Mod 6c Electrical Hardware

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Last updated 8:57 AM on 7/7/26
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138 Terms

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Insulated Wire

  • provides: dielectric insulation, thermal protection, abrasion resistance, moisture resistance, fire resistance, and fluid resistance.

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Conductor Materials

  • Resistance is directly proportional to length → Longer wire = higher resistance.

  • Resistance is inversely proportional to cross-sectional area → Larger cross-sectional area = lower resistance.

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Copper or Copper Alloy Wire

  • Non-magnetic – won’t interfere with sensitive flight equipment.

  • Malleable, conductive, and corrosion resistant.

  • Smaller cross-sectional area than aluminium (same current rating).

  • Easier to bend, shape, and terminate.

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Aluminium or Aluminium Alloy Wire

  • Used for high current over long distances.

  • Non-magnetic.

  • Higher specific resistance than copper → requires a larger cross-sectional area.

  • Approximately 50% weight saving compared to copper.

  • Can crystallise (work-harden) and break under vibration.

  • Rarely used for general aircraft wiring.

  • Do not use on engine-mounted accessories or in areas with:

    • Corrosive fumes

    • Severe vibration

    • Mechanical stresses

    • Frequent disconnection

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Conductor Plating

  • Copper and aluminium oxidise when exposed to oxygen.

  • Oxidation is accelerated by aircraft temperature and pressure variations.

  • Plated with tin, silver, or nickel to minimise oxidation.

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Wire Size

  • Measured using the American Wire Gauge (AWG) system.

  • Larger AWG number = smaller wire.

  • Typical aircraft wire sizes: 24 AWG (smallest) to 0000 (4/0) AWG (largest).

  • 24 AWG = 0.51 mm, 0000 (4/0) AWG = 11.7 mm.

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14 AWG

20 AMPs

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12 AWG Stranded & Solid

25 AMPs

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10 AWG

30 AMPs

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8 AWG

40 AMPs

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6 AWG

55 AMPs

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2 AWG

95 AMPs

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1/0 AWG

125 AMPs

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Aircraft Wire Insulation

  • Materials: PVC, nylon, Teflon®, various polymers, and glass cloth braid.

  • Most insulation is rated to 600 V.

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Wire Insulation Temperature Rating

  • Insulation does not affect wire resistance.

  • Resistance generates heat, which can burn the insulation.

  • Current limit depends on the insulation temperature rating.

  • Different types of insulation have different temperature ratings.

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Insulation Resistance

  • Resistance to current leakage through the insulation.

  • Measured with an insulation tester (megger).

  • Used to determine the condition of insulation.

  • Cracked or faulty insulation is not serviceable, even if insulation resistance is high.

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Electrical Cable

includes:

  • Two or more insulated conductors in a common insulating material.

  • One or more insulated conductors with an overall shield (shielded cable).

  • Two insulated conductors twisted together (twisted pair).

  • Single insulated centre conductor with a metallic braided outer conductor (coaxial cable).

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Aircraft Wire

  • Only approved aircraft wiring is permitted.

  • Must pass rigorous testing before being added to the Qualified Products List (QPL).

  • OEM/military wire must come from approved wire mills.

  • Majority of aircraft wiring is made from stranded copper.

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Conductor Stranding

  • Stranded wire = smaller wires twisted or wrapped together.

  • Provides more flexibility than solid conductors.

  • Reduces metal fatigue.

  • Reduces conductor breakage caused by flight vibration and flexing.

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Bonding

  • Grounds components not otherwise electrically connected.

  • Protects against static/electrostatic charge build-up and lightning strike discharge.

  • Correct bonding:

    • Minimises electrical damage.

    • Prevents high potential differences (sparks).

    • Reduces electric shock risk.

    • Reduces interference with radio communications and navigational aids.

    • Provides a low resistance electrical return path in earth-return systems.

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Shielding

  • Current-carrying wires produce a magnetic field.

