Product Details | AIRCRAFT STRUCTURAL COMPONENT SUPPORT

1560-01-206-2274 A device of various shapes to be permanently attached to the structure of an aircraft. It is designed to permanently mount and/or support an integral member, or group of members of the airframe in a proper position and bear the stress imposed by the components being supported. It may have mounting provisions, such as slots, holes, and/or attachments to facilitate installation. Excludes items which are primarily designed for dampening shock and/or vibration. Excludes BRACKET, ANGLE; BRACKET, DOUBLE ANGLE; BRACKET, SHELF; BRACKET, MOUNTING; BRACKET (1), STRUCTURAL COMPONENT, AIRCRAFT; and RADIUS BLOCK.

Part Alternates: 65C18770604, 65C18770-604, 1560-01-206-2274, 01-206-2274, 1560012062274, 012062274

Aircraft and Airframe Structural Components | Airframe Structural Components

Supply Group (FSG) NSN Assign. NIIN
15 16 APR 1985 01-206-2274

Cross Reference | NSN 1560-01-206-2274

Part Number Cage Code Manufacturer
65C18770-604 81205 THE BOEING COMPANY DBA BOEING

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Technical Data | NSN 1560-01-206-2274

Characteristic Specifications
MATERIAL NICKEL ALLOY
MATERIAL THICKNESS 0.063 INCHES NOMINAL

Restrictions/Controls & Freight Information | NSN 1560-01-206-2274

Category Code Description
Hazardous Material Indicator CodePThere is no information in the HMIS; however, the NSN is in an FSC in Table II of Federal Standard 313 and an MSDS may be required by the user. The requirement for an MSDS is dependent on a hazard determination of the supplier or the intended end use of the product
Demilitarization Code:BMunitions List Item - Mutilation (MUT) to the point of scrap required. (Formerly: Demilitarization not required. Trade Security Controls (TSCs) required at disposition.)
Precious Metals Indicator Code:AItem does not contain precious metal
Criticality Code:X The item does not have a nuclear hardened feature or any other critical feature such as tolerance, fit restriction or application.
Category Code Description
No Freight Information