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1680-01-657-9512
Aircraft Seat Cushion
1680016579512 016579512 871517-403
A molded foam rubber, one-piece, fabric-covered seating accommodation designed to upholster the bottom frame of an aircraft seat. It may include slide or snap-type fasteners for installation, seat cover removal, closure of inspection data pocket, and the like. Excludes CUSHION ASSEMBLY, SEAT AND BACK, AIRCRAFT; CUSHION, SEAT, PARACHUTE HARNESS; CUSHION, SEAT, AIRCRAFT SURVIVAL; and CUSHION, SEAT-SURVIVAL KIT, AIRCRAFT. View more Aircraft Seat Cushion
January 2023
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Marketplace 1680-01-657-9512
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Related Documents 1680-01-657-9512 1+ Documents (More...)
United States (US) 4. 1680-01-657-9512 Marketplace Restrictions Approved Sources Datasheet Management
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Restrictions 1680-01-657-9512
1680-01-657-9512 is a Aircraft Seat Cushion that does not have a nuclear hardened feature or any other critical feature such as tolerance, fit restriction or application. Demilitarization of this item has been confirmed and is not currently subject to changes. 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 is not suspected to be hazardous. This item does not contain a precious metal.
Import and Export 1680-01-657-9512
- Schedule B
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- HTS Code
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End Users 1680-01-657-9512
- United Kingdom (ZK01)
- Effective Date:
- 1 Sep 2016
Approved Sources 1680-01-657-9512
- Part Number
- Manufacturer
- Status
- 871517-403
- Manufacturer
- 29780 - Mag Aerospace Industries, Llc (Active)
- Primary Buy
- Primary Buy
Datasheet 1680-01-657-9512
- Characteristic
- Specifications
- FIIG
- Specifications
- T312-A
- Part Name Assigned By Controlling Agency [CXCY]
- Cushion Assembly,Bottom
- Supplementary Features [SUPP]
- Foam,Non-Flotation
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Freight Information 1680-01-657-9512
1680-01-657-9512 has freight characteristics.. 1680-01-657-9512 has a variance between NMFC and UFC when transported by rail and the description should be consulted.