| Part Number: 17P1E1138 | Manufacturer: Boeing Company The |
| NSN : 6610-01-577-1829 (6610015771829) | Item Name : data acquisition unit |
| CAGE Code: 88277 | FSC : 6610 Flight Instruments |
| NIIN : 01-577-1829 (015771829) | FSG : 66 Instruments and Laboratory Equipment |
| Country: USA | NCB Code: 01 |
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| MRC | Criteria | Characteristic |
|---|---|---|
| AJAF | Unpackaged Unit Length | 7.280 NOMINAL INCHES |
| AJAG | Unpackaged Unit Width | 6.230 NOMINAL INCHES |
| RTSE | Relationship To Similar Equipment | CONTAINS ONE ADDITIONAL FOUR CHANNEL MIL-STD-1553 INTERFACE CIRCUIT CARD ASSEMBLY THAN THE -003 VERSION |
| AJAH | Unpackaged Unit Height | 7.030 INCHES NOMINAL |
| FTLD | 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 |
| ACUR | Direct Current Voltage Rating In Volts | 28 |
| TMDN | Type/Model Designation | RO-626/A |
| CRTL | Criticality Code Justification | AGAV |
| AAXX | Mounting Type | RACK |
| MRC | Decoded Requirement | Clear Text Reply |
| AXQH | 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 |
| RDAL | Reference Data And Literature | TO 1C-17A-4-2 AND JETDAS DATA |
| AGAV | End Item Identification | C-17 AIRCRAFT |
| AWZJ | Power Source | EXTERNAL |
| CXCY | Part Name Assigned By Controlling Agency | RECORDER-REPRODUCER SET,SIGNAL DATA |
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