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- NSN 1560-01-527-9170
1560-01-527-9170
Description: Aircraft Door Hinge
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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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MIL-L-81352 Aircraft Door Hinge
Spec. Type | Spec. | Color | Gloss | Size |
---|---|---|---|---|
Surface treatment document and classification | MIL-L-81352 |
Array Properties
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NSN:Array
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Description:Aircraft Door Hinge
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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:3.390 inches
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Overall Width:1.484 inches
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Aircraft Location:Fus-midsection-entrance door-interconnect
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Aircraft Mission Design Series:C-2a-a20
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Special Features:Arm, having 1.500 inch diameter loop at bottom end, and having two drilled through holes (one wall only) of 0.127 to 0.133 inches in diameter located at perpendicullar planes of loop spaced 0.672 inches apart; top portion of arm has two parallel fingers each with a 0.2497 to 0.2507 ream hole diameter for close tolerance fit
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Material:Aluminum alloy
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Material Specification:Qq-a-200/2 federal specification single material response or qq-a-225/4 federal specification single material response
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Surface Treatment:Paint and primer epoxy-polyamide
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Surface Treatment Specification:Mil-l-81352 comp g military specification 1st treatment response and mil-p-23377 type 1 military specification 2nd treatment response