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1560-01-355-4256

Aircraft Structural Component Support

1560013554256 013554256 17P6W8225-1 17P6W8225-501 17P6W8225-505 17P6W8225-503

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

1560-01-355-4256 SUPPORT,STRUCTURAL COMPONENT,AIRCRAFT 1560013554256 013554256

Managed by United States
NSN Created on 17 Mar 1992
Data Last Changed
January 2023
NATO Update Count
2
NATO Data Quality
1560-01-355-4256 SUPPORT,STRUCTURAL COMPONENT,AIRCRAFT 1560013554256 013554256 1/1
NSN 1560-01-355-4256 (Generic Image) 1/1

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1560-01-355-4256 Related Documents Related Documents 1560-01-355-4256 2+ Documents (More...)

Documents 1560-01-566-5236 2+ Documents ( More... ) https//www.nsnlookup.com /fsg-15/fsc-1560/us 1560-01-355-4256
structural component, aircraft; and radius block. https//www.nsnlookup.com /fsg-15/fsc-1560/us 1560-01-355-4256
Aircraft Structural Component Support 1560-01-355-4256 1560013554256 013554256 is a device of various

1560-01-355-4256 Demil Restrictions 1560-01-355-4256

DEMIL: Q | DEMILI: 3 | CRITICALITY: N | HMIC: P | PMIC: A | EDC: | ADPEC: 0

IUID Required

1560-01-355-4256 is a Aircraft Structural Component Support This item has been confirmed as a Critical Munitions List Item or a Sensitive Commerce Control List Item and cannot be in the possession of any party anywhere in the World who is not an authorized NATO Government. Any other possessor of this item should mutilate it now as possession violates international and local laws. This item is a confirmed Commerce Control List Item (CCLI). 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.

1560-01-355-4256 HTS and ScheduleB Import and Export 1560-01-355-4256

1560-01-355-4256 End Users End Users 1560-01-355-4256

US Air Force (FBB5)
Effective Date:
1 Feb 2005
Former MOE Rule:
FGCX

1560-01-355-4256 Manufacturers Approved Sources 1560-01-355-4256

1560-01-355-4256 Technical Data Datasheet 1560-01-355-4256

Characteristic
Specifications
FIIG
A11800
Aircraft Location [CZDJ]
No.4 Actuator Spoiler
Aircraft Mission Design Series [CZEK]
C-17
Special Features [FEAT]
C/O 2 Brackets,1 Hinge,Misc Hardware

1560-01-355-4256 Management Data Management Data 1560-01-355-4256

Effective Date
Organization
Unit of Issue
Unit Price
Qty Unit Pack
Jan 2012
Department of the Air Force (DF)
EA
Subscribe
1
MOE
USC
Code
Statement
Order of Use
Jump To Code
Qty Per Assy
UOM
Technical Document
Quantative Expression
Department of the Air Force (DF)
F
F
When Exhausted Use 1560-01-566-5236
Department of the Air Force (DF)
I
F
When Exhausted Use 1560-01-566-5236

Air Force Air Force

Budget:
S
57X3010 - Aircraft Replenishment Spares
Aggregation Code:
BA
C-17 PROGRAM
Price Validation Code:
E
The current standard price is an estimated price.
Estimated Price challenges are allowed but follow procedures in para 60.b. (3) of section L of this manual.
This code will be changed to a P code upon notification of a contract price or this code will be changed to an updated code upon determination of a valid price.
Expendability
Recoverability
Repairability:
P
Expendable. Reparable. Condemn at Intermediate. Stock Fund (except Munitions).

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1560-01-355-4256 Freight Data Freight Information 1560-01-355-4256

1560-01-355-4256 has freight characteristics.. 1560-01-355-4256 has a variance between NMFC and UFC when transported by rail and the description should be consulted.