Filter :
| Standard and/or project under the direct responsibility of ISO/TC 20/SC 1 Secretariat | Stage | ICS |
|---|---|---|
|
ISO/R 224:1961 [Withdrawn]
Standard form of declaration of performance of aircraft electrical equipment
|
95.99 | |
|
ISO 461-1:1985 [Withdrawn]
Aircraft — Connectors for ground electrical supplies — Part 1: Design, performance and test requirements
|
95.99 | |
|
Aircraft — Connectors for ground electrical supplies — Part 1: Design, performance and test requirements
|
90.93 | |
|
Aircraft — Connectors for ground electrical supplies — Part 2: Dimensions
|
90.93 | |
|
ISO/R 461:1965 [Withdrawn]
Connections for aircraft ground electrical supplies
|
95.99 | |
|
Aircraft — Dimensions for single-hole mounting (Class 1 and Class 2) lever-operated manual switches
|
90.93 | |
|
Aircraft — General purpose push-pull single-pole circuit-breakers — Dimensions
|
90.92 | |
|
ISO/DIS 530 [Under development]
Aircraft — General purpose push-pull single-pole circuit-breakers — Dimensions
|
40.20 | |
|
Aircraft — Dimensions for general purpose push-pull three-pole circuit-breakers
|
90.92 | |
|
ISO/DIS 1033 [Under development]
Aircraft — Dimensions for general purpose push-pull three-pole circuit-breakers
|
40.20 | |
|
Sealed-beam landing lamps for aircraft — Dimensions
|
90.93 | |
|
Lever-operated manual switches for aircraft — Performance requirements
|
90.93 | |
|
ISO 1467:1973 [Withdrawn]
General purpose push-pull single-pole circuit-breakers for aircraft — Performance requirements
|
95.99 | |
|
General purpose push-pull single-pole circuit-breakers for aircraft — Performance requirements
|
60.60 | |
|
ISO 1509:1973 [Withdrawn]
General purpose push-pull three-pole circuit-breakers for aircraft — Performance requirements
|
95.99 | |
|
General purpose push-pull three-pole circuit-breakers for aircraft — Performance requirements
|
60.60 | |
|
ISO 1540:1984 [Withdrawn]
Aerospace — Characteristics of aircraft electrical systems
|
95.99 | |
|
Aerospace — Characteristics of aircraft electrical systems
|
90.93 | |
|
Aircraft — Precision fuse-links — General requirements
|
90.93 | |
|
Aircraft — Precision fuse-links — Type A
|
90.93 | |
|
Aircraft — Precision fuse-links — Type B
|
90.93 | |
|
ISO 1949:1973 [Withdrawn]
Design requirements for aircraft electrical plug and socket connectors
|
95.99 | |
|
Aircraft — Electrical connectors — Design requirements
|
90.20 | |
|
Aluminium terminal ends for crimping to aircraft aluminium electrical cables
|
90.60 | |
|
Crimped joints for aircraft electrical cables
|
90.92 | |
|
ISO 1966 [Under development]
Crimped joints for aircraft electrical cables
|
60.00 | |
|
Aircraft — Fire-resisting electrical cables — Dimensions, conductor resistance and mass
|
90.93 | |
|
Heat-resisting equipment wires for aircraft
|
90.93 | |
|
Aircraft electrical circuit diagrams
|
90.93 | |
|
ISO 2100:1972 [Withdrawn]
Tests for aircraft electrical plug and socket connectors
|
95.99 | |
|
Aircraft — Electrical connectors — Tests
|
90.93 | |
|
Aircraft — Fire-resisting electrical cables — Performance requirements
|
90.93 | |
|
Aircraft — Fire-resisting electrical cables — Methods of test
|
90.93 | |
|
Static invertors for aircraft
|
90.93 | |
|
Aircraft — Two- and four-pole sealed electromagnetic relays, 2 A and 3 A — Clearance and fixing dimensions
|
90.93 | |
|
Heat-resisting equipment wires for aircraft — Methods of test
|
90.93 | |
|
ISO 2574:1974 [Withdrawn]
Aircraft — Electrical cables — Identification
|
95.99 | |
|
Aircraft — Electrical cables — Identification marking
|
90.93 | |
|
ISO 2635:1979 [Withdrawn]
Aircraft — Conductors for general purpose aircraft electrical cables and aerospace applications — Dimensions and characteristics
|
95.99 | |
|
Aircraft — Conductors for general purpose aircraft electrical cables and aerospace applications — Dimensions and characteristics
|
90.93 | |
|
Aircraft — Conductors for general purpose aircraft electrical cables and aerospace applications — Dimensions and characteristics — Amendment 1: Correction of table 1
|
60.60 | |
|
Environmental tests for aircraft equipment — Insulation resistance and high voltage tests for electrical equipment
|
90.60 | |
|
Aircraft — Dimensions for single-hole and triple-hole mounting (Class 3) lever-operated manual switches
|
90.93 | |
|
ISO 3389:1975 [Withdrawn]
Aircraft — Radio frequency flexible coaxial cables — Dimensions and electrical characteristics
|
95.99 | |
|
Aircraft — Lever-operated manual switches (Class 3) — Performance requirements
|
