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1560-01-425-2690
Aircraft Structural Panel
1560014252690 014252690 351888-4
A preformed item of various shapes, and contours, which may have a sandwich or honeycomb core bonded to a metallic or nonmetallic facing material. It is used to enclose integral portions of the fuselage or to form partitions or sections within a wing, empennage, fuselage, nacelle or crew compartment. It may have mounting provisions such as predrilled holes to facilitate installation, but will have no items attached to it except bracket (s) or other securing devices to accommodate its own mounting or support. It may be mounted by means of fasteners, bonding or welding. Excludes PANEL, INTERIOR LINING, AIRCRAFT; COVER ACCESS; COVER, ACCESS, AIRCRAFT; FLOOR (1), AIRCRAFT; CORE MATERIAL, CELLULAR, STRUCTURAL. View more Aircraft Structural Panel
January 2023
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Related Documents 1560-01-425-2690 2+ Documents (More...)
RQST NE Updated Every Day 1560-01-425-2690 RQST Updated Every Day 1560-01-425-2690 RQST NE Restrictions
1560-01-425-2690 DEMIL: A | DEMILI : | CRITICALITY : X | HMIC : P | PMIC : A | EDC: A | ADPEC : 0 1560
Aircraft Structural Panel 1560014252690 day Upgrade your Account Upgrade 1560-01-425-2690Aircraft
Structural Panel1560014252690 014252690 351888 https//www.nsnlookup.com /fsg-59/fsc-5925/it 5925-15-
Restrictions 1560-01-425-2690
1560-01-425-2690 is a Aircraft Structural Panel that does not have a nuclear hardened feature or any other critical feature such as tolerance, fit restriction or application. This item is considered a low risk when released from the control of the Department of Defense. The item may still be subject to the requirements of the Export Administration Regulations (EAR) and the Code of Federal Regulations (CFR). 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 1560-01-425-2690
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 1560-01-425-2690
- New Zealand (ZE01)
- Effective Date:
- 1 Feb 1996
Approved Sources 1560-01-425-2690
- Part Number
- Manufacturer
- Status
- 351888-4
- Manufacturer
- 98897 - Lockheed Martin Corp (Active)
- Primary Buy
- Primary Buy
Datasheet 1560-01-425-2690
- Characteristic
- Specifications
- FIIG
- Specifications
- A11700
- Material [MATT]
- Aluminum Alloy
- Material Document And Classification [MDCL]
- Qq-A-250/3 Fed Spec Single Material Response
- Aircraft Location [CZDJ]
- Trailing Edge,Outer Wing Flap Sta100.180 To 173.19 Rh
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Freight Information 1560-01-425-2690
1560-01-425-2690 has freight characteristics managed by New Zealand.. 1560-01-425-2690 has a variance between NMFC and UFC when transported by rail and the description should be consulted.