  • Magnetic fields can interfere with aircraft instrumentation and control systems.

  • AC and pulsating DC have the greatest effect on electronic equipment.

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Airframe Wire

  • Designed for component interconnection in the aircraft airframe.

  • Normal or medium weight wire.

  • Two insulation coverings for improved abrasion protection.

  • Can be used without conduit in harsh conditions.

  • High tensile strength reduces installation damage and breakage.

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Airframe Wire Construction

  • Must have at least 19 conductor strands and be 18 AWG or larger.

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Airframe Wire Characteristics

  • Multiple thick insulation layers for harsh conditions.

  • Stiff and springy, making installation more difficult.

  • Corrosion-resistant plated conductors make soldering difficult.

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Interconnect/Hook-up Cable

  • Designed for component interconnection inside the fuselage.

  • Lightweight with one insulation layer.

  • Requires secondary insulation/conduit if used as airframe wire.

  • Smaller diameter than equivalent airframe wire.

  • More flexible, saving weight and space.

  • More prone to damage when pulled through pressure bungs.

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Interconnect Cable Construction

  • Must have at least 19 conductor strands.

  • Small gauge wires: use high-strength alloy conductors.

  • Wires smaller than 20 AWG:

    • Additional clamps.

    • Group with at least 3 other wires.

    • Additional support at terminations.

  • Do not use where there is:

    • Excessive vibration.

    • Repeated bending.

    • Frequent disconnection from screw terminations.

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Equipment Wire

  • Used within aircraft equipment (LRUs).

  • Smaller conductor sizes than hook-up wire.

  • More strands for flexibility and good solder joints.

  • Can be single-strand if secured to a solid structure.

  • Thinner, less springy insulation.

  • Not designed for interconnect wiring.

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Fire Resistant Cable

  • Used in flight critical circuits.

  • Resists flames up to 1093 °C (2000 °F) under short-time emergency conditions.

  • Predominantly used in the engine compartment.

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Warning: This Wire May Contain Asbest

  • Asbestos has not been permitted since 1993.

  • Undated fire resistant wire should be treated as containing asbestos.

  • Contact Environmental Health if asbestos is identified or suspected.

  • Replace with non-asbestos alternatives where feasible.

  • Fire resistance ≠ high temperature.

  • Use fire resistant cable only where required.

  • More susceptible to contamination and abrasion.

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Fire Resistant Cable Construction

  • Multiple insulation layers for fire protection.

  • Maintains insulation for 30 minutes to allow the aircraft to land.

  • Conductors have a thick alloy coating with a higher melting point than copper.

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Fire Resistant Cable Construction Diagram

inside → outside

  • Nickel clad high strength copper alloy conductor – conductor with a high melting point coating.

  • Inorganic barrierthermal insulation against fire.

  • Polyimide tapemaintains electrical insulation at high temperatures.

  • PTFE tapeouter protective layer (abrasion/chemical protection).

<p><span><strong>inside → outside</strong></span></p><ul><li><p><span><strong>Nickel clad high strength copper alloy conductor</strong> – conductor with a <strong>high melting point coating</strong>.</span></p></li><li><p><span><strong>Inorganic barrier</strong> – <strong>thermal insulation</strong> against fire.</span></p></li><li><p><span><strong>Polyimide tape</strong> – <strong>maintains electrical insulation</strong> at high temperatures.</span></p></li><li><p><span><strong>PTFE tape</strong> – <strong>outer protective layer</strong> (abrasion/chemical protection).</span></p></li></ul><p></p>
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High Temperature Cable

  • Temperature rating of 125 °C or higher (some manufacturers use 90 °C).

  • Different from fire-resistant cable.

  • Can be single- or multi-conductor.

  • May have a fibreglass braid or Kevlar-fibre jacket.

  • Two key factors:

    • Temperature rating – maximum continuous operating temperature.

    • Current capacity – maximum current without exceeding insulation/jacket temperature limits.

