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- NSN 1620-00-620-7642
1620-00-620-7642
Description: Landing Gear Drag Link
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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.)
1620-00-620-7642 Properties
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NSN:1620-00-620-7642
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Description:Landing Gear Drag Link
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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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End Application:Main landing gear
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Aircraft For Which Designed:B-52
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Criticality Code Justification:Feat
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Part Name Assigned By Controlling Agency:Link, tripod, drag strut
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Special Features:Make from 5-36475-2 forging, testja81205-5-36035-3, finish f-1.200 or f-1.205 opt'l after plating thickness.0003 mil., heat treat 150, 000-200, 000 psi, holes must be located to match the respective maching holes in 5-68441, 5-35964, &5-35423 such that assembly of the outer cylinder and tripod links is assured, bake after plating, magnetic inspection per mil-i-6868 all machoined surfaces exc.As noted
