 100 MPa -- Dimensions | 90.60 | 49.030.20 | TC 20/SC 4 |
| ISO 12261:1996 Aerospace -- Screws, pan head, internal offset cruciform ribbed or unribbed drive, pitch diameter shank, long length MJ threads, metallic material, coated or uncoated, strength classes less than or equal to 1 100 MPa -- Dimensions | 90.60 | 49.030.20 | TC 20/SC 4 |
| ISO 12268:1997 Aerospace -- Nuts, hexagonal, plain, reduced height, reduced across flats, with MJ threads, classifications: 450 MPa (at ambient temperature)/425 degrees C, 600 MPa (at ambient temperature)/235 degrees C, 600 MPa (at ambient temperature)/315 degrees C, 600 MPa (at ambient temperature)/650 degrees C, 900 MPa (at ambient temperature)/235 degrees C, 900 MPa (at ambient temperature)/730 degrees C and 1 100 MPa (at ambient temperature)/600 degrees C -- Dimensions | 90.60 | 49.030.30 | TC 20/SC 4 |
| ISO 12272:1998 Aerospace -- Nuts, anchor, self-locking, floating, two lug, with incremental counterbore, with MJ threads classifications: 900 MPa (at ambient temperature)/235 degrees C, 900 MPa (at ambient temperature)/315 degrees C and 900 MPa (at ambient temperature)/425 degrees C -- Dimensions | 90.60 | 49.030.30 | TC 20/SC 4 |
| ISO 12273:1997 Aerospace -- Nuts, anchor, self-locking, floating, self-aligning, two lug, with MJ threads, classifications: 900 MPa (at ambient temperature)/235 degrees C, 900 MPa (at ambient temperature)/315 degrees C and 900 MPa (at ambient temperature)/425 degrees C -- Dimensions | 90.60 | 49.030.30 | TC 20/SC 4 |
| ISO 12274:1997 Aerospace -- Nuts, anchor, self-locking, floating, self-aligning, single lug, with MJ threads, classifications: 900 MPa (at ambient temperature)/235 degrees C, 900 MPa (at ambient temperature)/315 degrees C and 900 MPa (at ambient temperature)/425 degrees C -- Dimensions | 90.60 | 49.030.30 | TC 20/SC 4 |
| ISO 12277:2000 Aerospace -- Gang channel, self-locking, floating, standard series, with counterbore, classifications: 1 100 MPa (at ambient temperature) / 120 degrees C, 1 100 MPa (at ambient temperature) / 235 degrees C and 1 100 MPa (at ambient temperature) / 425 degrees C -- Dimensions | 90.60 | 49.030.30 | TC 20/SC 4 |
| ISO 12278:1999 Aerospace -- Nuts, barrel, self-locking, floating, self-aligning, with MJ threads, classifications: 900 MPa (at ambient temperature) / 235 degrees C, 1100 MPa (at ambient temperature) / 235 degrees C, 1250 MPa (at ambient temperature) / 235 degrees C and 1550 MPa (at ambient temperature) / 235 degrees C -- Dimensions | 90.20 | 49.030.30 | TC 20/SC 4 |
| ISO 12280:1999 Aerospace -- Retainers, spring, sheet metal, for self-locking barrel nuts -- Dimensions | 90.20 | 49.030.99 | TC 20/SC 4 |
| ISO 12281:1999 Aerospace -- Rivets, solid, 100 degrees normal countersunk head, in metallic material, with or without surface treatment -- Dimensions | 90.20 | 49.030.60 | TC 20/SC 4 |
| ISO 12288:2000 Aerospace -- Rivets, solid, in nickel alloy -- Procurement specification | 90.60 | 49.030.60 | TC 20/SC 4 |
| ISO 12289:2003 Aerospace -- Rivets, solid, in corrosion-resisting steel -- Procurement specification | 90.60 | 49.030.60 | TC 20/SC 4 |
| ISO 12290:2000 Aerospace -- Rivets, solid, in titanium or titanium alloy -- Procurement specification | 90.60 | 49.030.60 | TC 20/SC 4 |
| ISO 12319:2006 Aerospace -- 'P' (loop style) clamps -- Procurement specification | 90.20 | 49.030.99 | TC 20/SC 10 |
| ISO 12333:2000 Aerospace -- Constant displacement hydraulic motors -- General specifications for 35 000 kPa systems | 90.60 | 49.080 | TC 20/SC 10 |
| ISO 12334:2000 Aerospace -- Hydraulic, pressure-compensated, variable delivery pumps -- General requirement for 35 000 kPa systems | 90.60 | 49.080 | TC 20/SC 10 |
| ISO 13411:1997 Aerospace -- Airframe needle roller, cylindrical roller and track roller bearings -- Technical specification | 90.60 | 49.035 | TC 20/SC 15 |
| ISO 13412:1997 Aerospace -- Airframe needle track roller, yoke type, single-row, sealed -- Inch series | 90.60 | 49.035 | TC 20/SC 15 |
| ISO 13413:1997 Aerospace -- Airframe needle track roller, yoke type, double-row, sealed -- Inch series | 90.60 | 49.035 | TC 20/SC 15 |
