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1680-01-398-5885

Aircraft Seat Cushion

1680013985885 013985885 103234-2 103234-1

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

1680-01-398-5885 CUSHION,SEAT,AIRCRAFT 1680013985885 013985885

Managed by United States
NSN Created on 5 Nov 1994
Data Last Changed
January 2023
NATO Update Count
5
NATO Data Quality
1680-01-398-5885 CUSHION,SEAT,AIRCRAFT 1680013985885 013985885 1/1
NSN 1680-01-398-5885 (Generic Image) 1/1

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1680-01-398-5885 Related Documents Related Documents 1680-01-398-5885 5+ Documents (More...)

| RNVC: 2 | DAC: 6 25 May 2011 1680-01-608-8658 https//www.nsnlookup.com /fsg-16/fsc-1680/us 1680-01-398-5885
Aircraft Seat Cushion 1680013985885 013985885 https//www.nsnlookup.com /nato/nato-stock-numbers
8405-17-112-2895 8405171122895 171122895 is multipurpose trousers for work and casual wear, including athletic activities, exercising, or the like. excludes trousers worn for dress and those designed for specific sports.
8405-17-110-8059 8405171108059 171108059 is a jacket for males past the age of physical maturity.
8405-17-110-8065 8405171108065 171108065 is a jacket for males past the age of physical maturity.
8405-17-110-8067 8405171108067 171108067 is a jacket for males past the age of physical maturity.

1680-01-398-5885 Demil Restrictions 1680-01-398-5885

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

1680-01-398-5885 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. 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.

1680-01-398-5885 HTS and ScheduleB Import and Export 1680-01-398-5885

1680-01-398-5885 End Users End Users 1680-01-398-5885

US Air Force (FBB5)
Effective Date:
1 May 2000
Former MOE Rule:
FECX
Canada (ZC01)
Effective Date:
1 Mar 2011
NATO Maintenance and Supply Agency (ZX01)
Effective Date:
1 Jan 2014

1680-01-398-5885 Manufacturers Approved Sources 1680-01-398-5885

1680-01-398-5885 Technical Data Datasheet 1680-01-398-5885

Characteristic
Specifications
FIIG
T312-A
Special Features [FEAT]
Cushion Assembly,Seat Pan-Crew Rest Seat
End Item Identification [AGAV]
C-17 Globemaster Aircraft

1680-01-398-5885 Management Data Management Data 1680-01-398-5885

Effective Date
Organization
Unit of Issue
Unit Price
Qty Unit Pack
Nov 2018
Department of the Air Force (DF)
EA
Subscribe

Air Force Air Force

Budget:
S
57X3010 - Aircraft Replenishment Spares
Aggregation Code:
BA
C-17 PROGRAM
Price Validation Code:
N
The current standard price in Catalog Management Data (CMD) has not analyzed or coded for LP/LM.
The price has not been analyzed or reviewed for accuracy.
ZOP or Standard price challenges are permissible but must be supported with adequate justification. However, if coded for Local Purchase (LP) or Fabrication/Manufacture as indicated with an (LM) Acquisition Advice Code of ā€œLā€ or ā€œFā€, then it must be evaluated locally where purchased or fabricated.
Expendability
Recoverability
Repairability:
N
Expendable. Condemn at User. Stock Fund (except Munitions).

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1680-01-398-5885 Freight Data Freight Information 1680-01-398-5885

1680-01-398-5885 has freight characteristics.. 1680-01-398-5885 has a variance between NMFC and UFC when transported by rail and the description should be consulted.