6605-14-537-6134
Inertial Navigation System
6605145376134 145376134 704A47-1520-23 SYG50HAA1XAIR
A self-contained, dead-reckoning system that senses acceleration along the pitch, yaw and roll axis of land vehicle, watercraft or aircraft and calculates the distance from a reference point. They can include INERTIAL NAVIGATION UNIT(s); PLATFORM, INERTIAL; power supplies; subsystems; mode selectors; and control displays. View more Inertial Navigation System
Managed by France
NSN Created on 12 Nov 2003
Data Last Changed
January 2023
January 2023
NATO Update Count
1
1
NATO Data Quality
Marketplace 6605-14-537-6134
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Related Documents 6605-14-537-6134 1+ Documents (More...)
704A47-1520-23 SYG50HAA1XAIR A self-contained, dead-reckoning system that senses acceleration along
RQST NE Updated Every Day 6605-14-537-6134 RQST Updated Every Day 6605-14-537-6134 RQST NE Related Documents
6605-14-537-6134 1+ Documents ( More... ) https//www.nsnlookup.com /fsg-66/fsc-6605/fr 6605-14-537-6134
RQST NE Updated Every Day 6605-14-537-6134 RQST Updated Every Day 6605-14-537-6134 RQST NE Related Documents
6605-14-537-6134 1+ Documents ( More... ) https//www.nsnlookup.com /fsg-66/fsc-6605/fr 6605-14-537-6134
Restrictions 6605-14-537-6134
End Users 6605-14-537-6134
- France (ZF)
Approved Sources 6605-14-537-6134
- Part Number
- Manufacturer
- Status
- 704A47-1520-23
- Manufacturer
- F0210 - Airbus Helicopters (Ets De (Active)
- Source Control
- Source Control
- SYG50HAA1XAIR
- F6151 - Safran (Active)
- Primary Buy
- Primary Buy
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