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| MRC | Criteria | Characteristic |
|---|---|---|
| AWZJ | POWER SOURCE | EXTERNAL |
| FAAZ | PHASE | SINGLE |
| RDAL | III REFERENCE DATA AND LITERATURE | T.O.5F1-2-5-3-1 |
| SUPP | III SUPPLEMENTARY FEATURES | MANUFACTURERS NAME: COMPUTER,FUEL SAVINGS ADVISORY SYSTEM |
| AXQJ | INTELLIGENCE INPUT METHOD | ELECTRICAL |
| AGAV | III END ITEM IDENTIFICATION | KC-135 AIRCRAFT |
| FREQ | FREQUENCY IN HERTZ | 400.0 |
| FEAT | SPECIAL FEATURES | TRAY MOUNTED PER ARINC, 1/2 ATR; MATERIAL ALUMINUM; CONTAINS SOFTWARE FOR AN OPERATIONS FLIGHT PROGRAM; P/N 7892013-005; INCLUDES 56 K UV PROM CIRCUIT CARD ASSY |
| AJAG | III UNPACKAGED UNIT WIDTH | 4.91 INCHES NOMINAL |
| AJAH | III UNPACKAGED UNIT HEIGHT | 7.79 INCHES NOMINAL |
| AXQH | INPUT INTELLIGENCE TYPE | AIR DATA AND DOPPLER |
| ACUQ | ALTERNATING CURRENT VOLTAGE RATING IN VOLTS | 115.0 |
| FTLD | III FUNCTIONAL DESCRIPTION | THIS COMPUTER MEASURES AND PROCESSES AIRCRAFT PERFORMANCE DATA AND, USING FLIGHT PLANNING INFORMATION SUPPLIED BY THE CREW, PERFORMS COMPUTATIONS USING COMPLEX ALGORITHMS TO PROVIDE THE CREW WITH CONTINUOUS IN-FLIGHT ADVISORIES TO MINIMIZE FUEL COMSUPTION |
| AJAF | III UNPACKAGED UNIT LENGTH | 21.78 INCHES NOMINAL |
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