NSN 6615-01-442-8053
Part Details | FLIGHT CONTROL PROCESSOR
6615-01-442-8053 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: 103E4151G14, 17P1E1050729, 17P1E1050-729, 17B1U6001555, 17B1U6001-555, 6615-01-442-8053, 01-442-8053, 6615014428053, 014428053
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 66 | MAR 24, 1997 | 01-442-8053 | 53048 ( PROCESSOR, FLIGHT CONTROL ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 6615-01-442-8053
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 103E4151G14 | 89954 | BAE SYSTEMS CONTROLS INC. |
| 17P1E1050-729 | 88277 | BOEING COMPANY, THEDBA BOEING |
| 17B1U6001-555 | 88277 | BOEING COMPANY, THEDBA BOEING |
Technical Data | NSN 6615-01-442-8053
| Characteristic | Specifications |
|---|---|
| INTELLIGENCE INPUT METHOD | ELECTRICAL |
| POWER SOURCE | EXTERNAL |
| DIRECT CURRENT VOLTAGE RATING IN VOLTS | B22.0$$B29.5 |
| FEATURES PROVIDED | ELECTROSTATIC SENSITIVE |
| SPECIAL FEATURES | OPERATING TEMP -40 TO 131 DEG F; ALTITUDE UP TO 50,000 FEET; MEMORY 314K; BASIC PROCESSOR UNIT WITHOUT SOFTWARE IS PART NUMBER 103E415G14; PART NUMBER 17B1U6001-555 IS THE BASIC UNIT WITH SOFTWARE VERSION 3.1 INSTALLED |
| 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 |
| SUPPLEMENTARY FEATURES | MANUFACTURERS NAME: COMPUTER,FLIGHT CONTROL |
| 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, HEAD UP DISPLAY CONTROL AND GROUND PROXIMITY WARNING SYSTEM |