| ISO 13414:1997 Aerospace -- Airframe needle roller bearings, single-row, shielded -- Inch series | 90.60 | 49.035 | TC 20/SC 15 |
| ISO 13415:1997 Aerospace -- Airframe needle track roller, stud type, single-row, sealed -- Inch series | 90.60 | 49.035 | TC 20/SC 15 |
| ISO 13416:1997 Aerospace -- Airframe needle track roller, yoke type, single-row, sealed -- Metric series | 90.60 | 49.035 | TC 20/SC 15 |
| ISO 13417:1997 Aerospace -- Airframe needle track roller, stud type, single-row, sealed -- Metric series | 90.60 | 49.035 | TC 20/SC 15 |
| ISO 13589:1998 Aerospace -- Nuts, bihexagonal, self-locking, with counterbore and MJ threads, classifications: 1 100 MPa (at ambient temperature)/425 degrees C, 1 100 MPa (at ambient temperature)/650 degrees C, 1 210 MPa (at ambient temperature)/425 degrees C, 1 210 MPa (at ambient temperature)/730 degrees C, 1 550 MPa (at ambient temperature)/235 degrees C, 1 550 MPa (at ambient temperature)/425 degrees C and 1 550 MPa (at ambient temperature)/600 degrees C -- Dimensions | 90.60 | 49.030.30 | TC 20/SC 4 |
| ISO 13595:2000 Aerospace -- Inserts, with self-locking floating nut, with MJ threads, in metallic material, coated or uncoated -- Dimensions | 90.60 | 49.030.99 | TC 20/SC 4 |
| ISO 13596:2000 Aerospace -- Inserts, self-locking, with MJ threads, closed type, in metallic material, coated or uncoated -- Dimensions | 90.60 | 49.030.99 | TC 20/SC 4 |
| ISO 13597:2000 Aerospace -- Inserts, self-locking, with MJ threads, open type, in metallic material, coated or uncoated -- Dimensions | 90.60 | 49.030.99 | TC 20/SC 4 |
| ISO 13598:2000 Aerospace -- Inserts, self-locking, with MJ threads, reduced flanges, closed type, in metallic material, coated or uncoated -- Dimensions | 90.60 | 49.030.99 | TC 20/SC 4 |
| ISO 13599:2000 Aerospace -- Inserts, with clearance hole, in metallic material, coated or uncoated -- Dimensions | 90.60 | 49.030.99 | TC 20/SC 4 |
| ISO 13764:1996 Space data and information transfer systems -- Standard formatted data units -- Control authority procedures | 90.20 | 49.140 | TC 20/SC 13 |
| ISO 13921:2008 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 | 60.60 | 49.030.20 | TC 20/SC 4 |
| ISO 14190:1998 Aerospace -- Airframe rolling bearings: ball and spherical roller bearings -- Technical specification | 90.60 | 49.035 | TC 20/SC 15 |
| ISO 14191:1998 Aerospace -- Airframe spherical roller bearings, single row, self-aligning, diameter series 3 and 4 -- Metric series | 90.60 | 49.035 | TC 20/SC 15 |
| ISO 14192:1998 Aerospace -- Airframe spherical roller bearings, single row, self-aligning, shielded, intermediate duty -- Metric series | 90.60 | 49.035 | TC 20/SC 15 |
| ISO 14193:1998 Aerospace -- Airframe spherical roller bearings, single row, self-aligning, sealed, extended inner ring intermediate duty -- Inch series | 90.60 | 49.035 | TC 20/SC 15 |
| ISO 14194:1998 Aerospace -- Airframe spherical roller bearings, double row, self-aligning, sealed, extended inner ring, heavy duty -- Inch series | 90.60 | 49.035 | TC 20/SC 15 |
| ISO 14195:1998 Aerospace -- Airframe spherical roller bearings, double row, self-aligning, sealed, torque tube design, light duty -- Inch series | 90.60 | 49.035 | TC 20/SC 15 |
| ISO 14196:1998 Aerospace -- Airframe spherical roller bearings, double row, self-aligning, sealed, plain inner ring, heavy duty -- Inch series | 90.60 | 49.035 | TC 20/SC 15 |
| ISO 14197:1998 Aerospace -- Airframe spherical roller bearings, single row, self-aligning, sealed, intermediate duty -- Inch series | 90.60 | 49.035 | TC 20/SC 15 |
| ISO 14201:1998 Aerospace -- Airframe ball bearings, double-row, self-aligning, diameter series 2 -- Metric series | 90.60 | 49.035 | TC 20/SC 15 |
| ISO 14202:1998 Aerospace -- Airframe ball bearings, single-row, rigid, diameter series 0 and 2 -- Metric series | 90.60 | 49.035 | TC 20/SC 15 |
| ISO 14203:1998 Aerospace -- Airframe ball bearings, single-row, rigid, diameter series 8 and 9 -- Metric series | 90.60 | 49.035 | TC 20/SC 15 |
| ISO 14204:1998 Aerospace -- Airframe ball bearings, double-row, rigid, diameter series 0 -- Metric series | 90.60 | 49.035 | TC 20/SC 15 |
| ISO 14206:1998 Aerospace -- Airframe ball bearings, single-row, rigid, sealed, light duty -- Inch series | 90.60 | 49.035 | TC 20/SC 15 |
