NSN 6615-01-464-9820
Part Details | FLIGHT CONTROL PROCESSOR
6615-01-464-9820 A unit which accepts and processes information from flight instruments and the control mechanism of an aircraft to initiate a change in the position or course of the aircraft.
Alternate Parts: 17B1U6001571, 17B1U6001-571, 6615-01-464-9820, 01-464-9820, 6615014649820, 014649820
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 66 | MAY 17, 1999 | 01-464-9820 | 53048 ( PROCESSOR, FLIGHT CONTROL ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 6615-01-464-9820
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 17B1U6001-571 | 88277 | BOEING COMPANY, THEDBA BOEING |
Technical Data | NSN 6615-01-464-9820
| Characteristic | Specifications |
|---|---|
| INTELLIGENCE INPUT METHOD | ELECTRICAL |
| POWER SOURCE | EXTERNAL |
| DIRECT CURRENT VOLTAGE RATING IN VOLTS | 28.0 |
| FEATURES PROVIDED | ELECTROSTATIC SENSITIVE |
| SPECIAL FEATURES | MFG NAME COMPUTER, FLIGHT CONTROL, OPERATING TEMP -40 TO 131 DEG F; ALTITUDE UP TO 50K FT; MEMORY 314K; BASICPROCESSOR UNIT WITHOUT SOFTWARE IS P/N103E4151G103; P/N 17B1U6001-571 IS THEBASIC UNIT W/SOFTWARE VERSION 6.1 INSTALLELD |
| CRITICALITY CODE JUSTIFICATION | CBBL |
| UNPACKAGED UNIT LENGTH | 16.30 INCHES NOMINAL |
| UNPACKAGED UNIT WIDTH | 10.10 INCHES NOMINAL |
| UNPACKAGED UNIT HEIGHT | 7.60 INCHES NOMINAL |
| END ITEM IDENTIFICATION | C-17 ACFT |
| FUNCTIONAL DESCRIPTION | USED TO COMPUTE PRIMARY FLIGHT CONTROL, STABILITY AND CONTROL AUGMENTATION AND AUTOMATIC FLIGHT CONTROL FUNCTIONS; PERFORMS ALL CALCULATIONS NECESSARY TO IMPLEMENT FUNCTIONS OF THE STABILITY AND CONTROL AUGMENTATION SYSTEM,AUTOPILOT, AUTOTHROTTLE, FLIGHT DIRECTOR, HEADS UP DISPLAY CONTROL AND GROUND PROXIMITY WARNING SYSTEM |