356A1409P53

Technical Characteristics

• Test Data Document

  89954-356a1407 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)

• Criticality Code Justification

  cbbl

• Part Name Assigned By Controlling Agency

  microcircuit, plastic encapsulated (surface mount) procurement and selection requirements (for quad diff receiver)

• Operating Temp Range

  -55.0/+125.0 deg celsius

• Features Provided

  electrostatic sensitive

• Design Function And Quantity

  4 receiver, line differential

• Body Length

  10.49 millimeters maximum

• End Item Identification

  c-17a aircraft

• Case Outline Source And Designator

  ms-012-ac joint electron device engineering council

• Voltage Rating And Type Per Characteristic

  5.0 volts nominal power source and 0.5 volts maximum output logic low and 2.4 volts minimum output logic high

• Input Circuit Pattern

  quad 3 input and 2 input

• Special Test Features

  brf1a16nb is 100 percent upscreened per para 3.1.1 of dwg 89954-s56a1407 by approved test facility for operation through temps of -55c to +125c.

• Special Features

  quad differential receiver w/ common enable/disable control

• Terminal Type And Quantity

  16 gullwing

• Inclosure Configuration

  dual-in-line

• Inclosure Material

  plastic

• Body Width

  7.62 millimeters maximum

• Output Logic Form

  transistor-transistor logic