4920-00-546-1808

Aircraft Engine Test Stand

4920005461808 005461808 391-100

A device designed to test the performance and/or operational characteristics of aircraft engines. For mobile items, see TEST STAND, ENGINE, SEMITRAILER MOUNTED. See also STAND, AIRCRAFT ENGINE; and STAND, MAINTENANCE, AIRCRAFT ENGINE. View more Aircraft Engine Test Stand

4920-00-546-1808 TEST STAND,AIRCRAFT ENGINE 4920005461808 005461808

Managed by United States
NSN Created on 1 Jan 1963
Data Last Changed
November 2023
NATO Update Count
20
NATO Data Quality
4920-00-546-1808 TEST STAND,AIRCRAFT ENGINE 4920005461808 005461808 1/1
NSN 4920-00-546-1808 (Generic Image) 1/1

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4920-00-546-1808 Related Documents Related Documents 4920-00-546-1808 5+ Documents (More...)

4920-00-546-1812 Aircraft Maintenance Kit 390J33-35-47RNCC: 5 | RNVC: 9 | DAC: 5 1 Jan 1963 4920-00-546-1808
5995-99-724-2463 5995997242463 997242463 is a definite continuous length of ribbon type cable, special purpose, electrical, having one or more ends (may or may not be branched) and/or intermediate positions processed or terminated with facilities which provide for electrical connections to other items. excludes cable assembly, printed, flexible; cable assembly, special purpose, electrical; and cable assemby, special purpose, electrical branched.
4320-99-341-3881 4320993413881 993413881 is an item consisting of power driven hydraulic pump(s) with instruments, controls and the like assembled on a common mounting. it may include engine(s) or motor(s) or be designed to be mounted on a vehicle which provides the power. it may include a hydraulic fluid reservoir, pressure fluid filters, accumulators, boosters, hose and hose reels or racks. it is used in the operation of hydraulic tools or equipment and/or checking of hydraulic systems. see also test stand, hydraulic system components. excludes filler, hydraulic system, guided missile.
4820-99-147-5905 4820991475905 991475905 is a valve designed to automatically release excessive pressures. it is actuated by static pressure upstream of the valve and is used as a safety valve or relief valve, and may be set to close at a predetermined pressure. it is not designed for regulation of continuously fluctuating loads. it may be inline or cartridge (manifold) design. excludes valve (1), relief, pressure and temperature.
4730-99-765-4221 4730997654221 997654221 is a fitting having three connections with the branch connection fixed at 90 degrees (1.5705 radians) to the run. the connections have machine threads (straight threads other than pipe or hose series) designed to accommodate a tube, or are unthreaded and designed to accommodate a tube. it may have side inlet(s). it is used as a junction at the intersection of a tube or tube fitting.

4920-00-546-1808 Demil Restrictions 4920-00-546-1808

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

4920-00-546-1808 is a Aircraft Engine Test Stand 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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