586R967H01

Technical Characteristics

• Case Outline Source And Designator

  d-5 mil-m-38510

• Operating Temp Range

  -55.0/+125.0 deg celsius

• Criticality Code Justification

  feat

• Body Length

  2.096 inches maximum

• Special Features

  weapon system essential

• Output Logic Form

  emitter-coupled logic and transistor-transistor logic

• End Item Identification

  f-16 aircraft. f100-pw-200 (f-16 a/b/c/d) aircraft engine.

• Test Data Document

  96906-mil-std-883 standard (includes industry or association standards, individual manufactureer standards, etc.).

• Storage Temp Range

  -65.0/+150.0 deg celsius

• Inclosure Material

  ceramic

• Terminal Surface Treatment

  solder

• Voltage Rating And Type Per Characteristic

  7.0 volts maximum power source

• Body Width

  0.510 inches minimum and 0.620 inches maximum

• Input Circuit Pattern

  12 input

• Terminal Type And Quantity

  40 printed circuit

• Features Provided

  burn in and hermetically sealed and w/clock and positive outputs

• Inclosure Configuration

  dual-in-line

• Design Function And Quantity

  1 integrator

• Body Height

  0.165 inches minimum and 0.210 inches maximum