Thank you for taking interest in Ge Aviation Systems Ltd part number 2870B4, which is listed with the NSN 6610-01-577-1829 and a product description of “Data Acquisition Unit.” In order to receive procurement options on this particular listing, we ask that you fill out and submit the form provided below with as much information as you can concerning your needs. By supplying our staff with key details on your desired quantity, pricing target, and expedited fulfillment timeframe, we can respond with a quote that has been specifically tailored to your unique specifications. We also ask that you make us aware of any restrictions that you may have as soon as possible, such as if you have a time constraint or are seeking unlisted items.
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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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