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- NSN 1560-01-113-7017
1560-01-113-7017
Description: Aircraft Former
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.)
More MIL-T-7046 Parts
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1560-01-488-5355 Air Structural Component Bracket
MIL-T-7046 Bracket
MIL-T-7046 Aircraft Former
Spec. Type | Spec. | Color | Gloss | Size |
---|---|---|---|---|
Material document and classification | MIL-T-7046 |
Array Properties
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NSN:Array
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Description:Aircraft Former
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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:14.650 inches
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Overall Width:3.350 inches
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Material Thickness:0.080 inches
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Side For Which Designed:Right side
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Criticality Code Justification:Feat
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Aircraft Location:Web assembly, speed brake closure forward
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Aircraft Mission Design Series:F-4e
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Special Features:Do not use cadmium plated tools on this item
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Material:Titanium alloy
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Material Specification:Mil-t-7046, type 3, cond annealed, comp c military specification single material response