| MRC | Criteria | Characteristic |
|---|---|---|
| AJAF | III UNPACKAGED UNIT LENGTH | 10.00 INCHES NOMINAL |
| AXQJ | INTELLIGENCE INPUT METHOD | ELECTRICAL |
| RTSE | III RELATIONSHIP TO SIMILAR EQUIPMENT | RETROFIT OF F110-GE-100/100B ENGINE MONITORING SYSTEM COMPUTER WITH NEWSOFTWARE, NSN 6610-01-429-9115 |
| RDAL | III REFERENCE DATA AND LITERATURE | TP5-E1-12-1 |
| SR-1 | MFR SOURCE CONTROLLING REFERENCE | 8KE124AAC9 |
| FEAT | SPECIAL FEATURES | AIR FRAME MOUNTED UNIT,LITHIUM BATTERY BACKUP,NORMAL OPERATING TEMP -65TO 160 DEG F, NORMAL OPERATING POWER 50 WATTS |
| AWZJ | POWER SOURCE | SELF-CONTAINED OR EXTERNAL |
| FTLD | III FUNCTIONAL DESCRIPTION | RECEIVES DIGITAL SIGNALS ON ENGINE PERFORMANCE FROM ENGINE MONITORING SYSTEM PROCESS AND AIRCRAFT MULTIPLEXERBUS. SIGNALS ARE COMPARED AGAINST PREDETERMINED LIMIT STORED IN THE EMSC |
| ACUR | DIRECT CURRENT VOLTAGE RATING IN VOLTS | 28.0 |
| SR-1 | MANUFACTURERS CODE | 97424 |
| AJAG | III UNPACKAGED UNIT WIDTH | 6.500 INCHES NOMINAL |
| SR-1 | SPEC/STD CONTROLLING DATA |
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