| ISO 14207:1998 Aerospace -- Airframe ball bearings, single-row, rigid, precision, sealed, light duty -- Inch series | 90.60 | 49.035 | TC 20/SC 15 |
| ISO 14208:1998 Aerospace -- Airframe ball bearings, single-row, rigid, sealed, intermediate duty -- Inch series | 90.60 | 49.035 | TC 20/SC 15 |
| ISO 14209:1998 Aerospace -- Airframe ball bearings, single-row, rigid, precision, sealed, intermediate duty -- Inch series | 90.60 | 49.035 | TC 20/SC 15 |
| ISO 14210:1998 Aerospace -- Airframe ball bearings, single-row, rigid, sealed, torque tube design, light duty -- Inch series | 90.60 | 49.035 | TC 20/SC 15 |
| ISO 14211:1998 Aerospace -- Airframe ball bearings, single-row, rigid, precision, sealed, torque tube design, light duty -- Inch series | 90.60 | 49.035 | TC 20/SC 15 |
| ISO 14212:1998 Aerospace -- Airframe ball bearings, single-row, rigid, sealed, torque tube design, extra-light duty -- Inch series | 90.60 | 49.035 | TC 20/SC 15 |
| ISO 14213:1998 Aerospace -- Airframe ball bearings, single-row, rigid, precision, sealed, torque tube design, extra-light duty -- Inch series | 90.60 | 49.035 | TC 20/SC 15 |
| ISO 14214:1998 Aerospace -- Airframe ball bearings, double-row, rigid, sealed, heavy duty -- Inch series | 90.60 | 49.035 | TC 20/SC 15 |
| ISO 14215:1998 Aerospace -- Airframe ball bearings, double-row, rigid, precision, sealed, heavy duty -- Inch series | 90.60 | 49.035 | TC 20/SC 15 |
| ISO 14216:1998 Aerospace -- Airframe ball bearings, double-row, self-aligning, sealed, heavy duty -- Inch series | 90.60 | 49.035 | TC 20/SC 15 |
| ISO 14217:1998 Aerospace -- Airframe ball bearings, double-row, self-aligning, precision, sealed, heavy duty -- Inch series | 90.60 | 49.035 | TC 20/SC 15 |
| ISO 14218:1998 Aerospace -- Airframe ball bearings, single-row, self-aligning, sealed, heavy duty -- Inch series | 90.60 | 49.035 | TC 20/SC 15 |
| ISO 14219:1998 Aerospace -- Airframe ball bearings, single-row, self-aligning, precision, sealed, heavy duty -- Inch series | 90.60 | 49.035 | TC 20/SC 15 |
| ISO 14220:1998 Aerospace -- Airframe ball bearings, single-row, self-aligning, sealed, light duty -- Inch series | 90.60 | 49.035 | TC 20/SC 15 |
| ISO 14221:1998 Aerospace -- Airframe ball bearings, single-row, self-aligning, precision, sealed, light duty -- Inch series | 90.60 | 49.035 | TC 20/SC 15 |
| ISO 14275:2002 Aerospace -- Drives, internal, offset cruciform, ribbed -- Metric series | 90.60 | 49.030.20 | TC 20/SC 4 |
| ISO 14276:2002 Aerospace -- Drives, internal, offset cruciform -- Metric series | 90.60 | 49.030.20 | TC 20/SC 4 |
| ISO 14277:2002 Aerospace -- Drivers, ribbed, for internal offset cruciform ribbed or unribbed drives -- Metric series | 90.60 | 49.030.20 | TC 20/SC 4 |
| ISO 14278:2002 Aerospace -- Gauges, for internal offset cruciform ribbed or unribbed drives -- Metric series | 90.60 | 49.030.20 | TC 20/SC 4 |
| ISO 14279:2002 Aerospace -- Drives, internal, cruciform -- Metric series | 90.60 | 49.030.20 | TC 20/SC 4 |
| ISO 14280:2002 Aerospace -- Drivers, ribbed, for internal cruciform ribbed or unribbed drives -- Metric series | 90.60 | 49.030.20 | TC 20/SC 4 |
| ISO 14281:2002 Aerospace -- Gauges, for internal cruciform ribbed or unribbed drives -- Metric series | 90.60 | 49.030.20 | TC 20/SC 4 |
| ISO 14300-1:2001 Space systems -- Programme management -- Part 1: Structuring of a programme | 90.92 | 49.140 | TC 20/SC 14 |
| ISO 14300-2:2002 Space systems -- Programme management -- Part 2: Product assurance | 90.92 | 49.140 | TC 20/SC 14 |
| ISO 14302:2002 Space systems -- Electromagnetic compatibility requirements | 90.93 | 33.100.01 49.140 | TC 20/SC 14 |
| ISO 14303:2002 Space systems -- Launch-vehicle-to-spacecraft interfaces | 90.93 | 49.140 | TC 20/SC 14 |
| ISO/TR 14618:1996 Middle atmosphere -- Global model at altitudes between 30 km and 120 km, and wind model at altitudes above 30 km | 60.60 | 07.040 49.020 | TC 20/SC 6 |
| ISO 14619:2003 Space systems -- Space experiments -- General requirements | 90.60 | 49.140 | TC 20/SC 14 |
| ISO 14620-1:2002 Space systems -- Safety requirements -- Part 1: System safety | 90.93 | 49.140 | TC 20/SC 14 |