  • Undersized cable overheats, reducing cable life and compromising the cable.

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Thermocouple Cable

  • Used to detect and measure temperature changes.

  • Made of a pair of dissimilar metallic conductors.

  • Extension leads must be the same material as the thermocouple.

  • Extension wires are paired in a braided jacket and colour coded.

  • Correct installation is required to maintain accuracy.

  • Gas turbine engines use multiple thermocouples arranged in a harness.

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Thermocouple Cable Construction

  • Harness insulation: silicone rubber or PTFE-impregnated fibreglass.

  • Harness terminates at an engine or firewall junction box.

  • Extension cable insulation: polyvinyl, as it is not subject to high temperatures.

<ul><li><p><span><strong>Harness insulation:</strong> silicone rubber or <strong>PTFE-impregnated fibreglass</strong>.</span></p></li><li><p><span><strong>Harness terminates</strong> at an <strong>engine or firewall junction box</strong>.</span></p></li><li><p><span><strong>Extension cable insulation:</strong> <strong>polyvinyl</strong>, as it is <strong>not subject to high temperatures</strong>.</span></p></li></ul><p></p>
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Bonding Lead

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Shock Mount with Bonding Strap

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Bonding Cable Construction

  • Made from copper or aluminium.

  • Must have sufficient surge capacity to carry the whole discharge.

  • Material must not produce galvanic corrosion.

  • Length: long enough for movement, not so long that resistance increases.

  • Sacrificial aluminium washers prevent galvanic corrosion between copper straps and aluminium structure.

  • Aluminium alloy straps are used in most cases.

  • Copper straps are used to bond stainless steel, cadmium plated steel, copper, brass, or bronze.

  • Always use the bonding cables/straps specified in the AMM and IPC.

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Bonding Strap on a Flight Control

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AC 43.13-1B Section 15

Grounding and Bonding

<p>Grounding and Bonding</p>
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Power Cables

  • Runs from power sources to bus bars, between bus bars, and from bus bars to equipment.

  • Protected by circuit protection devices.

  • Aluminium conductors are ~50% lighter than copper but are usually 2 AWG sizes larger.

  • Aluminium conductors have more strands to reduce vibration cracking (work hardening).

  • Copper cables are used between engine-mounted generators and the fuselage.

  • Generator feeder cables are an example of power cables.

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Generator Feeder Cables

Example of larger size cables

<p>Example of larger size cables</p>
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Data Cables

  • Connect different aircraft systems.

  • Carry voltage signals, not power → conduct very little current.

  • Lighter conductors.

  • Do not require overload protection.

  • Types: single conductor & earth, single screened, twisted pair, screened twisted pair, coaxial, triaxial, multiple screened, and fibre optic cables.

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Multicore Screened and Jacketed Cables

  • Up to four cores, twisted together.

  • May be jacketed or screened and jacketed.

  • Screening is usually a braid with 85% surface coverage.

  • Replacement cable must not reduce the screening standard.

  • Cores are colour coded for easy identification.

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Data Bus

  • Must be replaced only with the cable specified by the Design Authority.

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Unshielded Twisted Pair (UTP)

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Shielded Twisted Pair (STP)

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Twisted Pair Cable

  • Twisted wires cancel magnetic fields, reducing interference.

  • Twisting reduces unwanted induced signals.

  • UTP (Unshielded Twisted Pair) – no ground shield.

  • STP (Shielded Twisted Pair) – ground shield reduces external signal interference.

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High Tension Cables

  • Operating voltage over 600 V.

  • Mainly used in engine ignition systems (up to 40,000 V).

  • Single-core stranded, insulated, and metal braided screened to prevent interference.

  • Also used in: strobe systems, unregulated frequency wild generators, and hybrid/electric aircraft battery packs.

  • Spec 55: 600 V (single wall), 1000 V (dual wall).

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Piston Engine Ignition Cable Construction

  • Silicone jacket – heat, cold, chemicals, moisture.

