6130-12-325-9667

Static Power Inverter

6130123259667 123259667 121-031.SA001 121C031HP007 121E031SA001 121-031 121-031.GER 121-031GER

An item that changes a direct current input into a single or multiple phase alternating current output, by the combined action of oscillators, semiconductor devices, magnetic amplifiers, phase splitters, and the like. For items that perform the same function by means of rotating machine techniques, see MOTOR-GENERATOR. See also CONVERTER, FREQUENCY, STATIC. View more Static Power Inverter

6130-12-325-9667 INVERTER,POWER,STATIC 6130123259667 123259667

Managed by Germany
NSN Created on 25 Jul 1991
Data Last Changed
January 2023
NATO Update Count
1
NATO Data Quality
6130-12-325-9667 INVERTER,POWER,STATIC 6130123259667 123259667 1/1
NSN 6130-12-325-9667 (Generic Image) 1/1

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6130-12-325-9667 Related Documents Related Documents 6130-12-325-9667 5+ Documents (More...)

| RNVC: 2 | DAC: 3 5 Jan 2001 7310-17-120-6323 https//www.nsnlookup.com /fsg-61/fsc-6130/de 6130-12-325-9667
Static Power Inverter 6130123259667 123259667 6130-12-325-9667 6130123259667 123259667 is an item
Krasnoselskaya Moscow 107140 Russian Federation Points https//www.nsnlookup.com /fsg-61/fsc-6130/de 6130-12-325-9667
Static Power Inverter 6130123259667 123259667 6130-12-325-9667 6130123259667 123259667 is an item
| RNVC: 2 | DAC: 6 21 Jul 1999 2050-01-374-7199 https//www.nsnlookup.com /fsg-61/fsc-6130/de 6130-12-325-9667
Static Power Inverter 6130123259667 123259667 6130-12-325-9667 6130123259667 123259667 is an item
1560-01-375-7259 1560013757259 013757259 is a preformed item of various shapes, and contours, which may have a sandwich or honeycomb core bonded to a metallic or nonmetallic facing material. it is used to enclose integral portions of the fuselage or to form partitions or sections within a wing, empennage, fuselage, nacelle or crew compartment. it may have mounting provisions such as predrilled holes to facilitate installation, but will have no items attached to it except bracket (s) or other securing devices to accommodate its own mounting or support. it may be mounted by means of fasteners, bonding or welding. excludes panel, interior lining, aircraft; cover access; cover, access, aircraft; floor (1), aircraft; core material, cellular, structural.
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5305-14-490-8032 France (ZF) Approved Sources 5305-14-490-8032 Part NumberManufacturerStatus4042 121 031

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