NSN 6620-01-311-3516
Part Details | ENGINE COMPUTER
6620-01-311-3516 A computer that receives, monitors, and stores data of the engine's operation. It also includes analysis of fault data and interfaces with other aircraft indicators and systems.
Alternate Parts: 8KE124AAD1, 7148M74P01, 6620-01-311-3516, 01-311-3516, 6620013113516, 013113516
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 66 | NOV 23, 1989 | 01-311-3516 | 47029 ( COMPUTER, ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 6620-01-311-3516
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 8KE124AAD1 | 97424 | AMETEK INC.DBA AMETEK AEROSPACE & DEFENSE |
| 7148M74P01 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 6620-01-311-3516
| Characteristic | Specifications |
|---|---|
| INTELLIGENCE INPUT METHOD | ELECTRICAL |
| POWER SOURCE | J$H |
| DIRECT CURRENT VOLTAGE RATING IN VOLTS | 28.0 |
| SPECIAL FEATURES | OPERATING TEMP -65 TO 160 DEG F, MAX 30 MINUTES AT 203 DEG F; DOWNLOAD OPERATING POWER 20 WATTS; NORMAL OPERATING POWER 50 WATTS; DOWNLOAD OPERATING VOLTAGE 28 VDC; THE EMSC IS AN AIRFRAME MOUNTED UNIT CONTAINING A BATTERY (EXCEPT FOR AIR SHIPMENT), A FLEX/CONNECTOR ASSY AND 4 ELECTRONIC COMPONENT ASSEMBLIES INCLUDING DIGITAL PROGRAMMED CPU BOARD |
| CASE MATERIAL | ALUMINUM ALLOY |
| UNPACKAGED UNIT LENGTH | 10.00 INCHES NOMINAL |
| UNPACKAGED UNIT WIDTH | 6.50 INCHES NOMINAL |
| UNPACKAGED UNIT HEIGHT | 5.00 INCHES NOMINAL |
| END ITEM IDENTIFICATION | F110-GE-129 ENGINE F16 ACFT |
| SUPPLEMENTARY FEATURES | BATTERY IS NOT INCLUDED FOR AIR SHIPMENT; BATTERY POWER 3.67 VDC AND IS MOUNTED IN THE FRONT PANEL OF THE EMSC |
| FUNCTIONAL DESCRIPTION | RECEIVES DIGITAL ENGINE PERFORMANCE SIGNALS FROM THE DIGITAL ELECTRONIC CONTROL (DEC) AND ACFT PARAMETERS FROM THE ACFT MUX BUS; THESE SIGNALS ARE COMPARED AGAINST PREDETERMINED LIMITS STORED IN THE EMSC; EXCEEDENCES AND FAULTS ARE TRANSMITTED TO REMOTE ACFT SYSTEMS; ALSO MONITORS THE DEC AND ITS OWN PERFORMANCE AND TRANSMITS DATA TO THE PILOT DISPLAY; DETECTS ENGINE CONTROL LOOP FAILURES AND COMPRESSOR STALLS |
| REFERENCE DATA AND LITERATURE | T.O. 5E1-2-12-1, -4 |
| FSC APPLICATION DATA | ENGINE MONITORING SYSTEM COMPUTER EMSC |