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Aircraft — Nickel-chromium and nickel-aluminium thermocouple extension cables — Part 1: Conductors — General requirements and tests
90.93 Standard confirmed
Aircraft — Nickel-chromium and nickel-aluminium thermocouple extension cables — Part 2: Terminations — General requirements and tests
90.93 Standard confirmed
Aircraft — Nickel-chromium and nickel-aluminium thermocouple extension cables — Part 2: Terminations — General requirements and tests — Amendment 1
60.60 Standard published
Aircraft — Nickel-chromium and nickel-aluminium thermocouple extension cables — Part 3: Crimp-type ring terminal ends — Dimensions
90.93 Standard confirmed
Aircraft — Nickel-chromium and nickel-aluminium thermocouple extension cables — Part 4: Crimp-type butt connectors — Dimensions
90.93 Standard confirmed
Aircraft — Terminal junction systems — Part 1: Characteristics
90.93 Standard confirmed
Aircraft — Terminal junction systems — Part 3: Detail specification for type 1 system
90.93 Standard confirmed
Aircraft — Terminal junction systems — Part 4: Detail specification for type 2 system
90.93 Standard confirmed
Aircraft — Terminal junction systems — Part 5: Detail specification for type 3 system
90.93 Standard confirmed
Aircraft — Terminal junction systems — Part 6: Detail specification for type 4 system
90.93 Standard confirmed
Aircraft — Electrical cables and cable harnesses — Vocabulary
90.93 Standard confirmed
Aircraft — Solid-state remote power controllers — General requirements
90.60 Close of review
Aircraft — Solid-state remote power controllers — General requirements — Amendment 1
60.60 Standard published
Aircraft — Crimp-removable contacts for electrical connectors — Identification system
90.60 Close of review
Aircraft — Crimp-removable contacts for electrical connectors — Identification system — Amendment 1
60.60 Standard published
Aircraft — Terminal junction systems — Part 2: Tests
40.99 Full report circulated: DIS approved for registration as FDIS
Aerospace electrical requirements — Sleeves and moulded shapes — Specifications for aircraft use
60.60 Standard published
