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National Stock Number:
6615-01-397-7980
Federal Supply Class:
6615
National Item Identification Number:
013977980
Description:
CONTROLLER,FLIGHT,AUTOMATIC PILO
Detail:
A CONTROLLER DESIGNED TO CONTROL AN AIRCRAFT THROUGH AN AUTOMATIC PILOT IN PITCH, YAW, ROLL AND COORDINATED TURNS.
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Manufacturer Information:
| 5050051-9 | 0VWL8 | HONEYWELL INTL INC DEFENSE AVIONICS SYSTEMS | | 5050051-9 | 55972 | HONEYWELL INTL INC DEFENSE AVIONICS SYSTEMS | | 5050051-9 | 5Y043 | HONEYWELL INTERNATIONAL INC. | | CP-2284/AYW-1(V) | 80058 | JOINT ELECTRONICS TYPE DESIGNATION SYSTEM |
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Techincal Specification:
| CASE MATERIAL | ALUMINUM ALLOY | | FREQUENCY IN HERTZ | 400.0 | | FUNCTIONAL DESCRIPTION | FUNCTIONS FOR C-141 AND C-130 AIRCRAFT: PROVIDES THE DATA PROCESSING, COMPUTING, AND LOGIC MANIPULATION REQUIRED TO ACCOMPLISH THE FUNCTIONS NEEDED FOR AUTOPILOT OPERATION. ADDITIONAL FUNCTIONS FOR THE C-141 AIRCRAFT: FLIGHT DIRECTOR CONTROL LAW COMPUTATIONS, AUTOPILOT CONTROL LAW COMPUTATIONS, FLIGHT T CONTROL LAW COMPUTATIONS, FLIGHT DIRECTOR/AUTOPILOT ENGAGE/DISENGAGE LOGIC, FLIGHT DIRECTOR/AUTOPILOT MODE SELECT LOGIC, AUTOPILOT SERVO LOOP CLOSURES, ADI COMMAND BAR PROCESSING, & STABILIZER TRIM COMMAND GENERATION, FAIL OPERATIVE YAW DAMPER COMPUTATIONS AND A/T CONTROL LAW COMPUTATIONS ARE ALSO PROVIDED. | | PART NAME ASSIGNED BY CONTROLLING AGENCY | PROCESSOR, FLIGHT CONTROL AUTOMATIC PILOT | | PHASE | SINGLE | | POWER SOURCE | EXTERNAL | | PROPRIETARY CHARACTERISTICS | PACS | | MAXIMUM OVERALL HEIGHT | 7.620 INCHES | | MAXIMUM OVERALL LENGTH | 19.597 INCHES | | MAXIMUM OVERALL WIDTH | 8.850 INCHES | | MAXIMUM VOLTAGE RATING IN VOLTS | 115.0 AC | | REFERENCE DATA AND LITERATURE | DD FORM 61 | | SPECIAL FEATURES | RECIEVES AC & DC ANALOG, DISCRETE DIGITAL, SYNCHRO INPUTS, SENDS AC ANALOG, DISCRETE DIGITAL, RESOLVER OUTPUTS VIA MIL-STD 1553 INTERFACE, ARINC 429 DATA LINKS AND RS-422 DATA LINKS. | | TYPE/MODEL DESIGNATION | CP-2284/AYW-1(V) |
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