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1560-01-125-9481

Aircraft Structural Component Web

1560011259481 011259481 53-11041-38

An item designed as a principal member of various primary structures within an aircraft. It provides strength, rigidity and the like while maintaining the proper dimensional distances as required. It may include holes for mounting and/or joining to other items to form an assembly. View more Aircraft Structural Component Web

1560-01-125-9481 WEB,STRUCTURAL COMPONENT,AIRCRAFT 1560011259481 011259481

Managed by United States
NSN Created on 2 Feb 1982
Data Last Changed
January 2023
NATO Update Count
9
NATO Data Quality
1560-01-125-9481 WEB,STRUCTURAL COMPONENT,AIRCRAFT 1560011259481 011259481 1/1
NSN 1560-01-125-9481 (Generic Image) 1/1

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1560-01-125-9481 Related Documents Related Documents 1560-01-125-9481 1+ Documents (More...)

53-11041-38 An item designed as a principal member of various primary structures within an aircraft.
RQST NE Updated Every Day 1560-01-125-9481 RQST Updated Every Day 1560-01-125-9481 RQST NE Restrictions
1560-01-125-9481 DEMIL: B | DEMILI : | CRITICALITY : X | HMIC : P | PMIC : A | EDC: | ADPEC : 0 1560

1560-01-125-9481 Demil Restrictions 1560-01-125-9481

DEMIL: B | DEMILI: | CRITICALITY: X | HMIC: P | PMIC: A | EDC: | ADPEC: 0

1560-01-125-9481 is a Aircraft Structural Component Web that does not have a nuclear hardened feature or any other critical feature such as tolerance, fit restriction or application. This item is a US Munitions List Item and must be mutilated to scrap. 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.

1560-01-125-9481 HTS and ScheduleB Import and Export 1560-01-125-9481

1560-01-125-9481 End Users End Users 1560-01-125-9481

Germany (ZG01)
Effective Date:
1 Apr 1991

1560-01-125-9481 Manufacturers Approved Sources 1560-01-125-9481

1560-01-125-9481 Technical Data Datasheet 1560-01-125-9481

Characteristic
Specifications
FIIG
A11800
Aircraft Mission Design Series [CZEK]
F-4
Aircraft Location [CZDJ]
Speed Brake Closure, Forward
Material Document And Classification [MDCL]
Mil-T-9046 Mil Spec Single Material Response
Special Features [FEAT]
Matl: Titanium Aly Gal-4V;Comp C Type Iii Cond Annealed

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1560-01-125-9481 Freight Data Freight Information 1560-01-125-9481

1560-01-125-9481 has freight characteristics.. 1560-01-125-9481 has a variance between NMFC and UFC when transported by rail and the description should be consulted.

1560-01-125-9481 Packaging Data Packaging Data 1560-01-125-9481

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
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Unit Pack Level (Packaged)

Quantity per Pack
Unit Size
Unit Weight
Unit Cube
Preservation Method
Cleaning/Drying
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--
--
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Physical Protection
Any Suitable Process
Preservation Material
Wrapping Material
Cushioning/Dunnage
Cushioning Thickness
Container
Special Marking
No Requirement
No Requirement
PPP-C-1797, Polypropylene Foam Cushioning
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MIL-DTL-117, Type III, Class B, Style 2, Heavy Duty, Waterproof, Transparent Bag
No special marking

Intermediate Pack Level

Quantity of Unit Packs
Container
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