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1660-01-619-9460

Aircraft Ejection Seat Oxygen System

1660016199460 016199460 380C330-3

An ejection seat / ejection seat harness mounted system which primarily provides the pilot with oxygen from main oxygen supply in normal flying conditions. In case of emergency such as ejection, damaged hoses, and the like, it provides the same function after disconnection or deprivation from main oxygen supply. It generally consists of an oxygen regulator, a connection box, an anti-G valve, hoses, fittings, emergency oxygen suit, and the like. Excludes OXYGEN SYSTEM,AIRCRAFT SURVIVAL KIT. View more Aircraft Ejection Seat Oxygen System

1660-01-619-9460 OXYGEN SYSTEM,EJECTION SEAT,AIRCRAFT 1660016199460 016199460

Managed by United States
NSN Created on 24 Jun 2013
Data Last Changed
January 2023
NATO Update Count
3
NATO Data Quality
1660-01-619-9460 OXYGEN SYSTEM,EJECTION SEAT,AIRCRAFT 1660016199460 016199460 1/1
NSN 1660-01-619-9460 (Generic Image) 1/1

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1660-01-619-9460 Related Documents Related Documents 1660-01-619-9460 5+ Documents (More...)

380C330-3 An ejection seat / ejection seat harness mounted system which primarily provides the pilot
RQST NE Updated Every Day 1660-01-619-9460 RQST Updated Every Day 1660-01-619-9460 RQST NE Related Documents
HTS Code End Users 1660-01-619-9460 Belgium (ZB01) Effective Date:1 Jun 2013 Approved Sources 1660-01
Ejection Seat Oxygen System 522-4255 1660-14-481-9409 www.nsnlookup.com /fsg-16/fsc-1660/us 1660-01-619-9460
1660-01-522-4255 1660-14-481-9409 502-3980 1660-99-353-1045 1660-01-473-2858 1660-14-481-4941 1660-01-619-9460
1660-01-522-4255 1660-14-481-9409 https//www.nsnlookup.com /fsg-16/fsc-1660/us 1660-01-619-9460
Seat Oxygen System -01-473-2858 Aircraft Ejection Seat Oxygen System 473-2858 1660-14-481-4941 1660-01-619-9460
1660-99-353-1045 Aircraft Ejection Seat Oxygen System www.nsnlookup.com /fsg-16/fsc-1660/us 1660-01-619-9460
Aircraft Ejection Seat Oxygen System System 473-2858 1660-14-481-4941 1660-01-619-9460 1660-01-
Aircraft Ejection Seat Oxygen System System 473-2858 1660-14-481-4941 1660-01-619-9460 1660-01-
522-4255 Related to 1660-01-502-3980 1660-99-353-1045 1660-01-473-2858 1660-14-481-4941 1660-01-619-9460
Oxygen System Related to 1660-01-473-2858 1660-99-353-1045 System 473-2858 1660-14-481-4941 1660-01-619-9460
1660-01-528-5726 1660-99-434-5266 1660-99-581-5867 https//www.nsnlookup.com /fsg-16/fsc-1660/us 1660-01-619-9460
Stock Numbers Related to 1660-99-581-5867 1660-99-353-1045 1660-01-473-2858 1660-14-481-4941 1660-01-619-9460

1660-01-619-9460 Demil Restrictions 1660-01-619-9460

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

1660-01-619-9460 is a Aircraft Ejection Seat Oxygen System 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 US Munitions List Item and must be mutilated to scrap. This item is not suspected to be hazardous. This item does not contain a precious metal.

1660-01-619-9460 HTS and ScheduleB Import and Export 1660-01-619-9460

1660-01-619-9460 End Users End Users 1660-01-619-9460

Belgium (ZB01)
Effective Date:
1 Jun 2013

1660-01-619-9460 Manufacturers Approved Sources 1660-01-619-9460

1660-01-619-9460 Technical Data Datasheet 1660-01-619-9460

Characteristic
Specifications
FIIG
A23800
End Item Identification [AGAV]
Ewwi
Special Features [FEAT]
Ewi-Tm-380 Ind 4
Part Name Assigned By Controlling Agency [CXCY]
Automate Relise Cable

1660-01-619-9460 Related Items NATO Stock Numbers Related to 1660-01-619-9460

1660-01-619-9460 Freight Data Freight Information 1660-01-619-9460

1660-01-619-9460 has freight characteristics.. 1660-01-619-9460 has a variance between NMFC and UFC when transported by rail and the description should be consulted.