  • Reinforcing member – strength & terminal retention.

  • Silicone insulation – dielectric & heat performance.

  • Conductive silicone layer – EMI/RFI suppression.

  • Fibreglass braid – strength.

  • Carbon impregnated fibreglass core – conductivity.

  • Kevlar® reinforcement – strength.

  • Ferrite layer – EMI/RFI suppression.

  • Wire-wound layer – EMI/RFI suppression.

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High Tension Cable - Picture

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Spec 55 Insulated System - Single Wall

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Spec 55 Insulated System - Dual Wall

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Ignition Cable (Piston Engine)

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High-Tension Ignition Cable Terminations

  • Connected using special end fittings with springs or contact caps, secured to the conductor, insulation, and threaded coupling assembly.

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High-Tension Ignition Cable End Exploded View

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High-tension ignition Cable Termination Picture

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High Tension Cable for Piston Engine

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Warning - Igniter Plug

  • Igniter plug discharge can be up to 2,000 amps.

  • Low battery voltage does not reduce discharge power, only the rate of spark discharge.

  • HEIU output voltage can cause significant injury.

  • Isolate input power and wait at least 1 minute before working on the system.

  • Short the capacitor before working inside the HEIU.

  • Coil and magneto systems have higher voltage but lower current than HEIUs.

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1: High temperature "Class E" silicone jacket to withstand heat, cold, chemicals and moisture.

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2: Reinforcing member for added strength and terminal retention.

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3. Silicone insulation for superior dielectric and heat performance.

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4. Conductive silicon layer for high temperature performance and EMI/RFI noise suppression.

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5. Fiberglass braid for maximum strength

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6. Carbon impregnated berglass core for superior support conductivity.

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7. Core reinforced with KEVLAR®.

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8. Layer impregnated with Ferrite.

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9. Wire-wound layer to suppress EMI/RFI noise.

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Spark Plug Wires

  • Carry over 20,000 volts from the distributor cap to the spark plug.

  • Fibre core carries the high voltage.

  • Older metallic core wires caused electrical interference.

  • Some have a locking connection at the distributor cap.

  • To remove: remove the distributor cap first, squeeze the terminals together, then remove the spark plug wire.

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Coaxial Cabel

  • Used to connect electronic equipment to antennas.

  • Prevents radio frequency interference (RFI).

  • Two conductors:

    • Centre conductor covered by a dielectric.

    • Outer conductor covered by a protective sheath.

  • Do not kink, squash, stand on, or drop tools on the cable – it will become unserviceable.

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Coaxial Cable Construction

  • Centre conductor: solid or stranded copper (plain, tinned, silver plated, or gold plated).

  • Dielectric: polyethylene or Teflon®.

  • Outer conductor: fine wire braid.

  • Outer jacket: protects against weather, fluids, mechanical and electrical damage.

  • Used in: communication, navigation, and capacitance fuel quantity indicating systems.

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Antenna connected using co-axial connector

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Coaxial Cable Construction

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Coaxial Cable Advantages

  • Shielded against electrostatic and magnetic fields.

  • Does not radiate or pick up external interference.

  • Common impedance: 75 Ω.

  • Damage that changes the cable’s coaxiality changes its impedance, degrading or stopping equipment operation.

  • After insulation testing, always short the cable before reconnecting to prevent equipment damage.

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Co-axial Cable Diagram

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Typical Co-axial Lead with BNC Connector

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Impendence Calculations of Coaxial Cable

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Triaxial Cable

Three Parts (Remember: Signal → Return → Noise)

  • Centre wire → Carries the signal.

  • First shieldReturn path for the signal.

  • Second shield → Carries external noise to ground.

Used For

  • Antenna cable for very sensitive signal detection systems.

  • Example: Automatic Direction Finder (ADF).

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Multiple Layers of Shielding

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Triax Cable

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MIL-W-22759 Aircraft Wire

  • is commonly used in new aircraft wiring installations.

