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NSN 2835-01-032-7140, 2835010327140
ENGINE,GAS TURBINE,NONAIRCRAFT

Federal Supply Classification
FSC 2835 - Gas Turbines and Jet Engines; Non-Aircraft Prime Mover, Aircraft Non-Prime Mover, and Components
National Item Identification Number
NIIN 010327140
Codification Country
United States
Item Name Code
INC 50489
Criticality
(N) This item does not have a critical feature such as tolerance, fit restrictions or application. Nuclear hardness properties have not been determined (not valid for input).
Hazardous Material Indicator Code
(N) There is no data in the HMIRS and the NSN is in an FSC not generally suspected of containing hazardous materials.
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DLMS® Summary

National Stock Number 2835-01-032-7140

National Stock Number (NSN) 2835-01-032-7140, or NIIN 010327140, (engine,gas turbine,nonaircraft) was assigned December 18, 1976 in the Federal Logistics Information System (FLIS). This NIIN is Available for Manual Assignment. This NSN does not replace any other NSNs.

There are 2 manufacturer part numbers associated with this NSN. None of the associated part number(s) are considered obsolete. The manufacturer part numbers were originally supplied by one supplier. Today, one supplier is listed as an Active supplier for this NSN. Of the active suppliers, there are no suppliers that are deemed design controlled or valid supply parts.

This part number has not been procured by the US Government in over 5 years.

Based on a planned procurement review by the Primary Inventory Control Activity (PICA) on Apr 02, 1991, this NSN's acquisition method was noted as: Acquire directly from the actual manufacturer, whether or not the prime contractor is the actual manufacturer. Acquisition of this part is restricted to source(s) specified on "Source Control", "Altered Item" or "Selected Item" drawings/documents. Valid AMCs: 1, 2, 3, 4 and 5.

This NSN is assigned to Item Name Code (INC) 50489. [A CONTINUOUS COMBUSTION TYPE ENGINE. CONSISTS PRIMARILY OF A COMPRESSOR, NONAIRCRAFT GAS TURBINE ENGINE; CHAMBER, COMBUSTION, NONAIRCRAFT GAS TURBINE ENGINE AND A TURBINE ASSEMBLY, NONAIRCRAFT GAS TURBINE ENGINE. IT MAY HAVE A FAN SECTION. AIR IS COMPRESSED AND HEATED BY A COMBUSTIBLE FUEL AND EXPANDED THROUGH THE TURBINE. IT IS DESIGNED TO FURNISH A SOURCE OF ROTARY SHAFT AND/OR PNEUMATIC POWER. THE PNEUMATIC POWER IS OBTAINED BY A BLEEDOFF OF THE ENGINE COMPRESSOR. FOR A COMPLETE OPERATING POWER UNIT, MOUNTED ON A BASE, SEE POWER UNIT, GAS TURBINE ENGINE.]. This item does not have a critical feature such as tolerance, fit restrictions or application. Nuclear hardness properties have not been determined (not valid for input). There is no data in the HMIRS and the NSN is in an FSC not generally suspected of containing hazardous materials. NSN 2835010327140 contains an unknown precious metal.

This NSN is associated to Schedule B 8411818000: gas turbine engine, except aircraft nesoi, of a power not exceeding 5,000 kw. The Schedule B End Use is listed as industrial engines. NAICS classification category 333611: turbine and turbine generator set units manufacturing.

This information was last updated on .


Technical Characteristics

REFERENCE NUMBER DIFFERENTIATING CHARACTERISTICS
(ZZZY) AS DIFFERENTIATED BY SOURCE CONTROL DWG NO.,STEEL CONTAINER
SPECIAL FEATURES
(FEAT) PNEUMATIC SHAFT POWER OUTPUT,190.0 SHAFT HORSEPOWER RATING,6000.0 RPM SHAFT HORSEPOWER SPEED RATING,40700.0 AIR HORSEPOWER RATING,460.0 LB PER MINUTE AIR FLOW,80.0 PSI DISCHARGE PRESSURE,0.0 ALTITUTE AT WHICH HORSEPOWER IS RATED,130.0 DEG FAHRENHEIT HORSEPOWER RATED,7500 HR OF OPERATION BETWEEN OVERHAULS,JET FUEL,AC,120.0/208.0 V,CENTRIFUGAL SWITCH,DUAL PAD DRIVE,FUEL CONTROL,IGNITER,OIL COOLER,OIL PUMP,STARTER,LOAD CONTROL VALVE,INCLOSURE,BASE FRAME MOUNTING,STEEL CONTAINER ACCOMMODATES ENGINE,42.630 IN. MAX O/A LG,27.810 IN. NOM O/A HEIGHT,29.460 IN. NOM O/A WIDTH

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