| ISO 14620-2:2000 Space systems -- Safety requirements -- Part 2: Launch site operations | 90.92 | 49.140 | TC 20/SC 14 |
| ISO 14620-3:2005 Space systems -- Safety requirements -- Part 3: Flight safety systems | 90.60 | 49.140 | TC 20/SC 14 |
| ISO 14621-1:2003 Space systems -- Electrical, electronic and electromechanical (EEE) parts -- Part 1: Parts management | 90.60 | 49.140 | TC 20/SC 14 |
| ISO 14621-2:2003 Space systems -- Electrical, electronic and electromechanical (EEE) parts -- Part 2: Control programme requirements | 90.93 | 49.140 | TC 20/SC 14 |
| ISO 14622:2000 Space systems -- Structural design -- Loads and induced environment | 90.60 | 49.140 | TC 20/SC 14 |
| ISO 14623:2003 Space systems - Pressure vessels and pressurized structures -- Design and operation | 90.60 | 49.140 | TC 20/SC 14 |
| ISO 14624-1:2003 Space systems -- Safety and compatibility of materials -- Part 1: Determination of upward flammability of materials | 90.93 | 13.220.40 49.025.01 49.140 | TC 20/SC 14 |
| ISO 14624-2:2003 Space systems -- Safety and compatibility of materials -- Part 2: Determination of flammability of electrical-wire insulation and accessory materials | 90.93 | 13.220.40 49.025.01 49.140 | TC 20/SC 14 |
| ISO 14624-3:2005 Space systems -- Safety and compatibility of materials -- Part 3: Determination of offgassed products from materials and assembled articles | 90.93 | 49.140 49.025.01 | TC 20/SC 14 |
| ISO 14624-4:2003 Space systems -- Safety and compatibility of materials -- Part 4: Determination of upward flammability of materials in pressurized gaseous oxygen or oxygen-enriched environments | 90.93 | 13.220.40 49.025.01 49.140 | TC 20/SC 14 |
| ISO 14624-5:2006 Space systems -- Safety and compatibility of materials -- Part 5: Determination of reactivity of system/component materials with aerospace propellants | 90.60 | 49.140 49.025.01 | TC 20/SC 14 |
| ISO 14624-6:2006 Space systems -- Safety and compatibility of materials -- Part 6: Determination of reactivity of processing materials with aerospace fluids | 90.60 | 49.025.01 49.140 | TC 20/SC 14 |
| ISO 14624-7:2006 Space systems -- Safety and compatibility of materials -- Part 7: Determination of permeability and penetration of materials to aerospace fluids | 90.60 | 49.140 49.025.01 | TC 20/SC 14 |
| ISO 14625:2007 Space systems -- Ground support equipment for use at launch, landing or retrieval sites -- General requirements | 60.60 | 49.100 49.140 | TC 20/SC 14 |
| ISO 14711:2003 Space systems -- Unmanned mission operations concepts -- Guidelines for defining and assessing concept products | 90.93 | 49.140 | TC 20/SC 14 |
| ISO 14721:2003 Space data and information transfer systems -- Open archival information system -- Reference model | 90.60 | 49.140 | TC 20/SC 13 |
| ISO 14950:2004 Space systems -- Unmanned spacecraft operability | 90.93 | 49.140 | TC 20/SC 14 |
| ISO 14951-1:1999 Space systems -- Fluid characteristics -- Part 1: Oxygen | 95.20 | 49.140 | TC 20/SC 14 |
| ISO 14951-2:1999 Space systems -- Fluid characteristics -- Part 2: Hydrogen propellant | 95.20 | 71.100.20 49.140 | TC 20/SC 14 |
| ISO 14951-3:1999 Space systems -- Fluid characteristics -- Part 3: Nitrogen | 95.20 | 49.140 | TC 20/SC 14 |
| ISO 14951-3:1999/Cor 1:2000 | 60.60 | 49.140 | TC 20/SC 14 |
| ISO 14951-4:1999 Space systems -- Fluid characteristics -- Part 4: Helium | 95.20 | 49.140 | TC 20/SC 14 |
| ISO 14951-4:1999/Cor 1:2000 | 60.60 | 49.140 | TC 20/SC 14 |
| ISO 14951-5:1999 Space systems -- Fluid characteristics -- Part 5: Nitrogen tetroxide propellant | 95.20 | 49.140 | TC 20/SC 14 |
| ISO 14951-5:1999/Cor 1:2004 | 60.60 | 49.140 | TC 20/SC 14 |
| ISO 14951-6:1999 Space systems -- Fluid characteristics -- Part 6: Monomethylhydrazine propellant | 95.20 | 49.140 | TC 20/SC 14 |
| ISO 14951-6:1999/Cor 1:2004 | 60.60 | 49.140 | TC 20/SC 14 |
| ISO 14951-7:1999 Space systems -- Fluid characteristics -- Part 7: Hydrazine propellant | 95.20 | 49.140 | TC 20/SC 14 |
| ISO 14951-7:1999/Cor 1:2004 | 60.60 | 49.140 | TC 20/SC 14 |
| ISO 14951-8:1999 Space systems -- Fluid characteristics -- Part 8: Kerosene propellant | 95.20 | 49.140 | TC 20/SC 14 |
