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- NSN 6930-00-907-1759
6930-00-907-1759
Description: Instrument And Flight Di Trainer
Price Quote
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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.)
6930-00-907-1759 Properties
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NSN:6930-00-907-1759
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Description:Instrument And Flight Di Trainer
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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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Frequency In Hertz:Between 60.0 and 400.0
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Installation Design:Mobile
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Ac Operating Voltage Rating In Volts:Between 115.0 and 208.0
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Power Source:Ac
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Alternating Current Usage:Required
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Training Phase:Operation and maintenance of the air vehicle
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Phase:Three
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Special Features:Dwg name, trainer, flight director system, aircraft; direct cirrent, 28v, required; length, 84 in; width, 42in; height; major components c/o, rate of turn sensor, tru-2a/a; gyro, md-1; rate switching gyro, mc-1; horizontal situation indicator aqu-2/a; attitude director indicator aru-28/a; computer cpu-27/a; special features, the silhouette shall be supported by a one-piece column and universal action type of ball joint assembly, pitch and roll movement of the silhouette shall be restricted to plus and minus 20 degrees; the control console shall not extend above the horizontal base of the silhouette; the compass simulator shall be incorporated into the base of the support column; dd61 n., usaf-65-21