90.93 | |
|
ISO 4084:1977 [Withdrawn]
Aircraft — Repairable contactors (not hermetically sealed) — Performance requirements
|
95.99 | |
|
Aircraft — Magnetic indicators — Part 1: Characteristics
|
90.93 | |
|
Aircraft — Magnetic indicators — Part 2: Tests
|
90.93 | |
|
Aircraft — Hermetically sealed monostable electrical relays, 2A and 3A — Part 1: Operating characteristics and test conditions
|
90.93 | |
|
Aircraft — Hermetically sealed monostable electrical relays, 2A and 3A — Part 2: Type approval tests
|
90.93 | |
|
Aircraft — 2 and 3A plug-in base change-over relays, Type II, with crimped connections — Clearance and fixing dimensions
|
90.60 | |
|
Aircraft — Electromagnetic relays and contactors — Part 1: General requirements
|
90.93 | |
|
ISO 6858:1982 [Withdrawn]
Aircraft — Ground support electrical supplies — General requirements
|
95.99 | |
|
Aircraft — Ground support electrical supplies — General requirements
|
90.92 | |
|
ISO/CD 6858 [Under development]
Aircraft — Ground support electrical supplies — General requirements
|
30.60 |
|
|
Aircraft — Proximity switches — Part 1: General requirements
|
90.60 | |
|
Aircraft — Nickel-chromium and nickel-aluminium thermocouple extension cables — Part 1: Conductors — General requirements and tests
|
90.93 | |
|
Aircraft — Nickel-chromium and nickel-aluminium thermocouple extension cables — Part 2: Terminations — General requirements and tests
|
90.93 | |
|
Aircraft — Nickel-chromium and nickel-aluminium thermocouple extension cables — Part 2: Terminations — General requirements and tests — Amendment 1
|
60.60 | |
|
Aircraft — Nickel-chromium and nickel-aluminium thermocouple extension cables — Part 3: Crimp-type ring terminal ends — Dimensions
|
90.93 | |
|
Aircraft — Nickel-chromium and nickel-aluminium thermocouple extension cables — Part 4: Crimp-type butt connectors — Dimensions
|
90.93 | |
|
Aircraft — Terminal junction systems — Part 1: Characteristics
|
90.60 | |
|
Aircraft — Terminal junction systems — Part 2: Tests
|
90.93 | |
|
ISO/DIS 8668-2 [Under development]
Aircraft — Terminal junction systems — Part 2: Tests
|
40.99 | |
|
Aircraft — Terminal junction systems — Part 3: Detail specification for type 1 system
|
90.60 | |
|
Aircraft — Terminal junction systems — Part 4: Detail specification for type 2 system
|
90.60 | |
|
Aircraft — Terminal junction systems — Part 5: Detail specification for type 3 system
|
90.93 | |
|
Aircraft — Terminal junction systems — Part 6: Detail specification for type 4 system
|
90.60 | |
|
Aircraft — Electrical cables and cable harnesses — Vocabulary
|
90.93 | |
|
Aircraft — Solid-state remote power controllers — General requirements
|
90.92 | |
|
Aircraft — Solid-state remote power controllers — General requirements — Amendment 1
|
60.60 | |
|
ISO/AWI 8816 [Under development]
Aircraft — Solid-state remote power controllers — General requirements
|
20.00 |
|
|
ISO 8843:1991 [Withdrawn]
Aircraft — Crimp-removable contacts for electrical connectors — Identification system
|
95.99 | |
|
Aircraft — Crimp-removable contacts for electrical connectors — Identification system
|
90.60 | |
|
Aircraft — Crimp-removable contacts for electrical connectors — Identification system — Amendment 1
|
60.60 | |
|
Aircraft — Hybrid remote power controllers — General requirements
|
90.93 | |
|
Aerospace — Requirements for digital equipment for measurements of aircraft electrical power characteristics
|
90.93 | |
|
Aerospace — Wire, aluminium alloy and copper-clad aluminium conductors — General performance requirements
|
90.93 | |
|
Aircraft — LED based taxiing lightsystem — General requirements
|
90.93 | |
|
Aircraft — Smart contactor — General requirements
|
90.93 | |
|
Aerospace electrical requirements — Sleeves and moulded shapes — Specifications for aircraft use
|
60.60 | |
|
Aerospace — High-power solid-state power controller — General performance requirements
|
60.60 | |
|
Aircraft — Auto-transformer rectifier units (ATRUs) — General requirements
|
60.60 | |
|
ISO/DIS 25207 [Under development]
General requirements for integrated optoelectronic connectors for aerospace applications
|
40.99 | |
|
ISO/WD 25898 [Under development]
Aircraft — Autotransformer Unit (ATU) — General Requirements
|
20.20 |
|
|
ISO 27027:2008 [Withdrawn]
Aerospace — Solid-state remote power controllers — General performance requirements
|
95.99 | |
|
Aerospace — Solid-state remote power controllers — General performance requirements
|
90.93 |
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