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- NSN 1560-01-466-7749
1560-01-466-7749
Description: Aircraft Structural Plate
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.)
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5935-01-093-6390 Electrical Receptacle Connector
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MIL-A-8625 Aircraft Structural Plate
Spec. Type | Spec. | Color | Gloss | Size |
---|---|---|---|---|
Surface treatment document and classification | MIL-A-8625 |
Array Properties
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NSN:Array
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Description:Aircraft Structural Plate
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Shelf Life:N/A
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DEMIL:DEMIL/MLI
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UOM:--
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Overall Length:31.300 inches
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Overall Width:Between 4.970 inches and 5.030 inches
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Material Thickness:Between 0.570 inches and 0.630 inches
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Part Name Assigned By Controlling Agency:Strap
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Aircraft Location:Lower fuselage
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Aircraft Station Number:Fs1058
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Aircraft Mission Design Series:C-141
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Material:Aluminum alloy 7075
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Material Specification:Qq-a-250/12, t6 federal specification single material response
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Surface Treatment:Anodize and paint epoxy and paint
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Surface Treatment Specification:Mil-a-8625, typeii, class1 military specification 1st treatment response and mil-p-23377, typei, classc military specification 2nd treatment response and mil-c-85285, typei military specification 3rd treatment response