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1560-01-359-2675

Aircraft Structural Component Support

1560013592675 013592675 17P8D8541-1

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. View more Aircraft Structural Component Support

Managed by United States

NSN Created on 1 Jun 1992

Data Last Changed
January 2023

NATO Update Count
7

NATO Data Quality

1560-01-359-2675 SUPPORT,STRUCTURAL COMPONENT,AIRCRAFT 1560013592675 013592675 1/1 — NSN 1560-01-359-2675 (Generic Image) 1/1

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Restrictions 1560-01-359-2675

IUID Required

1560-01-359-2675 is a Aircraft Structural Component Support that does not have a nuclear hardened feature or any other critical feature such as tolerance, fit restriction or application. Demilitarization of this item has been confirmed and is not currently subject to changes. This item is a US Munitions List or Commerce Control List Item which must be destroyed to prevent restoration or repair. Only authorized parties may possess this item. This item may be hazardous as it is in a Federal Supply Class for potentially hazardous items. A MSDS should be available from the supplier for the end user to evaluate any hazards. This item does not contain a precious metal.

Import and Export 1560-01-359-2675

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End Users 1560-01-359-2675

US Air Force (FBB4)
Effective Date:: 1 Aug 1999
Former MOE Rule:: FEE4; AMC 0 AMSC 0 AMSC P IMC E DSOR CN

Canada (ZC01)
Effective Date:: 1 Mar 2011

Approved Sources 1560-01-359-2675

Part Number
Manufacturer
Status
17P8D8541-1: 88277 - The Boeing Company (Active); Primary Buy; RNCC 3 RNVC 2 DAC 2

Datasheet 1560-01-359-2675

Characteristic
Specifications
FIIG: A11800
Aircraft Location [CZDJ]: Engine Nacelle
Aircraft Mission Design Series [CZEK]: C-17
Material [MATT]: Nickel Alloy
Material Document And Classification [MDCL]: Dms2075 Mfr Ref Single Material Response
Special Features [FEAT]: Support Assembly,Door,Blocker,Core Thrust Reverser

Management Data 1560-01-359-2675

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Effective Date: Organization; Unit of Issue; Unit Price; Qty Unit Pack
Oct 2018: Department of the Air Force (DF); EA; Subscribe; 1

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Freight Information 1560-01-359-2675

1560-01-359-2675 has freight characteristics.. 1560-01-359-2675 has a variance between NMFC and UFC when transported by rail and the description should be consulted.

Packaging Data 1560-01-359-2675

Responsible Activity
Packaging Data Source: Primary Inventory Control Activity (PICA); Packaging Data does not meet current MIL-STD-2073-1E

Item Pack Level (Unpackaged)

Item Size
Item Weight
Characteristics
Weight/Dimensions Category
Fragility
Item Preservation: 16.8" H x 13.7" W x 5.4" L; --; --; Over 10lb; Less than 85G; No Requirement

Unit Pack Level (Packaged)

Quantity per Pack
Unit Size
Unit Weight
Unit Cube
Preservation Method
Cleaning/Drying: 1; 31.0" H x 28.0" W x 15.0" L; --; --; --; Any Suitable Process

Preservation Material
Wrapping Material
Cushioning/Dunnage
Cushioning Thickness
Container
Special Marking: No Requirement; A-A-3174, Plastic Sheet, Polyolefin, 2mil; PPP-C-795, Cellular Plastic Film Cushioning; or A-A-3129, Open Cell Plastic Cushioning; or PPP-C-1797, Polypropylene Foam Cushioning; or A-A-59136, Polyethylene Foam Cushioning; --; PPP-B-1672, Type III, Telescoping Encapsulated Cushioning in Reusable Box; No special marking

Intermediate Pack Level

Quantity of Unit Packs
Container: --; No Requirement