NSN 6610-01-395-4256
Part Details | FUEL SAVINGS ADVISORY COMPUTER
6610-01-395-4256 A computer specifically designed to provide continuous in-flight advisories to minimize fuel consumption. This is done by measuring and processing aircraft performance data and comparing it to the flight plan provided by the crew. It performs computations to show the differences between the two and sends the data to a display (not included) for monitoring.
Alternate Parts: 1728880101, 172888-01-01, MODEL 2902B, CPU193A24J28, CPU-193/A24J-28, 6610-01-395-4256, 01-395-4256, 6610013954256, 013954256
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 66 | AUG 29, 1994 | 01-395-4256 | 53116 ( COMPUTER, FUEL SAVINGS ADVISORY ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 6610-01-395-4256
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 172888-01-01 | 35351 | GE AVIATION SYSTEMS LLC |
| MODEL 2902B | 35351 | GE AVIATION SYSTEMS LLC |
| CPU-193/A24J-28 | 80058 | JOINT ELECTRONICS TYPE DESIGNATIONSYSTEM |
Technical Data | NSN 6610-01-395-4256
| Characteristic | Specifications |
|---|---|
| INPUT INTELLIGENCE TYPE | FUEL SENSOR AND PITCH-ROLL SIGNAL DATA AND ALTITUDE DATA AND VERTICAL ACCELERATION SIGNAL |
| INTELLIGENCE INPUT METHOD | ELECTRICAL |
| OUTPUT INTELLIGENCE TYPE | NAVIGATION COURSE SELECTED |
| POWER SOURCE | EXTERNAL |
| ALTERNATING CURRENT VOLTAGE RATING IN VOLTS | 115.0 |
| FREQUENCY IN HERTZ | 400.0 |
| PHASE | SINGLE |
| TERMINAL TYPE | CONNECTOR, PLUG |
| MOUNTING TYPE | RACK |
| SPECIAL FEATURES | SEMICONDUCTOR UV ERASEABLE PROM, 120K 16-BIT WORD, DATA STORAGE, DIGITAL AND ANALOG INPUTS AND OUTPUTS, LOGIC CIRCUITS WITH A FORCED AIR INTERNAL BLOWER |
| UNPACKAGED UNIT LENGTH | 19.560 INCHES NOMINAL |
| UNPACKAGED UNIT WIDTH | 7.940 INCHES NOMINAL |
| UNPACKAGED UNIT HEIGHT | 7.630 INCHES NOMINAL |
| END ITEM IDENTIFICATION | C-141 AND A-5 AIRCRAFT |
| FUNCTIONAL DESCRIPTION | INTERFACES WITH AIRCRAFT SENSORS AND COMPUTES THE OPTIMUM FLIGHT PROFILES |