  • Always consult the manufacturer's Service Manual (AMM) and Service Bulletins (SBs) before replacing aircraft wiring.

  • Check for the correct:

    • Wire type

    • Wire size

  • All aircraft wire must have its type identification imprinted along its length.

Memory Trick

"22759 = Check Manual, Check Size, Check Stamp."

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MIL22759

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Crimping

  • Attaches a terminal/contact to a conductor without solder.

  • Uses compression (deformation) of the terminal barrel around the conductor.

  • Creates a homogenous mass between the conductor and terminal.

  • Produces a strong mechanical and electrical connection

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A Good Crimp should ?

  • Be as strong as the conductor.

  • Have good electrical conductivity.

  • Not introduce impedance or signal discontinuity.

  • Use the correct combination of:

    • Conductor

    • Crimp barrel/terminal

    • Crimp tool

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Advantages of Crimping

  • Faster and easier fabrication.

  • Uniform operation.

  • Good electrical conductivity.

  • Lower voltage drop.

  • Strong connections (as strong as the conductor).

  • Eliminates solder-related problems (solder slop and flux).

  • No dry solder joints

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Crip Types

  • Ring terminal

  • Slotted terminal

  • Hook-type terminal

  • Ring terminal (lug) is the most commonly used.

  • Preferred because it virtually eliminates circuit failure due to terminal disconnection.

Memory Tip

Ring = Reliable (most secure, least likely to disconnect).

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Splices

  • A method of connecting conductors using a crimped connector.

  • Usually a permanent connection using a self-insulated splice connector.

  • Permitted only if it does not affect the reliability or electromechanical characteristics of the wiring.

  • Maximum of one splice is allowed in any one wire segment between two connectors or disconnect points.

  • Crimper calibration must be checked before use by verifying the calibration label/sticker is current.

  • Refer to MIL-C-22520 for crimping tool requirements.

  • TIR (Total Indicator Reading) measures the total deviation from the true centre line after a contact is crimped.

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Crimping Tool Calibration Label

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Contact Size and Deformation by crimper

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MIL-C-22520 Crimping Tool

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Types of Electrical Connectors

  • M (Motion Picture) Series (1925):

  • Mechanical locking ring to prevent accidental disconnection.

  • P (Paramount Studios) Series:

    • Introduced die-cast shells, moulded pin inserts and latch locking devices.

  • F (Fox Studios) Series:

    • Introduced the threaded coupling ring.

    • Adapted for the Douglas DC-1 and later aircraft.

    • Led to the AF firewall connector, the first hostile environment connector for aircraft.

  • Most common aircraft connectors are AN (Army-Navy) and MS (Military Specification).

  • AN connectors have been superseded by MS connectors (same part number, AN replaced with MS).

  • Installed on wiring that is frequently disconnected.

  • Power supply side is typically connected to the socket to reduce the chance of an accidental short when connectors are separated.

  • Commonly used on avionic components with multi-pin connectors for easy maintenance.

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Military Connector Specifications

  • Standardise aircraft and military connectors.

  • Ensure reliability, performance and environmental protection.

  • Define:

    • Housing dimensions

    • Insert layout

    • Operating characteristics

  • Approved manufacturers are listed on the Qualified Products List (QPL).

  • Crimped contacts are generally used.

  • Use environmental-resistant connectors where there are fluids, vibration, shock or corrosion.

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QPL

Qualified Products List

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Millarary Specs

ensure reliability, performance and environmental protection.

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Plug

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Receptacle

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Connector Housings

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Connector Identification

  • Designed to meet military specifications.

  • Adapted for use in most aircraft.

  • Reference identification must remain legible throughout the life of the aircraft.

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Military Specication Connector Identication

  • Military specifications (MIL specs) vary greatly.

  • Part number descriptions can vary between MIL specs.

  • Refer to the applicable MIL spec and part number to determine a connector's exact characteristics.

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MIL Spec Part Number Breakdown

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