| ISO 14951-9:1999 Space systems -- Fluid characteristics -- Part 9: Argon | 95.20 | 49.140 | TC 20/SC 14 |
| ISO 14951-9:1999/Cor 1:2000 | 60.60 | 49.140 | TC 20/SC 14 |
| ISO 14951-10:1999 Space systems -- Fluid characteristics -- Part 10: Water | 95.20 | 49.140 | TC 20/SC 14 |
| ISO 14951-11:1999 Space systems -- Fluid characteristics -- Part 11: Ammonia | 95.20 | 49.140 | TC 20/SC 14 |
| ISO 14951-12:1999 Space systems -- Fluid characteristics -- Part 12: Carbon dioxide | 95.20 | 49.140 | TC 20/SC 14 |
| ISO 14951-13:1999 Space systems -- Fluid characteristics -- Part 13: Breathing air | 95.20 | 49.140 | TC 20/SC 14 |
| ISO 14952-1:2003 Space systems -- Surface cleanliness of fluid systems -- Part 1: Vocabulary | 90.60 | 49.140 49.080 | TC 20/SC 14 |
| ISO 14952-2:2003 Space systems -- Surface cleanliness of fluid systems -- Part 2: Cleanliness levels | 90.60 | 49.140 49.080 | TC 20/SC 14 |
| ISO 14952-3:2003 Space systems -- Surface cleanliness of fluid systems -- Part 3: Analytical procedures for the determination of nonvolatile residues and particulate contamination | 90.60 | 49.140 49.080 | TC 20/SC 14 |
| ISO 14952-4:2003 Space systems -- Surface cleanliness of fluid systems -- Part 4: Rough-cleaning processes | 90.60 | 49.140 49.080 | TC 20/SC 14 |
| ISO 14952-5:2003 Space systems -- Surface cleanliness of fluid systems -- Part 5: Drying processes | 90.60 | 49.140 49.080 | TC 20/SC 14 |
| ISO 14952-6:2003 Space systems -- Surface cleanliness of fluid systems -- Part 6: Precision-cleaning processes | 90.60 | 49.140 49.080 | TC 20/SC 14 |
| ISO 14953:2000 Space systems -- Structural design -- Determination of loading levels for static qualification testing of launch vehicles | 90.60 | 49.140 | TC 20/SC 14 |
| ISO 14954:2005 Space systems -- Dynamic and static analysis -- Exchange of mathematical models | 90.93 | 49.140 | TC 20/SC 14 |
| ISO 14961:2002 Space data and information transfer systems -- Parameter value language specification | 90.60 | 49.140 | TC 20/SC 13 |
| ISO 14962:1997 Space data and information transfer systems -- ASCII encoded English | 90.20 | 49.140 | TC 20/SC 13 |
| ISO 15387:2005 Space systems -- Single-junction solar cells -- Measurements and calibration procedures | 90.93 | 27.160 49.140 | TC 20/SC 14 |
| ISO 15388:2004 Space systems -- Contamination and cleanliness control | 90.60 | 49.140 | TC 20/SC 14 |
| ISO 15389:2001 Space systems -- Flight-to-ground umbilicals | 90.93 | 49.140 | TC 20/SC 14 |
| ISO 15389:2001/Cor 1:2006 | 60.60 | 49.140 | TC 20/SC 14 |
| ISO 15389:2001/Amd 1:2005 Prevention of accidental cross-connection | 60.60 | 49.140 | TC 20/SC 14 |
| ISO 15390:2004 Space environment (natural and artificial) -- Galactic cosmic ray model | 90.60 | 49.140 | TC 20/SC 14 |
| ISO 15395:1998 Space data and information transfer systems -- Standard formatted data units -- Control authority data structures | 90.60 | 49.140 | TC 20/SC 13 |
| ISO 15396:2007 Space data and information transfer systems -- Cross support reference model -- Space link extension services | 60.60 | 49.140 | TC 20/SC 13 |
| ISO 15859-1:2004 Space systems -- Fluid characteristics, sampling and test methods -- Part 1: Oxygen | 90.60 | 49.140 | TC 20/SC 14 |
| ISO 15859-2:2004 Space systems -- Fluid characteristics, sampling and test methods -- Part 2: Hydrogen | 90.60 | 49.140 | TC 20/SC 14 |
| ISO 15859-3:2004 Space systems -- Fluid characteristics, sampling and test methods -- Part 3: Nitrogen | 90.60 | 49.140 | TC 20/SC 14 |
| ISO 15859-4:2004 Space systems -- Fluid characteristics, sampling and test methods -- Part 4: Helium | 90.60 | 49.140 | TC 20/SC 14 |
| ISO 15859-5:2004 Space systems -- Fluid characteristics, sampling and test methods -- Part 5: Nitrogen tetroxide propellants | 90.60 | 49.140 | TC 20/SC 14 |
| ISO 15859-6:2004 Space systems -- Fluid characteristics, sampling and test methods -- Part 6: Monomethylhydrazine propellant | 90.60 | 49.140 | TC 20/SC 14 |
| ISO 15859-7:2004 Space systems -- Fluid characteristics, sampling and test methods -- Part 7: Hydrazine propellant | 90.60 | 49.140 | TC 20/SC 14 |
| ISO 15859-8:2004 Space systems -- Fluid characteristics, sampling and test methods -- Part 8: Kerosine propellant | 90.60 | 49.140 | TC 20/SC 14 |
