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- NSN 6615-01-125-6581
6615-01-125-6581
Description: Displacement Gyroscope
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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.)
6615-01-125-6581 Properties
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NSN:6615-01-125-6581
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Description:Displacement Gyroscope
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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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Overall Length:6.600 inches
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Overall Height:4.000 inches
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Overall Width:4.000 inches
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Current Type:Ac
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Unit Type:Vertical
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Wheel Power Method:Electric
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Axis Displacement Limitation In Deg:Porm 82 degrees for pitch axis, 360 degrees roll attitude sensing
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Voltage In Volts:115.0
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Phase:Single
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Special Features:Mounting data - per scs-413: design activity data: jet electronics and technology, inc. Fscm 25583, p/n 501-1332-01; aircraft installed. Funct desc: gyroscope develops electrical signals representative of aircraft attitude through 360 degrees roll and +/-82 degrees pitch
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Frequency In Hertz:400.0
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Supplementary Features:Consists of an electrically driven rotor situated in a gimbal arrangement to provide accurate angular displacement measurement is referenced to vertical by means of electrical erection is vibration isolated. Item part of: ch-47 helicopter item used with: aru-12/a indicator intchg stmt: two-way interchangeable. Except by maintenance parts cn-811/asn & cn-811a/asn