| Mfg Part Number: APU-5B B | Alternate P/N: APU5BB | NSN : 6615-01-110-6322 | NIIN : 011106322 | CAGE Code : 80058 | Manufacturer: Joint Electronics Type Designation | Item Name : Controller Flight A | FSC : 6615 Automatic Pilot Mechanisms and Airborne Gyro Components |
Controller Flight A011106322 Thank you for your interest in the various NSN parts and components that we offer on Hardware Domain. NSN 6615-01-110-6322 is listed alongside the part number APU-5B B, having been manufactured by Joint Electronics Type Designation. If you would like to procure NSN part APU-5B B, or other items related to Controller Flight A, we invite you to first begin with a quote for your comparisons which you may receive by completing the RFQ form that is provided below. When completing our form, we ask that you offer us as many details as you can regarding your needs so that we may craft a solution that is individually personalized.
This Joint Electronics Type Designation part APU-5B B was produced under the CAGE Code 80058, which ensures that you are procuring exactly what you require. To guarantee the quality of our offerings, we enact a strict NO CHINA SOURCING pledge and subject countless items to rigorous quality assurance measures as necessary. As a culmination of our efforts in terms of quality control and export compliance, we are proud to operate with AS9120B, ISO 9001:2015, and FAA AC 00-56B certification and accreditation. Complete an RFQ form today for NSN 6615-01-110-6322 or get in contact with one of our representatives to see how Hardware Domain can fulfill all your part requirements with ease.
| MRC | Criteria | Characteristic |
|---|---|---|
| AMPS | Current Rating In Amps | 0.2 AND 0.7 |
| FAAZ | Phase | SINGLE |
| FREQ | Frequency In Hertz | 400 |
| ATJK | Power Source | EXTERNAL |
| FTLD | Functional Description | RELAYS COMMANDS RECVD FROM THE ACFT DIRECTLY OR INDIRECTLY THROUGH THE REMOTE CONTROL SUBSYSTEM DATA LINK TO THE TARGET DETECTING DEVICE FOR DETECTING, DESIGNATING AND TRACKING TARGETS; ALSO PROCESSES GUIDANCE AND INERTIAL STABILIZATION SIGNALS RECVD FROM THE MIDCOURSE GUIDANCE DEVICE, TARGET DETECTING DEVICE AND INERTIAL SENSORS INTO POSITION COMMANDS FOR THE FLIGHT CONTROL SURFACE ACTUATORS IN ORDER TO CONTROL THE FLIGHT PATH OF THE GBU-15(V) |
| MRC | Decoded Requirement | Clear Text Reply |
| FEAT | Special Features | GUIDED BOMB AUTOMATIC PILOT; HAS ANALOG INPUTS FOR PITCH AND YAW, MIDCOURSE GUIDANCE DEVICE, INTERTIAL SENSORS, LINE OF SIGHT RATE COMMANDS; ANALOG OUTPUTS FOR FLIGHT CONTROL SYSTE; DISVRETE INPUTS AND OUTPUTS FOR ACFT COMMAMNDS, DATA LINK COMMANDS, IDENTIFIERS, TIME DELAY, WEAPON COMMANDS, WEAPON READY STATUS; DESIGNED FOR AIRBORNE GUIDED BOMB INSTALLATION; INSTALLED IN THE COMMON CONTROL MODULE BY MEANS OF 4 SOCKET HEAD CAP SCREWS; A SINGLE 158 CONTACT CONNECTOR ATTACHES TO THE COMMON CONTROL MODULE WIRING HARNESS |
| AFXE | Maximum Voltage Rating In Volts | 115.0 AC AND 28.0 DC |
| CHQP | Maximum Overall Length | 9.800 INCHES |
| CHQR | Maximum Overall Height | 4.200 INCHES |
| CHQQ | Maximum Overall Width | 4.200 INCHES |
| ADTV | Case Material | ALUMINUM |
| AGAV | End Item Identification | MODULAR GUIDED BOMB GBU-15(V)1/B AND 2/B |
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