| ISO 15859-9:2004 Space systems -- Fluid characteristics, sampling and test methods -- Part 9: Argon | 90.60 | 49.140 | TC 20/SC 14 |
| ISO 15859-10:2004 Space systems -- Fluid characteristics, sampling and test methods -- Part 10: Water | 90.60 | 49.140 | TC 20/SC 14 |
| ISO 15859-11:2004 Space systems -- Fluid characteristics, sampling and test methods -- Part 11: Ammonia | 90.60 | 49.140 | TC 20/SC 14 |
| ISO 15859-12:2004 Space systems -- Fluid characteristics, sampling and test methods -- Part 12: Carbon dioxide | 90.60 | 49.140 | TC 20/SC 14 |
| ISO 15859-13:2004 Space systems -- Fluid characteristics, sampling and test methods -- Part 13: Breathing air | 90.60 | 49.140 | TC 20/SC 14 |
| ISO 15860:2006 Space systems -- Gas contamination -- Measurement methods for field tests | 90.20 | 49.140 | TC 20/SC 14 |
| ISO 15862:2009 Space systems -- Launch-vehicle-to-spacecraft flight environments telemetry data processing | 60.60 | 49.140 | TC 20/SC 14 |
| ISO 15863:2003 Space systems -- Spacecraft-to-launch-vehicle interface control document | 90.60 | 49.140 | TC 20/SC 14 |
| ISO 15864:2004 Space systems -- General test methods for space craft, subsystems and units | 90.93 | 49.140 | TC 20/SC 14 |
| ISO 15865:2005 Space systems -- Qualification assessment | 90.93 | 49.140 | TC 20/SC 14 |
| ISO 15872:2002 Aerospace -- UNJ threads -- Gauging | 90.60 | 49.030.10 | TC 20/SC 4 |
| ISO 15887:2000 Space data and information transfer systems -- Data systems -- Lossless data compression | 90.60 | 49.140 | TC 20/SC 13 |
| ISO 15887:2000/Cor 1:2009 | 60.60 | 49.140 | TC 20/SC 13 |
| ISO 15888:2000 Space data and information transfer systems -- Standard formatted data units -- Referencing environment | 90.60 | 49.140 | TC 20/SC 13 |
| ISO 15889:2003 Space data and information transfer systems -- Data description language -- EAST specification | 90.60 | 49.140 | TC 20/SC 13 |
| ISO 15891:2000 Space data and information transfer systems -- Protocol specification for space communications -- Network protocol | 90.60 | 49.140 | TC 20/SC 13 |
| ISO 15892:2000 Space data and information transfer systems -- Protocol specification for space communications -- Security protocol | 90.60 | 49.140 | TC 20/SC 13 |
| ISO 15893:2000 Space data and information transfer systems -- Protocol specification for space communications -- Transport protocol | 90.92 | 49.140 | TC 20/SC 13 |
| ISO 15894:2000 Space data and information transfer systems -- Protocol specification for space communications -- File protocol | 90.60 | 49.140 | TC 20/SC 13 |
| ISO 16004:2005 Aircraft ground equipment -- Passenger boarding bridge or transfer vehicle -- Requirements for interface with aircraft doors | 90.60 | 49.100 | TC 20/SC 9 |
| ISO 16031-1:2002 Aerospace fluid systems -- O-rings, inch series: Inside diameters and cross sections, tolerances and size-identification codes -- Part 1: Close tolerances for hydraulic systems | 90.60 | 49.080 | TC 20/SC 10 |
| ISO 16031-2:2003 Aerospace fluid systems -- O-rings, inch series: Inside diameters and cross-sections, tolerances and size-identification codes -- Part 2: Standard tolerances for non-hydraulic systems | 90.60 | 49.080 | TC 20/SC 10 |
| ISO 16049-1:2001 Air cargo equipment -- Restraint straps -- Part 1: Design criteria and testing methods | 90.92 | 49.120 | TC 20/SC 9 |
| ISO 16049-2:2005 Air cargo equipment -- Restraint straps -- Part 2: Utilization guidelines and lashing calculations | 90.92 | 49.120 | TC 20/SC 9 |
| ISO 16091:2002 Space systems -- Integrated logistic support | 90.93 | 49.140 | TC 20/SC 14 |
| ISO 16412:2005 Air cargo equipment -- Air cargo pallets -- Utilization guidelines | 90.60 | 55.180.30 | TC 20/SC 9 |
| ISO 16454:2007 Space systems -- Structural design -- Stress analysis requirements | 60.60 | 49.140 | TC 20/SC 14 |
| ISO/TS 16457:2009 Space systems -- Space environment (natural and artificial) -- The Earth's ionosphere model: international reference ionosphere (IRI) model and extensions to the plasmasphere | 60.60 | 07.060 49.140 | TC 20/SC 14 |
| ISO 16458:2004 Space systems -- Unmanned spacecraft transportation -- General requirements | 90.93 | 49.140 | TC 20/SC 14 |
