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- NSN 2840-01-460-8957
2840-01-460-8957
Description: Aircraft Gas Turbi Turbine Frame
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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.)
2840-01-460-8957 Properties
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NSN:2840-01-460-8957
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Description:Aircraft Gas Turbi Turbine Frame
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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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Outside Diameter:33.556 inches
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End Application:F110-ge-129 aircraft gas turbine eng
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Number Of Variable Guide Vanes:10
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Special Features:This change addresses cracks and rivet breakage in the turbine frame fwd outer liner supports; root cause is a lack of thermal growth capability, which causes the support to crack and load the rivets. Changes will increase sheet metal hole size, spacers with longer stem and larger washers
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Reference Data And Literature:T.O. 2j-f110-4, fig 79, ind 15 orfig 81, ind 19

