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1560-01-497-5366
Aircraft Structural Panel
1560014975366 014975366 17P2A6015-53
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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United States (US) 4. 1560-01-497-5366 Marketplace Restrictions Approved Sources Datasheet Management
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Restrictions 1560-01-497-5366
IUID Required
1560-01-497-5366 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.
Import and Export 1560-01-497-5366
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 1560-01-497-5366
- US Air Force (FBB4)
- Effective Date:
- 1 May 2002
Approved Sources 1560-01-497-5366
- Part Number
- Manufacturer
- Status
- 17P2A6015-53
- Manufacturer
- 88277 - The Boeing Company (Active)
- Primary Buy
- Primary Buy
Datasheet 1560-01-497-5366
- Characteristic
- Specifications
- FIIG
- Specifications
- A11700
- Material [MATT]
- Plastic Polyamide And
- Material [MATT]
- Plastic Aramid
- Material Document And Classification [MDCL]
- Dms1974-2-2B-3 Mfr Ref 1St Material Response And
- Material Document And Classification [MDCL]
- Dms2288-2-2D Mfr Ref 2Nd Material Response And
- Material Document And Classification [MDCL]
- Dms2288-3-4E Mfr Ref 3Rd Material Response
- Surface Treatment [SFTT]
- Primer Epoxy-Polyamide
- Surface Treatment Document And Classification [STDC]
- Mil-P-23377 Mil Spec 1St Treatment Response And
- Surface Treatment Document And Classification [STDC]
- Mil-F-18264 Mil Spec 2Nd Treatment Response
- Fabrication Method [AARN]
- Honeycomb And
- Fabrication Method [AARN]
- Laminated And
- Fabrication Method [AARN]
- Composite
- Aircraft Location [CZDJ]
- Wing To Fuselage Fillet
- Aircraft Station Number [CZEJ]
- Y981.500 To Y1045.750
- Side For Which Designed [BWJF]
- Left Side
- Aircraft Mission Design Series [CZEK]
- C-17A
- Special Features [FEAT]
- Used On The Following Nha:17P2a6015-1, -501, -503, -505, -507, -509 And -521 Configurations
- Design Control Reference Or Manufacturers Code [SR-5]
- Design Control Reference Or Manufacturers Code [SR-5]
- 88277
- Design Control Reference Or Manufacturers Code [SR-5]
- 17P2a6015-53
Management Data 1560-01-497-5366
- Effective Date
- Organization
- Unit of Issue
- Unit Price
- Qty Unit Pack
- Unit of Issue
- Oct 2005
- Department of the Air Force (DF)
- EA
- Subscribe
- 1
- EA
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Freight Information 1560-01-497-5366
1560-01-497-5366 has freight characteristics.. 1560-01-497-5366 has a variance between NMFC and UFC when transported by rail and the description should be consulted.