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NSN 2840-00-591-0741, 2840005910741
DISK AND HUB,TURBINE,AIRCRAFT GA

Federal Supply Classification
FSC 2840 - Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
National Item Identification Number
NIIN 005910741
Codification Country
United States
Item Name Code
INC 50565
Criticality
(F) This item is a Flight Safety Critical Aircraft Part (FSCAP).
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.
Availability: Request Qualified Suppliers: Currently qualifying suppliers

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DLMS® Summary

National Stock Number 2840-00-591-0741

National Stock Number (NSN) 2840-00-591-0741, or NIIN 005910741, (disk and hub,turbine,aircraft ga) was assigned January 3, 1975 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. One of those part number(s) are considered obsolete. The manufacturer part numbers were originally supplied by 2 suppliers. Today, 2 suppliers are listed as Active suppliers for this NSN. Of the active suppliers, only one supplier is deemed design controlled or valid supply parts.

This part number has not been procured by the US Government in over 5 years, with the most recent procurement date of Jun 27, 2013. There have been 2 contracts issued for this part number, with 4 awards given. The US Government has only awarded those contracts to one supplier. The last contract numbers awarded were: SPM4A111G0010, SPM4A111G0010, SPM4A111G0010, SPM4A111G0010, SPM4A111G0010. The total value of the awarded contracts has been US$ 232,271.00.

This NSN is somewhat common among different platforms, belonging to 7 different weapons systems.

There has been a small amount of demand for this national stock number. The demand for this NSN originated from less than 5 countries. Based on a planned procurement review by the Primary Inventory Control Activity (PICA) on Jul 02, 2006, this NSN's acquisition method was noted as: Acquire directly from the actual manufacturer, whether or not the prime contractor is the actual manufacturer. This part requires engineering source approval by the design control activity in order to maintain the quality of the part. An alternate source must qualify in accordance with the design control activity's procedures, as approved by the cognizant Government engineering activity. Valid AMCs: 1, 2, 3, 4 and 5.

This NSN is assigned to Item Name Code (INC) 50565. [AN ITEM THAT CONSISTS OF A DISK, TURBINE, AIRCRAFT GAS TURBINE ENGINE AND A HUB, TURBINE, AIRCRAFT GAS TURBINE ENGINE.]. This item is a Flight Safety Critical Aircraft Part (FSCAP). There is no data in the HMIRS and the NSN is in an FSC not generally suspected of containing hazardous materials. NSN 2840005910741 contains an unknown precious metal.

This NSN is associated to Schedule B 8411997050: parts of gas turbine aircraft engines, other than for use in civil aircraft. The Schedule B End Use is listed as engines and turbines for military aircraft. NAICS classification category 336412: aircraft engine and engine parts manufacturing.

This information was last updated on .


Technical Characteristics

GENERAL CHARACTERISTICS ITEM DESCRIPTION
(TEXT) CRES,M3603,FSCM 91547,ROCKWELL A SCALE 69 MIN,73 MAX HARDNESS,3.805 IN. MIN,3.815 IN. MAX O/A LG,9.820 IN. NOM OD DISK,1.394 IN.MIN,1.397 IN. MAX LG DISK,60 BLADE GROOVES EQUALLY SPACED ON DISKOD,2 STEPPED HUBS,2.830 IN. MIN,2.840 IN. MAX OD 1ST STEP 1ST END,0.700 IN. NOM LG 1ST STEP 1ST END,3.320 IN. NOM DIA 2ND STEP 1STEND,0.603 IN. MIN,0.607 IN. MAX LG 2ND STEP 1ST END,EXTERNALSPLINES 1ST STEP 2ND END,69 TEETH,30 DEG PRESSURE ANGLE,2.8750 IN.NOM PITCH DIA,0.380 IN. MIN,0.420 IN. MAX LG SPLINES,0.681 IN.MIN,0.738 IN. MAX LG 2ND STEP 2ND END,STEPPED BORE,3.805 IN. MIN,3.815 IN. MAX O/A LG BORE,2.5576 IN. MIN,2.5579 IN. MAX DIA 1STSTEP 1ST END,0.950 IN. NOM LG 1ST STEP 1ST END,2.566 IN. MIN,2.576 IN. MAX DIA 2ND STEP 1ST END,0.600 IN. NOM LG 2ND STEP 1STEND,2.2133 IN. MIN,2.2137 IN. MAX DIA 1ST STEP 2ND END,0.275 IN.MIN,0.295 IN. MAX LG 1ST STEP 2ND END,2.425 IN. MIN,2.435 IN. MAXDIA 2ND STEP 2ND END,0.165 IN. MIN,0.205 IN. MAX LG 2ND STEP 2NDEND,INTERNAL SPLINES 3RD STEP 2ND
SPECIAL FEATURES
(FEAT) CRES,M3603,FSCM 91547,ROCKWELL A SCALE 69 MIN,73 MAX HARDNESS,3.805 IN. MIN,3.815 IN. MAX O/A LG,9.820 IN. NOM OD DISK,1.394 IN.MIN,1.397 IN. MAX LG DISK,60 BLADE GROOVES EQUALLY SPACED ON DISKOD,2 STEPPED HUBS,2.830 IN. MIN,2.840 IN. MAX OD 1ST STEP 1ST END,0.700 IN. NOM LG 1ST STEP 1ST END,3.320 IN. NOM DIA 2ND STEP 1STEND,0.603 IN. MIN,0.607 IN. MAX LG 2ND STEP 1ST END,EXTERNALSPLINES 1ST STEP 2ND END,69 TEETH,30 DEG PRESSURE ANGLE,2.8750 IN.NOM PITCH DIA,0.380 IN. MIN,0.420 IN. MAX LG SPLINES,0.681 IN.MIN,0.738 IN. MAX LG 2ND STEP 2ND END,STEPPED BORE,3.805 IN. MIN,3.815 IN. MAX O/A LG BORE,2.5576 IN. MIN,2.5579 IN. MAX DIA 1STSTEP 1ST END,0.950 IN. NOM LG 1ST STEP 1ST END,2.566 IN. MIN,2.576 IN. MAX DIA 2ND STEP 1ST END,0.600 IN. NOM LG 2ND STEP 1STEND,2.2133 IN. MIN,2.2137 IN. MAX DIA 1ST STEP 2ND END,0.275 IN.MIN,0.295 IN. MAX LG 1ST STEP 2ND END,2.425 IN. MIN,2.435 IN. MAXDIA 2ND STEP 2ND END,0.165 IN. MIN,0.205 IN. MAX LG 2ND STEP 2NDEND,INTERNAL SPLINES 3RD S

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