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| MRC | Criteria | Characteristic |
|---|---|---|
| AWZJ | POWER SOURCE | EXTERNAL |
| AGAV | END ITEM IDENTIFICATION | C-17 AIRCRAFT |
| AJAG | UNPACKAGED UNIT WIDTH | 10.10 INCHES NOMINAL |
| AJAH | UNPACKAGED UNIT HEIGHT | 7.60 INCHES NOMINAL |
| AXQJ | INTELLIGENCE INPUT METHOD | ELECTRICAL |
| FEAT | SPECIAL FEATURES | EFFECTIVITY P41 TO SUBSEQUENT ACFT; P/N 103E4151G14 IS THE HARDWARE ONLY |
| FTLD | FUNCTIONAL DESCRIPTION | USED TO COMPUTE PRIMARY FLIGHT CONTROL, STABILITY AND CONTROL AUGMENTATION AND AUTOMATIC FLIGHT CONTROL FUNCTIONS; PERFORMS ALL CALCULATIONS NECESSARY TO IMPLEMENT FUNCTIONS OF THE STABILITY AND CONTROL AUGMENATION SYSTEM, AUTOPILOT, AUTOTHROTTLE, FLIGHT DIRECTOR, HEADS UP DISPLAY CONTROL AND GROUND PROXIMITY WARNING SYSTEM |
| CBBL | FEATURES PROVIDED | ELECTROSTATIC SENSITIVE |
| ACUR | DIRECT CURRENT VOLTAGE RATING IN VOLTS | 22.0 AND 29.5 |
| CRTL | CRITICALITY CODE JUSTIFICATION | CBBL |
| SUPP | SUPPLEMENTARY FEATURES | MANUFACTURERS NAME: COMPUTER,FLIGHT CONTROL |
| AJAF | UNPACKAGED UNIT LENGTH | 16.30 INCHES NOMINAL |
| 17B 1091 L | 17B-4-3 WITH TABS | 17B-10-3 | 17B-1029-12-3 |
| 17B-1029-12-3 | 17B-1033-5-3 | 17B-4-3 WITH TABS | 17B-1033-4-3 |
| 17B-10-1 | 17B-1091-R | 17B-1091-L | 17B-1033-4-3 |
| 17B-1033-4-3 | 17B-1033-4-3 | 17B-10-3 | 17B-13-1 |
 |
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