17P1E1138: DATA ACQUISITION UNIT.
The DATA ACQUISITION UNIT is a THE BOEING COMPANY industrial component. Key specifications include POWER SOURCE: EXTERNAL, MOUNTING TYPE: RACK, UNPACKAGED UNIT WIDTH: 6.230 INCHES NOMINAL IN, TYPE/MODEL DESIGNATION: RO-626/A, UNPACKAGED UNIT HEIGHT: 7.030 INCHES NOMINAL IN, UNPACKAGED UNIT LENGTH: 7.280 INCHES NOMINAL IN. This part is cataloged in the U.S.
Government catalog under NSN 6610-01-577-1829, indicating validated use in U.S. government and defense logistics supply chains. Available through authorized enterprise resellers and TPM (Third Party Maintenance) channels.
Verify compatibility with your specific system configuration before ordering.
| POWER SOURCE | EXTERNAL |
| MOUNTING TYPE | RACK |
| UNPACKAGED UNIT WIDTH | 6.230 INCHES NOMINAL IN |
| TYPE/MODEL DESIGNATION | RO-626/A |
| UNPACKAGED UNIT HEIGHT | 7.030 INCHES NOMINAL IN |
| UNPACKAGED UNIT LENGTH | 7.280 INCHES NOMINAL IN |
| END ITEM IDENTIFICATION | C-17 AIRCRAFT |
| INPUT INTELLIGENCE TYPE | WIND DIRECTION AND WIND SPEED AND STRAIN GAGES AND AIRCRAFT LATTITUDE AND FUEL TRANSFER AND PITCH ACCELERATION AND YAW ACCELERATION AND ENGINE STALL |
| REFERENCE DATA AND LITERATURE | TO 1C-17A-4-2 & JETDAS DATA A |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| RELATIONSHIP TO SIMILAR EQUIPMENT | CONTAINS ONE ADDITIONAL FOUR CHANNEL MIL-STD-1553 INTERFACE CIRCUIT CARD ASSEMBLY THAN THE -003 VERSION |
| DIRECT CURRENT VOLTAGE RATING IN VOLTS | 28.0 |
| NSN | 6610-01-577-1829 |
| RELATIONSHIP TO SIMILAR EQUIPMENT | CONTAINS ONE ADDITIONAL FOUR CHANNEL MIL-STD-1553 INTERFACE CIRCUIT CARD ASSEMBLY THAN THE -003 VERSION |
| UNPACKAGED UNIT LENGTH | 7.280 INCHES NOMINAL IN |
| POWER SOURCE | EXTERNAL |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| REFERENCE DATA AND LITERATURE | TO 1C-17A-4-2 & JETDAS DATA A |
| UNPACKAGED UNIT WIDTH | 6.230 INCHES NOMINAL IN |
| DIRECT CURRENT VOLTAGE RATING IN VOLTS | 28.0 |
| UNPACKAGED UNIT HEIGHT | 7.030 INCHES NOMINAL IN |
| INPUT INTELLIGENCE TYPE | WIND DIRECTION AND WIND SPEED AND STRAIN GAGES AND AIRCRAFT LATTITUDE AND FUEL TRANSFER AND PITCH ACCELERATION AND YAW ACCELERATION AND ENGINE STALL |
| FUNCTIONAL DESCRIPTION | SOFTWARE CONTROLLED DATA RECORDERACQUIRING AIRCRAFT PARAMETER DATA FROM MIL-STD-1553 DATA BUSSES, FOUR ARINC 429 DATA BUSSES, AND SEVEN FUSELAGE MOUNTED STRAIN GAUGES. STORED DATA IS DOWNLOADED FOR MAINTENANCE ANALYSIS. MISHAP DATA IS FORWARDED TO FLIGHT DATA MEMORY UNIT |