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- NSN 2840-01-458-2759
2840-01-458-2759
Description: Aircraft Gas Turb Compressor Hub
Price Quote
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We are commited to quality and satisfaction as a certified supplier in the aerospace and military industries.
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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.)
2840-01-458-2759 Properties
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NSN:2840-01-458-2759
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Description:Aircraft Gas Turb Compressor Hub
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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:12.726 inches
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Diameter:Between 16.741 inches and 16.743 inches
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End Application:Tf-33 aircraft gas turbine engine
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Design Type:Axial compressor
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Criticality Code Justification:Feat and abhp and abmz and czbj
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Engine Section Location:Compressor
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Special Features:P/n not to be procured; p/n taken off engine and put into supply then reworked up to p/n 753538 (01-160-6504); depending on repair it will get assigned a different p/n; if this p/n has cracks in the tie rod holes will be assigned p/n 784473; if this item has nocracks, is reworked to p/n 774659
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Material:Steel
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Material Specification:Ams6415 assn standard single material response
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Reference Data And Literature:T.O. 2j-tf33-34, fig 6, ind 51

