NSN 6615-01-448-2341
Part Details | FLIGHT CONTROL PROCESSOR
6615-01-448-2341 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, 17B1U6001567, 17B1U6001-567, 17B1U6001559, 17B1U6001-559, 6615-01-448-2341, 01-448-2341, 6615014482341, 014482341
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 66 | AUG 25, 1997 | 01-448-2341 | 53048 ( PROCESSOR, FLIGHT CONTROL ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 6615-01-448-2341
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 103E4151G14 | 89954 | BAE SYSTEMS CONTROLS INC. |
| 17B1U6001-567 | 88277 | BOEING COMPANY, THEDBA BOEING |
| 17B1U6001-559 | 88277 | BOEING COMPANY, THEDBA BOEING |
Technical Data | NSN 6615-01-448-2341
| 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 | EFFECTIVITY P41 TO SUBSEQUENT ACFT; P/N 103E4151G14 IS THE HARDWARE ONLY |
| 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 AIRCRAFT |
| 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 AUGMENATION SYSTEM, AUTOPILOT, AUTOTHROTTLE, FLIGHT DIRECTOR, HEADS UP DISPLAY CONTROL AND GROUND PROXIMITY WARNING SYSTEM |