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- NSN 4920-01-020-8027
4920-01-020-8027
Description: Aircraft Co Test Set Subassembly
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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.)
4920-01-020-8027 Properties
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NSN:4920-01-020-8027
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Description:Aircraft Co Test Set Subassembly
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Shelf Life:N/A
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DEMIL:NO
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UOM:1 EA
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Overall Length:12.000 inches
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Overall Height:8.000 inches
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Overall Width:8.750 inches
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End Application:E-3a aircraft
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Part Name Assigned By Controlling Agency:Flight recorder/locator system simulator test adapter set
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Special Features:4ea type 509 6-volt battery power source
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Functional Description:Used during performance of unscheduled intermediate maintenance at the flightline to verify the dc parameter outputs while troubleshooting and fault isolating. The signal outputs from the egt and epr indicators, and fuel flow (ff) amplifier are required to exercise those channels of data recorded by the flight recorder/locator system. The output of the flight recorder/locator system is monitored by the data display monitor (ddu-4) as the input signal is varied from 0 to 5 volts dc. The signals are generated by operating engines or by providing a simulated voltage at the output of each indicator and the amplifier. The input impedance of the signal data converter between high and low is 150, 000 ohms (+o.1%)
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Entry Date:77-01-01
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Reference Data And Literature:T.O.1e-3a-2-23-1 communications system usaf section x11 and t.O.35-1-251-1