| ISO 17057:1999 Aerospace -- Rivets, solid -- Test method | 90.20 | 49.030.60 | TC 20/SC 4 |
| ISO 17355:2007 Space data and information transfer systems -- CCSDS file delivery protocol | 90.92 | 49.140 | TC 20/SC 13 |
| ISO 17399:2003 Space systems -- Man-systems integration | 90.60 | 49.140 | TC 20/SC 14 |
| ISO/TR 17400:2003 Space systems -- Space launch complexes, integration sites and other facilities -- General testing guidelines | 60.60 | 49.140 | TC 20/SC 14 |
| ISO 17401:2004 Space systems -- Spacecraft interface requirements document for launch vehicle services | 90.60 | 49.140 | TC 20/SC 14 |
| ISO 17666:2003 Space systems -- Risk management | 90.93 | 49.140 | TC 20/SC 14 |
| ISO 17775:2006 Aircraft -- Ground-service connections -- Potable water, toilet-flush water and toilet drain | 90.20 | 49.080 49.100 | TC 20/SC 10 |
| ISO 19933:2007 Space systems -- Format for spacecraft launch environment test report | 60.60 | 49.140 | TC 20/SC 14 |
| ISO 20652:2006 Space data and information transfer systems -- Producer-archive interface -- Methodology abstract standard | 90.60 | 49.140 | TC 20/SC 13 |
| ISO 20683-1:2005 Aircraft ground equipment -- Design, test and maintenance for towbarless towing vehicles (TLTV) interfaced with nose-landing gear -- Part 1: Main-line aircraft | 90.60 | 49.100 | TC 20/SC 9 |
| ISO 20683-2:2004 Aircraft ground equipment -- Design, test and maintenance for towbarless towing vehicles (TLTV) interfaced with nose-landing gear -- Part 2: Regional aircraft | 90.60 | 49.100 | TC 20/SC 9 |
| ISO 21347:2005 Space systems -- Fracture and damage control | 90.93 | 49.140 | TC 20/SC 14 |
| ISO 21348:2007 Space environment (natural and artificial) -- Process for determining solar irradiances | 60.60 | 49.140 | TC 20/SC 14 |
| ISO 21349:2007 Space systems -- Project reviews | 60.60 | 49.140 | TC 20/SC 14 |
| ISO 21350:2007 Space systems -- Off-the-shelf item utilization | 60.60 | 49.140 | TC 20/SC 14 |
| ISO 21351:2005 Space systems -- Functional and technical specifications | 90.93 | 49.140 | TC 20/SC 14 |
| ISO 21459:2006 Space data and information transfer systems -- Proximity-1 space link protocol -- Coding and synchronization sublayer | 90.20 | 49.140 | TC 20/SC 13 |
| ISO 21460:2007 Space data and information transfer systems -- Proximity-1 space link protocol -- Physical layer | 60.60 | 49.140 | TC 20/SC 13 |
| ISO 21648:2008 Space systems -- Flywheel module design and testing | 60.60 | 49.140 | TC 20/SC 14 |
| ISO 21849:2006 Aircraft and space -- Industrial data -- Product identification and traceability | 90.20 | 35.240.60 49.020 | TC 20 |
| ISO 21961:2003 Space data and information transfer systems -- Data entity dictionary specification language (DEDSL) -- Abstract syntax | 90.60 | 49.140 | TC 20/SC 13 |
| ISO 21962:2003 Space data and information transfer systems -- Data entity dictionary specification language (DEDSL) -- PVL syntax | 90.60 | 49.140 | TC 20/SC 13 |
| ISO 22009:2009 Space systems -- Space environment (natural and artificial) -- Model of the earth's magnetospheric magnetic field | 60.60 | 49.140 | TC 20/SC 14 |
| ISO 22010:2007 Space systems -- Mass properties control | 60.60 | 49.140 | TC 20/SC 14 |
| ISO 22072:2005 Aerospace -- Electrohydrostatic actuator (EHA) -- Characteristics to be defined in procurement specifications | 90.92 | 49.080 | TC 20/SC 10 |
| ISO 22089:2009 Aerospace -- Hydraulic power transfer units -- General specifications | 60.60 | 49.080 | TC 20/SC 10 |
| ISO 22108:2008 Space systems -- Non-flight items in flight hardware -- Identification and control | 60.60 | 49.140 | TC 20/SC 14 |
| ISO 22538-1:2007 Space systems -- Oxygen safety -- Part 1: Design of oxygen systems and components | 60.60 | 49.140 | TC 20/SC 14 |
| ISO 22538-2:2007 Space systems -- Oxygen safety -- Part 2: Selection of metallic materials for oxygen systems and components | 60.60 | 49.140 | TC 20/SC 14 |
| ISO 22538-3:2007 Space systems -- Oxygen safety -- Part 3: Selection of non-metallic materials for oxygen systems and components | 60.60 | 49.140 | TC 20/SC 14 |
