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1560-01-455-6004
Aircraft Structural Component Support
1560014556004 014556004 3341662-9
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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Related Documents 1560-01-455-6004 2+ Documents (More...)
United States (US) 4. 1560-01-455-6004 Marketplace Restrictions Approved Sources Datasheet Management
RQST NE Updated Every Day 1560-01-455-6004 RQST Updated Every Day 1560-01-455-6004 RQST NE Related Documents
Restrictions 1560-01-455-6004
1560-01-455-6004 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 1560-01-455-6004
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 1560-01-455-6004
- United Kingdom (ZK01)
- Effective Date:
- 1 May 1998
Approved Sources 1560-01-455-6004
- Part Number
- Manufacturer
- Status
- 3341662-9
- Manufacturer
- 98897 - Lockheed Martin Corp (Active)
- Primary Buy
- Primary Buy
Datasheet 1560-01-455-6004
- Characteristic
- Specifications
- FIIG
- Specifications
- A11800
- Material [MATT]
- Aluminum Alloy 2024
- Aircraft Location [CZDJ]
- Crew Compartment
- Aircraft Station Number [CZEJ]
- Fs182.5 To Fs212.0
- Side For Which Designed [BWJF]
- Right Side
- Aircraft Mission Design Series [CZEK]
- C-130J
- Overall Length [ABHP]
- 32.970 Inches Nominal
- Overall Width [ABMK]
- 0.880 Inches Nominal
- Hole Quantity [ASXK]
- 9
- Height [HGTH]
- 0.800 Inches Nominal
- Special Features [FEAT]
- Parts Included With Assembly: 4 Ms21059-3 Nuts, Nsn 5310-00-778-2655; 1Angle P/N 3341662-11
- End Item Identification [AGAV]
- Support Angle-Trim Panel For The C-130J Aircraft Crew Compartment Fuselage
- Part Name Assigned By Controlling Agency [CXCY]
- Support Angle-Trim Panel, Crew Compartment Fuselage Station 182.5 To 212.0 Right Side, Assembly
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Freight Information 1560-01-455-6004
1560-01-455-6004 has freight characteristics managed by the Bureau of Accounts.. 1560-01-455-6004 has a variance between NMFC and UFC when transported by rail and the description should be consulted.