6615-12-393-9313
Attitude-Heading Gyroscope Control
6615123939313 123939313 145130-7001 LCR-100
A control designed for use with automatic pilots and/or remote attitude indicators consisting primarily of a gyroscope which provides signals for controlling an aircraft about its lateral and longitudinal axis and/or signals for providing a visual presentation of attitude to the pilot. View more Attitude-Heading Gyroscope Control
Managed by Germany
NSN Created on 23 Oct 2013
Data Last Changed
January 2023
January 2023
NATO Update Count
1
1
NATO Data Quality

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145130-7001 LCR-100 A control designed for use with automatic pilots and/or remote attitude indicators
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9150/de 9150-12-321-7180 Damping Fluid 9150123217180123217180 OEL CR 100CR 100CR1000007946 06V001-1 LCR 100
42/fsc-4230/ca 4230-21-904-2007 Hazardous Spill Cle 4230219042007 219042007 CR1000007946 06V001-1 LCR 100
-91/fsc-9150/de 9150-12-321-7180 Damping Fluid 9150123217180123217180CR 100 CR1000007946 06V001-1 LCR 100
42/fsc-4230/ca 4230-21-904-2007 Hazardous Spill Cle 4230219042007 219042007 CR1000007946 06V001-1 LCR 100
-91/fsc-9150/de 9150-12-321-7180 Damping Fluid 9150123217180123217180CR 100 CR1000007946 06V001-1 LCR 100
www.nsnlookup.com /fsg-66/fsc-6615/de 6615-12-188-7539 https//www.nsnlookup.com /fsg-66/fsc-6615/de 6615-12-393-9313
Attitude-Heading Gyroscope Control 123939313 www.nsnlookup.com /fsg-66/fsc-6615/de 6615-12-393-
Attitude-Heading Gyroscope Control 123939313 www.nsnlookup.com /fsg-66/fsc-6615/de 6615-12-393-
5 30 May 1969 6615-12-188-7539 Deckel 450900-6629-001RNCC: 3 | RNVC: 2 | DAC: 4 28 Jul 1981 6615-12-393-9313
Restrictions 6615-12-393-9313
End Users 6615-12-393-9313
- Turkey (ZW)
Approved Sources 6615-12-393-9313
- Part Number
- Manufacturer
- Status
- 145130-7001
- Manufacturer
- D4856 - Northrop Grumman Litef Gmbh (Active)
- Primary Buy
- Primary Buy
- LCR-100
- D4856 - Northrop Grumman Litef Gmbh (Active)
- Canceled/Obsolete
- Canceled/Obsolete
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