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1560-00-558-4802
Aircraft Structural Component Support
1560005584802 005584802 3306943-3
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
January 2023
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SUPPORT,STRUCTURAL COMPONENT,AIRCRAFT 8 EA NS Request Quotation Updated Every Day 1560-00-558-4802
RQST NE Updated Every Day 1560-00-558-4802 RQST Updated Every Day 1560-00-558-4802 RQST NE Restrictions
Restrictions 1560-00-558-4802
1560-00-558-4802 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. 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.
Import and Export 1560-00-558-4802
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 1560-00-558-4802
- US Air Force (FGG5)
- Effective Date:
- 1 Apr 1991
- US Navy (N9FG)
- Effective Date:
- 1 Apr 1991
Approved Sources 1560-00-558-4802
- Part Number
- Manufacturer
- Status
- 3306943-3
- Manufacturer
- 98897 - Lockheed Martin Corp (Active)
- Primary Buy
- Primary Buy
Datasheet 1560-00-558-4802
- Characteristic
- Specifications
- FIIG
- Specifications
- A11800
- Aircraft Location [CZDJ]
- Web Splice,Front Beam,Outer Wing Station 158.40 And 201.60
- Aircraft Mission Design Series [CZEK]
- C-130
- Material Document And Classification [MDCL]
- Mil-S-5059,Comp 301 1/2H Mil Spec Single Material Response
- Material Thickness [ABPX]
- 0.032 Inches Nominal
- Material [MATT]
- Steel Comp 301
- Overall Length [ABHP]
- 5.000 Inches Nominal
- Overall Width [ABMK]
- 3.000 Inches Nominal
Management Data 1560-00-558-4802
Navy
- Cognizance:
- 9F
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Freight Information 1560-00-558-4802
1560-00-558-4802 has freight characteristics managed by the General Services Administration (GSA).. 1560-00-558-4802 has a variance between NMFC and UFC when transported by rail and the description should be consulted.