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1560-01-476-5183

Aircraft Structural Panel

1560014765183 014765183 3352111-7

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

1560-01-476-5183 PANEL,STRUCTURAL,AIRCRAFT 1560014765183 014765183

Managed by United States
NSN Created on 14 Jul 2000
Data Last Changed
May 2023
NATO Update Count
3
NATO Data Quality
1560-01-476-5183 PANEL,STRUCTURAL,AIRCRAFT 1560014765183 014765183 1/1
1560-01-476-5183 Photo 1/1

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Aircraft Structural Panel 1560014765183 3352111-7 A preformed item of various shapes, and contours,
vendors Request Updated Every Day 1560-01-594-6020 https//www.nsnlookup.com /fsg-15/fsc-1560/us 1560-01-476-5183
Aircraft Structural Panel 1560014765183 -476-5183 Aircraft Structural Panel 1680997487292 748-7292
Aircraft Structural Panel 1680997703989 770-3989 1560-01-585-2925 1560-00-394-6392 1560-01-594-6020 1560-01-476-5183
Aircraft Structural Panel 1560014765183 0814 Aircraft Structural Panel 1560000720814 Aircraft Structural
Panel 1680997013702 701-3702 1560-01-585-2925 -394-6392 1560-01-594-6020 1560-01-476-5183 Aircraft Structural
Panel 1680997487292 748-7292 1560-01-585-2925 -394-6392 1560-01-594-6020 1560-01-476-5183 Aircraft Structural
1560000720814 Panel 1680997013702 701-3702 1560-01-585-2925 1560-00-394-6392 1560-01-594-6020 1560-01-476-5183
-01-477-1188 Panel 1680997487292 748-7292 1560-01-585-2925 1560-00-394-6392 1560-01-594-6020 1560-01-476-5183
-01-477-1188 Panel 1680997703989 770-3989 1560-01-585-2925 1560-00-394-6392 1560-01-594-6020 1560-01-476-5183
Aircraft Structural Panel 1680997013702 701-3702 1560-01-585-2925 1560-00-394-6392 1560-01-594-6020 1560-01-476-5183
Aircraft Structural Panel 1680997487292 748-7292 1560-01-585-2925 1560-00-394-6392 1560-01-594-6020 1560-01-476-5183
Aircraft Structural Panel 1680997703989 770-3989 1560-01-585-2925 1560-00-394-6392 1560-01-594-6020 1560-01-476-5183

1560-01-476-5183 Demil Restrictions 1560-01-476-5183

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

1560-01-476-5183 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 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.

1560-01-476-5183 HTS and ScheduleB Import and Export 1560-01-476-5183

1560-01-476-5183 End Users End Users 1560-01-476-5183

United Kingdom (ZK01)
Effective Date:
1 Jul 2000

1560-01-476-5183 Manufacturers Approved Sources 1560-01-476-5183

1560-01-476-5183 Technical Data Datasheet 1560-01-476-5183

Characteristic
Specifications
FIIG
A11700
End Item Identification [AGAV]
C130j Aircraft

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1560-01-476-5183 Freight Data Freight Information 1560-01-476-5183

1560-01-476-5183 has freight characteristics managed by the Bureau of Accounts.. 1560-01-476-5183 has a variance between NMFC and UFC when transported by rail and the description should be consulted.