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| MRC | Criteria | Characteristic |
|---|---|---|
| RDAL | III REFERENCE DATA AND LITERATURE | TO 5E1-2-12-1 |
| FEAT | SPECIAL FEATURES | AMBIENT OPERATING TEMPERATURE -65 TO +160 DEG F.;DOWNLOAD OPERATING POWER 20 WATTS;NORMAL OPERATING POWER 50 WATTS;THE EMSC IS AN AIRFRAME MOUNTED UNIT;BATTERY BACKUP |
| SR-1 | MANUFACTURERS CODE | 07482 |
| AGAV | III END ITEM IDENTIFICATION | F110-GE100 ENGINE F-16C/D ACFT |
| AJAG | III UNPACKAGED UNIT WIDTH | 6.50 INCHES NOMINAL |
| AXQJ | INTELLIGENCE INPUT METHOD | ELECTRICAL |
| AJAH | III UNPACKAGED UNIT HEIGHT | 5.00 INCHES NOMINAL |
| ZZZV | III FSC APPLICATION DATA | ENGINE MONITORING SYSTEM COMPUTER (EMSC)SUPPGBATTERY NOT INCLUDED |
| AWZJ | POWER SOURCE | EXTERNAL OR SELF-CONTAINED |
| FTLD | III FUNCTIONAL DESCRIPTION | RECEIVES DIGITAL ENGINE PERFORMANCE SIGNALS FROM THE ENGINE MONITORING SYSTEM PROCESSOR AND AIRCRAFT PARAMETERS FROM THE MUX;THESE SIGNALS ARE COMPARED AGAINST PREDETERMINED LIMITS STORED IN THE EMSC;EXCEEDENCES AND FAULTS ARE TRANSMITTED TO REMOTE AIRCRAFT SYSTEMS;ALSO MONITORS THE DEC AND ITS OWN PERFORMANCES AND TRANSMITTS DATA TO THE PILOT DISPLAYS;DETECTS ENGINE CONTROL LOOP FAILURES AND COMPRESSOR STALLS |
| SR-1 | MFR SOURCE CONTROLLING REFERENCE | 7127M73P08 |
| ACUR | DIRECT CURRENT VOLTAGE RATING IN VOLTS | 28.0 |
| AJAF | III UNPACKAGED UNIT LENGTH | 10.00 INCHES NOMINAL |
| ADTV | III CASE MATERIAL | ALUMINUM ALLOY |
| SR-1 | SPEC/STD CONTROLLING DATA |
 |
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