7010-21-907-2018

Digital Computer System

7010219072018 219072018 MMD-988-09670 MBC675

A complete digital computer system, as defined by computer, digital, which includes the computer and all the associated peripheral hardware. May be a networked system or stand alone. Also, may or may not have satellite and/or global capabilities via built-in or add-on devices. View more Digital Computer System

7010-21-907-2018 COMPUTER SYSTEM,DIGITAL 7010219072018 219072018

Managed by Canada
NSN Created on 9 Jun 1990
Data Last Changed
January 2023
NATO Update Count
1
NATO Data Quality
7010-21-907-2018 COMPUTER SYSTEM,DIGITAL 7010219072018 219072018 1/1
NSN 7010-21-907-2018 (Generic Image) 1/1

7010-21-907-2018 Stock and Availability Marketplace 7010-21-907-2018

Need Help?
Request a Quotation from participating marketplace vendors
eBay Updated Every Day
7010-21-907-2018 RQST NE eBay
eBay Updated Every Day
7010-21-907-2018 RQST eBay
Amazon Updated Every Day
7010-21-907-2018 RQST NE Amazon

7010-21-907-2018 Related Documents Related Documents 7010-21-907-2018 5+ Documents (More...)

1990 6665-21-898-4008 https//www.nsnlookup.com /cage Natural Resources Canada (CAGE Code 35924) 7010-21-907-2018
2995-00-905-6940 2995009056940 009056940 is an item designed to accelerate a gas turbine engine from rest to starter cutoff speed by means of a combustion gas driven turbine and reduction gear assembly constructed to be mounted on the engine starter drive. the combustion gas is generated from ignited liquid fuel and air in the combustion chamber or from a solid propellant cartridge attached to the combustion chamber of the starter. may have provision for energizing the turbine by low pressure air from engine bleed or ground equipment air supply.
4 27 Mar 1983 4330-21-900-4615 Fluid Filter 1217-05969RNCC: 6 | RNVC: 9 | DAC: 9 14 Mar 1986 7010-21-907-2018
DAC: 2 13 Feb 1986 5961-14-544-6816 Transistor 2SC4239RNCC: 3 | RNVC: 2 | DAC: 4 17 Feb 2005 7010-21-907-2018
2995-01-490-6993 2995014906993 014906993 is an item designed to accelerate a gas turbine engine from rest to starter cutoff speed by means of a combustion gas driven turbine and reduction gear assembly constructed to be mounted on the engine starter drive. the combustion gas is generated from ignited liquid fuel and air in the combustion chamber or from a solid propellant cartridge attached to the combustion chamber of the starter. may have provision for energizing the turbine by low pressure air from engine bleed or ground equipment air supply.

7010-21-907-2018 Demil Restrictions 7010-21-907-2018

DEMIL: | DEMILI: | CRITICALITY: | HMIC: | PMIC: | EDC: | ADPEC:

7010-21-907-2018 is a Digital Computer System

7010-21-907-2018 End Users End Users 7010-21-907-2018

Canada (ZC)

7010-21-907-2018 Related Items NATO Stock Numbers Related to 7010-21-907-2018