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6615-01-437-9024

Attitude-Heading Gyroscope Control

6615014379024 014379024 060-00013-0002 060-0013-02 KSG105-M1 985.99.11.077

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

6615-01-437-9024 CONTROL,GYROSCOPE,ATTITUDE-HEADING 6615014379024 014379024

Managed by United States
NSN Created on 25 Oct 1996
Data Last Changed
November 2023
NATO Update Count
3
NATO Data Quality
6615-01-437-9024 CONTROL,GYROSCOPE,ATTITUDE-HEADING 6615014379024 014379024 1/1
NSN 6615-01-437-9024 (Generic Image) 1/1

6615-01-437-9024 Stock and Availability Marketplace 6615-01-437-9024

6615-01-437-9024 Related Documents Related Documents 6615-01-437-9024 4+ Documents (More...)

060-00013-0002 060-0013-02 KSG105-M1 985.99.11.077 A control designed for use with automatic pilots
RQST Updated Every Day 6615-01-437-9024 RQST NE Related Documents 6615-01-437-9024 5+ Documents ( More
pilots RQST NS Request Quotation Updated Every Day 6615-01-437-9024 RQST NE Updated Every Day 6615-01
Documents 6615-01-438-4119 5+ Documents ( More https//www.nsnlookup.com /fsg-66/fsc-6615/us 6615-01-437-9024
Attitude-Heading Gyroscope Control 014379024 66/fsc-6615/us 6615-01-438-4122 Amplifier-Computer
fsg-66/fsc-6615/us 6615-01-438-4119 Amplifier-Computer 6615014384119014384119 66/fsc-6615/us 6615-01-437-9024
-438-4122 5+ Documents ( More https Amplifier-Computer 6615014384119014384119 66/fsc-6615/us 6615-01-437-9024
Attitude-Heading https 6615/us 6615-01-438-4122 https//www.nsnlookup.com /fsg-66/fsc-6615/us 6615-01-437-9024
Attitude-Heading Gyroscope Control 014379024 6615-01-437-9024 RQST NE Updated Every Day 6615-01
6615-01-438-4122 Amplifier-Computer 6 Nov 1996 6615-01-438-4119 Amplifier-Computer 6 Nov 1996 6615-01-437-9024

6615-01-437-9024 Demil Restrictions 6615-01-437-9024

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

6615-01-437-9024 is a Attitude-Heading Gyroscope Control that does not have a nuclear hardened feature or any other critical feature such as tolerance, fit restriction or application. This item is considered a low risk when released from the control of the Department of Defense. The item may still be subject to the requirements of the Export Administration Regulations (EAR) and the Code of Federal Regulations (CFR). This item is not suspected to be hazardous. This item does not contain a precious metal.

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