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1680-01-486-1341
Aircraft Interior Lining Panel
1680014861341 014861341 17P9B3125-528
A preformed metallic/nonmetallic item specifically designed for mounting on the inside of the fuselage of an aircraft. It is of a special size, shape, and thickness to conform to the contour of the aircraft. It conceals cavities, controls, tubing, wiring and the like, as well as provides a sound barrier. Pockets, trays or shelves may be included. Excludes: PANEL, STRUCTURAL, AIRCRAFT. View more Aircraft Interior Lining Panel
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Related Documents 1680-01-486-1341 1+ Documents (More...)
United States (US) 4. 1680-01-486-1341 Marketplace Restrictions Approved Sources Datasheet Management
RQST NE Updated Every Day 1680-01-486-1341 RQST Updated Every Day 1680-01-486-1341 RQST NE Related Documents
Restrictions 1680-01-486-1341
1680-01-486-1341 is a Aircraft Interior Lining 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 is not suspected to be hazardous. This item does not contain a precious metal.
Import and Export 1680-01-486-1341
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 1680-01-486-1341
- US Air Force (FBB5)
- Effective Date:
- 1 Jun 2001
Approved Sources 1680-01-486-1341
- Part Number
- Manufacturer
- Status
- 17P9B3125-528
- Manufacturer
- 88277 - The Boeing Company (Active)
- Primary Buy
- Primary Buy
Datasheet 1680-01-486-1341
- Characteristic
- Specifications
- FIIG
- Specifications
- A11700
- Material [MATT]
- Plastic And
- Material [MATT]
- Glass Fiber
- Material Document And Classification [MDCL]
- Dms2240 Mfr Ref Single Material Response
- Surface Treatment [SFTT]
- Paint Polyurethane
- Surface Treatment Document And Classification [STDC]
- Dps4.50-153 Mfr Ref Single Treatment Response
- Fabrication Method [AARN]
- Molded
- Aircraft Location [CZDJ]
- Center Fuselage
- Aircraft Mission Design Series [CZEK]
- C-17
- Overall Length [ABHP]
- 26.030 Inches Nominal
- Thickness [ABNM]
- 0.500 Inches Nominal
- Special Features [FEAT]
- Manufacturer Suggested Name-Panelassembly, Support-Side, Catwalk; Nha 17P9b3121
- 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]
- 17P9b3125-528
Management Data 1680-01-486-1341
- Effective Date
- Organization
- Unit of Issue
- Unit Price
- Qty Unit Pack
- Unit of Issue
- Aug 2005
- Department of the Air Force (DF)
- EA
- Subscribe
- 1
- EA
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Freight Information 1680-01-486-1341
1680-01-486-1341 has freight characteristics.. 1680-01-486-1341 has a variance between NMFC and UFC when transported by rail and the description should be consulted.