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- NSN 6610-01-577-1829
6610-01-577-1829
Description: Data Acquisition Unit
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Export Restrictions
Any part(s) quoted or sold by MilSpec.parts and re-sold (to a third party) CANNOT be sold to a USA embargoed country, company, entity, or person(s). Depending on the ECCN, these commodities may require export license or exception. Diversion contrary to U.S. law is prohibited. Unless otherwise noted, this sale, order or quote may include Munitions List Items (MLI) or Commerce Controlled List Items (CCLI). MLI/CCLI property is controlled by the US Government and in many cases cannot be transferred (exported, sold or given) to a foreign country, a non-US Citizen/National or a non- Permanent US Resident without a valid State/Commerce Department export authorization. It is the responsibility of (the Purchaser) to determine what the applicable requirements may be, to obtain all necessary authorizations, licenses or approvals and are subject to both review and acceptance by MilSpec.parts. The use, disposition, export and re-export of the property covered or included in this sale, order or quote is subject to the provisions of law referenced in End-Use Certificate DLA form 1822, DEC 2001, including, but not limited to, the Arms Export Control Act (22 USC 2751 et seq.); Export Administration Act of 1979 (50 USC App. 2401 et seq.) as contained under Executive Order 12924; International Traffic in Arms Regulations (22 CFR 120 et seq.); Export Administration Regulations (15 CFR 730 et seq.); Foreign Assets Control Regulations (31 CFR 500 et seq.) and the Espionage Act (18 USC 793 et seq.)
6610-01-577-1829 Properties
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NSN:6610-01-577-1829
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Description:Data Acquisition Unit
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Shelf Life:N/A
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DEMIL:DEMIL/MLI
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UOM:1 EA
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Mounting Type:Rack
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Direct Current Voltage Rating In Volts:28.0
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End Application:C-17 aircraft
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Unpackaged Unit Length:7.280 inches
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Unpackaged Unit Width:6.230 inches
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Unpackaged Unit Height:7.030 inches
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Power Source:External
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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
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Criticality Code Justification:Agav
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Part Name Assigned By Controlling Agency:Recorder-reproducer set, signal data
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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
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Reference Data And Literature:To 1c-17a-4-2 & jetdas data
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Relationship To Similar Equipment:Contains one additional four channel mil-std-1553 interface circuit card assembly than the -003 version
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Type/model Designation:Ro-626/a
