6620-14-407-2512
Engine Testing Thrust Indicator
6620144072512 144072512 704A46-580-004 192000B 192000A
An engine testing instrument designed to reflect the forwardly directed reaction force produced by a high-speed jet of fluid discharged rearwards from a nozzle orifice (as in a jet plane or rocket). It designates in units of thrust, the thrust output of gas turbine or jet propulsion engines. This instrument is normally used on a stationary, mobile, or portable gas turbine engine test system. View more Engine Testing Thrust Indicator
Managed by France
NSN Created on 12 Feb 1986
Data Last Changed
January 2023
January 2023
NATO Update Count
1
1
NATO Data Quality
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Related Documents 6620-14-407-2512 5+ Documents (More...)
704A46-580-004 192000B 192000A An engine testing instrument designed to reflect the forwardly directed
/fsg-66/fsc-6620/fr 6620-14-407-2512 Indicator 144072512 fr 6620-14-407-2512 / Engine Testing Thrust
Engine Testing Thrust Indicator 144072512 /fsg-66/fsc-6620/fr 6620-14-407-2512 Engine Testing Thrust
/fsg-66/fsc-6620/fr 6620-14-407-2512 Indicator 144072512 fr 6620-14-407-2512 / Engine Testing Thrust
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Restrictions 6620-14-407-2512
End Users 6620-14-407-2512
- Brazil (YA)
- France (ZF)
Approved Sources 6620-14-407-2512
- Part Number
- Manufacturer
- Status
- 704A46-580-004
- Manufacturer
- F0210 - Airbus Helicopters (Ets De (Active)
- Source Control
- Source Control
- 192000B
- F7250 - Speg Pronergy (Active)
- Primary Buy
- Primary Buy
- 192000A
- F7250 - Speg Pronergy (Active)
- Secondary Buy
- Secondary Buy
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