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 |
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