2075135-0702

Technical Characteristics

• End Item Identification

  aircraft, hawkeye e-2c; aircraft, tomcat f-14; aircraft, hornet f/a-18; landing craft air cushion (lcac); helicopter, advance attack, ah-1w; helicopter, uscg search and rescue, hh-60j; helicopter, lamps mark iii, sh-60b; apx-100 airborne radar;

• Operating Temp Range

  -55.0/+125.0 deg celsius

• Criticality Code Justification

  feat

• Special Features

  weapon system essential

• Terminal Type And Quantity

  14 printed circuit

• Body Height

  0.185 inches maximum

• Input Circuit Pattern

  6 input

• Test Data Document

  96906-mil-std-883 drawing (this is the basic governing drawing, such as a contractor drawing, original equipment manufacturer drawing, etc.; excludes any specification, standard or other document that may be referenced in a basic governing drawing)

• Body Length

  0.785 inches maximum

• ~1

  helicopter, search and rescue, hh-60h; helicopter, carr

• Storage Temp Range

  -65.0/+150.0 deg celsius

• Design Function And Quantity

  2 comparator, voltage, differential

• Body Width

  0.220 inches minimum and 0.310 inches maximum

• Inclosure Material

  ceramic

• Terminal Surface Treatment

  solder

• Voltage Rating And Type Per Characteristic

  7.0 volts maximum power source

• Case Outline Source And Designator

  d-1 mil-m-38510

• Maximum Power Dissipation Rating

  500.0 milliwatts

• Inclosure Configuration

  dual-in-line

• Features Provided

  hermetically sealed and burn in and w/strobe and w/resistor