XT-2026

Technical Characteristics

• End Item Identification

  engine, aircraft, j85-ge-5/13 (f-5a/b, t-38a; aircraft, stratolifter c-135; aircraft, sof (ac-130h, mc-130h, ec-130e, hc-130) aircraft, hercules c-130

• Mounting Facility Type And Quantity

  4 unthreaded hole single mounting facility

• Overall Length

  1.355 inches maximum

• Mounting Facility Pattern

  rectangular single mounting facility

• Overall Width

  0.800 inches maximum

• Criticality Code Justification

  feat

• Special Features

  weapon system essential

• Environmental Protection

  hermetic

• Overall Height

  1.080 inches maximum

• Winding Dc Resistance Rating

  720.0 ohms nominal single winding

• Main Contact Load Current Rating At Maximum Rated Voltage

  1.0 amperes ac resistive load and 2.0 amperes dc resistive load

• Winding Quantity

  1

• Time Delay

  0.002 seconds nominal fixed release time

• Center To Center Distance Between Mounting Facilities Parallel To Width

  0.400 inches nominal single mounting facility

• Operating Voltage Rating And Type At Specified Temp

  26.5 volts teardrop, two holes type 4f single winding

• Nonpile-Up Main Contact Arrangement

  4 pole, double throw, one position momentary

• Time Delay

  0.008 seconds nominal fixed operate time

• Main Contact Maximum Voltage Rating In Volts

  115.0 ac and 30.0 dc

• Coil Quantity

  1

• Terminal Type And Quantity

  14 pin all functions

• Unthreaded Mounting Hole Diameter

  0.096 inches nominal single mounting facility

• Duty Type

  continuous

• Center To Center Distance Between Mounting Facilities Parallel To Length

  1.078 inches nominal single mounting facility