Aerospace — Lever-operated, two-position, ON/OFF switches — Directions of operation

Withdrawal of ISO/R 47-1957

Withdrawal of ISO/R 222-1961

Withdrawal of ISO 223-1975

Aircraft — Connectors for ground electrical supplies — Part 1: Design, performance and test requirements

Aircraft — Connectors for ground electrical supplies — Part 1: Design, performance and test requirements

Aircraft — Connectors for ground electrical supplies — Part 2: Dimensions

Connections for aircraft ground electrical supplies

Withdrawal of ISO/R 469-1966

Aircraft — Dimensions for single-hole mounting (Class 1 and Class 2) lever-operated manual switches

Aircraft — General purpose push-pull single-pole circuit-breakers — Dimensions

Aircraft — Dimensions for general purpose push-pull three-pole circuit-breakers

Sealed-beam landing lamps for aircraft — Dimensions

Lever-operated manual switches for aircraft — Performance requirements

General purpose push-pull single-pole circuit-breakers for aircraft — Performance requirements

General purpose push-pull single-pole circuit-breakers for aircraft — Performance requirements

General purpose push-pull three-pole circuit-breakers for aircraft — Performance requirements

General purpose push-pull three-pole circuit-breakers for aircraft — Performance requirements

Aerospace — Characteristics of aircraft electrical systems

Aerospace — Characteristics of aircraft electrical systems

Aerospace — Characteristics of aircraft electrical systems

Aerospace — Characteristics of aircraft electrical systems

Aircraft — Precision fuse-links — General requirements

Aircraft — Precision fuse-links — Type A

Aircraft — Precision fuse-links — Type B

Design requirements for aircraft electrical plug and socket connectors

Aircraft — Electrical connectors — Design requirements

Aluminium terminal ends for crimping to aircraft aluminium electrical cables

Crimped joints for aircraft electrical cables

Aircraft — Fire-resisting electrical cables — Dimensions, conductor resistance and mass

Heat-resisting equipment wires for aircraft

Aircraft electrical circuit diagrams

Tests for aircraft electrical plug and socket connectors

Aircraft — Electrical connectors — Tests

Aircraft — Fire-resisting electrical cables — Performance requirements

Aircraft — Fire-resisting electrical cables — Methods of test

Static invertors for aircraft

Aircraft — Two- and four-pole sealed electromagnetic relays, 2 A and 3 A — Clearance and fixing dimensions

Heat-resisting equipment wires for aircraft — Methods of test

Aircraft — Electrical cables — Identification

Aircraft — Electrical cables — Identification marking

Aircraft — Conductors for general purpose aircraft electrical cables and aerospace applications — Dimensions and characteristics

Aircraft — Conductors for general purpose aircraft electrical cables and aerospace applications — Dimensions and characteristics

Aircraft — Conductors for general purpose aircraft electrical cables and aerospace applications — Dimensions and characteristics — Amendment 1: Correction of table 1

Environmental tests for aircraft equipment — Part 1: Insulation resistance and high voltage tests for electrical equipment

Environmental tests for aircraft equipment — Insulation resistance and high voltage tests for electrical equipment

Aircraft — Dimensions for single-hole and triple-hole mounting (Class 3) lever-operated manual switches

Aircraft — Radio frequency flexible coaxial cables — Dimensions and electrical characteristics

Aircraft — Lever-operated manual switches (Class 3) — Performance requirements

Aircraft — Repairable contactors (not hermetically sealed) — Performance requirements

Aircraft — Hermetically sealed monostable electrical relays, 2A and 3A — Part 1: Operating characteristics and test conditions

Aircraft — Hermetically sealed monostable electrical relays, 2A and 3A — Part 2: Type approval tests

Aerospace construction — List of equivalent terms — Part 1: Aerospace electrical equipment

Aircraft — 2 and 3A plug-in base change-over relays, Type II, with crimped connections — Clearance and fixing dimensions

Aircraft — Electromagnetic relays and contactors — Part 1: General requirements

Aircraft — Ground support electrical supplies — General requirements

Aircraft — Ground support electrical supplies — General requirements

Aircraft — Proximity switches — Part 1: General requirements

Aircraft — Nickel-chromium and nickel-aluminium thermocouple extension cables — Part 1: Conductors — General requirements and tests

Aircraft — Nickel-chromium and nickel-aluminium thermocouple extension cables — Part 2: Terminations — General requirements and tests

Aircraft — Nickel-chromium and nickel-aluminium thermocouple extension cables — Part 2: Terminations — General requirements and tests — Amendment 1

Aircraft — Nickel-chromium and nickel-aluminium thermocouple extension cables — Part 3: Crimp-type ring terminal ends — Dimensions

Aircraft — Nickel-chromium and nickel-aluminium thermocouple extension cables — Part 4: Crimp-type butt connectors — Dimensions

Aircraft — Terminal junction systems — Part 1: Characteristics

Aircraft — Terminal junction systems — Part 2: Tests

Aircraft — Terminal junction systems — Part 2: Tests

Aircraft — Terminal junction systems — Part 3: Detail specification for type 1 system

Aircraft — Terminal junction systems — Part 4: Detail specification for type 2 system

Aircraft — Terminal junction systems — Part 5: Detail specification for type 3 system

Aircraft — Terminal junction systems — Part 6: Detail specification for type 4 system

Aircraft — Electrical cables and cable harnesses — Vocabulary

Aircraft — Electrical cables and cable harnesses — Vocabulary

Aircraft — Solid-state remote power controllers — General requirements

Aircraft — Solid-state remote power controllers — General requirements — Amendment 1

Aircraft — Crimp-removable contacts for electrical connectors — Identification system

Aircraft — Crimp-removable contacts for electrical connectors — Identification system

Aircraft — Crimp-removable contacts for electrical connectors — Identification system — Amendment 1

Aircraft — Hybrid remote power controllers — General requirements

Aerospace — Requirements for digital equipment for measurements of aircraft electrical power characteristics

Aerospace — Wire, aluminium alloy and copper-clad aluminium conductors — General performance requirements

Aircraft — LED based taxiing lightsystem — General requirements

Aircraft — Smart contactor — General requirements

Aerospace electrical requirements — Sleeves and moulded shapes — Specifications for aircraft use

Information technology — Sensor networks — Use cases of aeronautics industry: Active Air-flow Control

Aerospace — High-power solid-state power controller — General performance requirements

Aircraft — Auto-transformer rectifier units (ATRUs) — General requirements

Aerospace — Solid-state remote power controllers — General performance requirements

Aerospace — Solid-state remote power controllers — General performance requirements