6615-14-451-4509
Attitude-Heading Gyroscope Control
6615144514509 144514509 PCN52P22 PCN52P22-01
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
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Managed by France
NSN Created on 21 Nov 1991
Data Last Changed
January 2023
January 2023
NATO Update Count
1
1
NATO Data Quality

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Related Documents 6615-14-451-4509 1+ Documents (More...)
PCN52P22 PCN52P22-01 A control designed for use with automatic pilots and/or remote attitude indicators
RQST NE Updated Every Day 6615-14-451-4509 RQST Updated Every Day 6615-14-451-4509 RQST NE Related Documents
6615-14-451-4509 1+ Documents ( More... ) https//www.nsnlookup.com /fsg-66/fsc-6615/fr 6615-14-451-4509
RQST NE Updated Every Day 6615-14-451-4509 RQST Updated Every Day 6615-14-451-4509 RQST NE Related Documents
6615-14-451-4509 1+ Documents ( More... ) https//www.nsnlookup.com /fsg-66/fsc-6615/fr 6615-14-451-4509
Restrictions 6615-14-451-4509
End Users 6615-14-451-4509
- France (ZF)
Approved Sources 6615-14-451-4509
- Part Number
- Manufacturer
- Status
- PCN52P22-01
- Manufacturer
- F6151 - Safran (Active)
- Primary Buy
- Primary Buy
- PCN52P22
- F6151 - Safran (Active)
- Incomplete Secondary Reference
- Incomplete Secondary Reference
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