| ISO 22538-4:2007 Space systems -- Oxygen safety -- Part 4: Hazards analyses for oxygen systems and components | 60.60 | 49.140 | TC 20/SC 14 |
| ISO 22641:2005 Space data and information transfer systems -- TM (telemetry) synchronization and channel coding | 90.60 | 49.140 | TC 20/SC 13 |
| ISO 22642:2005 Space data and information transfer systems -- TC (telecommand) synchronization and channel coding | 90.60 | 49.140 | TC 20/SC 13 |
| ISO 22642:2005/Cor 1:2007 | 60.60 | 49.140 | TC 20/SC 13 |
| ISO 22643:2003 Space data and information transfer systems -- Data entity dictionary specification language (DEDSL) -- XML/DTD Syntax | 90.93 | 49.140 | TC 20/SC 13 |
| ISO 22644:2006 Space data and information transfer systems -- Orbit data messages | 90.92 | 49.140 | TC 20/SC 13 |
| ISO 22645:2005 Space data and information transfer systems -- TM (telemetry) space data link protocol | 90.60 | 49.140 | TC 20/SC 13 |
| ISO 22646:2005 Space data and information transfer systems -- Space packet protocol | 90.60 | 49.140 | TC 20/SC 13 |
| ISO 22647:2006 Space data and information transfer systems -- Space link identifiers | 90.92 | 49.140 | TC 20/SC 13 |
| ISO 22663:2007 Space data and information transfer systems -- Proximity-1 space link protocol -- Data link layer | 60.60 | 49.140 | TC 20/SC 13 |
| ISO 22664:2005 Space data and information transfer systems -- TC (telecommand) space data link protocol | 90.60 | 49.140 | TC 20/SC 13 |
| ISO 22666:2007 Space data and information transfer systems -- AOS (advanced orbiting systems) space data link protocol | 60.60 | 49.140 | TC 20/SC 13 |
| ISO 22667:2005 Space data and information transfer systems -- Communication operations Procedure-1 | 90.60 | 49.140 | TC 20/SC 13 |
| ISO 22669:2007 Space data and information transfer systems -- Space link extension (SLE) -- Return-all-frames service | 60.60 | 49.140 | TC 20/SC 13 |
| ISO 22670:2006 Space data and information transfer systems -- Space link extension (SLE) -- Return-channel-frames service | 90.60 | 49.140 | TC 20/SC 13 |
| ISO 22671:2007 Space data and information transfer systems -- Space link extension (SLE) -- Forward communications link transmission unit (CLTU) service | 60.60 | 49.140 | TC 20/SC 13 |
| ISO 22672:2006 Space data and information transfer systems -- Space link extension (SLE) -- Forward space packet service | 90.60 | 49.140 | TC 20/SC 13 |
| ISO 23038:2006 Space systems -- Space solar cells -- Electron and proton irradiation test methods | 90.20 | 49.140 | TC 20/SC 14 |
| ISO 23041:2007 Space systems -- Unmanned spacecraft operational procedures -- Documentation | 60.60 | 49.140 | TC 20/SC 14 |
| ISO/TR 23462:2007 Space systems -- Guidelines to define the management framework for a space project | 60.60 | 49.140 | TC 20/SC 14 |
| ISO 23933:2006 Aerospace -- Aramid reinforced lightweight polytetrafluoroethylene (PTFE) hose assemblies, classification 135 degrees C/20 684 kPa (275 degrees F /3 000 psi) and 135 degrees C/21 000 kPa (275 degrees F/3 046 psi) -- Procurement specification | 90.60 | 49.080 | TC 20/SC 10 |
| ISO 23935:2006 Aircraft -- Environmental test procedures for airborne fluid system components -- Resistance to fire in designated fire zones | 90.60 | 49.080 | TC 20/SC 10 |
| ISO 24637:2009 Space systems -- Electromagnetic interference (EMI) test reporting requirements | 60.60 | 49.140 | TC 20/SC 14 |
| ISO 24638:2008 Space systems -- Pressure components and pressure system integration | 60.60 | 49.140 | TC 20/SC 14 |
| ISO 26143:2007 Space data and information transfer systems -- Space link extension (SLE) -- Return operational control fields service | 60.60 | 49.140 | TC 20/SC 13 |
| ISO 26868:2009 Space data and information transfer systems -- Image data compression | 60.60 | 49.140 | TC 20/SC 13 |
| ISO 26870:2009 Space systems -- Launch pad and integration site operational documents | 60.60 | 49.140 | TC 20/SC 14 |
| ISO 27027:2008 Aerospace -- Solid-state remote power controllers -- General performance requirements | 60.60 | 49.060 | TC 20/SC 1 |
| ISO 27996:2009 Aerospace fluid systems -- Elastomer seals -- Storage and shelf life | 60.60 | 49.080 83.140.50 | TC 20/SC 10 |
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