AM2504DMB

Technical Characteristics

• ~1

  engine, aircraft tf33-pw-102 (c-135e, ec-135h/k/p);

• Test Data Document

  35351-156618 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)

• Operating Temp Range

  -55.0/+125.0 deg celsius

• Criticality Code Justification

  feat

• Case Outline Source And Designator

  -0-015-aa joint electron device engineering council

• Features Provided

  w/register output and w/storage and synchronous and resettable and w/enable and complementary outputs and positive outputs and monolithic and hermetically sealed and medium speed

• Input Circuit Pattern

  4 input

• Special Features

  weapon system essential

• Bit Quantity (Non-Core)

  12

• Body Height

  0.140 inches minimum and 0.185 inches maximum

• Storage Temp Range

  -65.0/+150.0 deg celsius

• Terminal Surface Treatment

  solder

• Design Function And Quantity

  1 shift register, universal

• Inclosure Material

  ceramic and glass

• Output Logic Form

  transistor-transistor logic

• Maximum Power Dissipation Rating

  605.0 milliwatts

• Body Width

  0.545 inches maximum

• Voltage Rating And Type Per Characteristic

  5.5 volts maximum power source

• Terminal Type And Quantity

  24 printed circuit

• Inclosure Configuration

  dual-in-line

• Body Length

  1.235 inches minimum and 1.290 inches maximum

• End Item Identification

  navigational set,loran,type an/arn-101; support equipment, b-52 aircraft; helicopter, search and rescue, hh-60h; helicopter, carrier based asw, sh-60f; forrestal class cv; spruance class dd (963); landing craft air cushion (lcac); nimitz class cvn;