6620-01-413-2316

Engine Testing Thrust Indicator

6620014132316 014132316 4004670-742

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

6620-01-413-2316 INDICATOR,THRUST,ENGINE TESTING 6620014132316 014132316

Managed by United States
NSN Created on 9 May 1995
Data Last Changed
November 2023
NATO Update Count
3
NATO Data Quality
6620-01-413-2316 INDICATOR,THRUST,ENGINE TESTING 6620014132316 014132316 1/1
NSN 6620-01-413-2316 (Generic Image) 1/1

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portable gas turbine engine test system. https https//www.nsnlookup.com /fsg-66/fsc-6620/us 6620-01-413-2316
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6620-01-413-2316 Demil Restrictions 6620-01-413-2316

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

6620-01-413-2316 is a Engine Testing Thrust Indicator 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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