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NSN 2840-00-157-3605, 2840001573605
ROTOR,TURBINE,AIRCRAFT GAS TURBI

Federal Supply Classification
FSC 2840 - Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
National Item Identification Number
NIIN 001573605
Codification Country
United States
Item Name Code
INC 50591
Criticality
(X) This item does not have a nuclear hardened feature or any other critical feature such as tolerance, fit restriction or application.
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: Readily Available Qualified Suppliers: Currently qualifying suppliers

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DLMS® Summary

National Stock Number 2840-00-157-3605

National Stock Number (NSN) 2840-00-157-3605, or NIIN 001573605, (rotor,turbine,aircraft gas turbi) was assigned May 20, 1970 in the Federal Logistics Information System (FLIS). This NIIN is Available for Manual Assignment. This NSN does not replace any other NSNs.

There is only one manufacturer part number 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, 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.

This NSN is assigned to Item Name Code (INC) 50591. [A SINGLE OR MULTISTAGE ASSEMBLY DESIGNED TO RECEIVE THERMAL ENERGY FROM THE COMBUSTION SECTION AND CONVERT IT TO MECHANICAL ENERGY TO DRIVE THE ROTOR, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE AND/OR THE ROTOR, FAN, AIRCRAFT GAS TURBINE ENGINE THROUGH A SHAFT, TURBINE, AIRCRAFT GAS TURBINE ENGINE. IT CONSISTS OF DISKS, BLADES, HUBS, AND THE LIKE. IT IS THE MOVING PART OF A TURBINE ASSEMBLY, AIRCRAFT GAS TURBINE ENGINE. IT HAS FACILITIES FOR ATTACHING TO A SHAFT, TURBINE, AIRCRAFT GAS TURBINE ENGINE.]. This item does not have a nuclear hardened feature or any other critical feature such as tolerance, fit restriction or application. There is no data in the HMIRS and the NSN is in an FSC not generally suspected of containing hazardous materials. NSN 2840001573605 does not contain precious metals.

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

OVERALL LENGTH
(ABHP) 3.945 INCHES MINIMUM AND 3.960 INCHES MAXIMUM
MATERIAL DOCUMENT AND CLASSIFICATION
(MDCL) CRES,CPW203 CAGE 00198 MFR REF SINGLE MATERIAL RESPONSE OVERALL
MATERIAL
(MATT) NICKEL ALLOY OVERALL
SPECIAL FEATURES
(FEAT) 58 BLADES; 8.547 MIN 8.549 MAX IN. O/A OD; 1ST END STEPPED HUB; 1.12 MIN 1.1207 MAX OD 1ST STEP 1ST END; 0.2 MIN 0.21 MAX LG 1ST STEP 1ST END; EXT SPLINES 2ND STEP 1ST END; 38 TEETH; 30 DEG PRESSURE ANGLE; 1.2188 IN. NOM PITCH DIA 0.54 MIN 0.57 MAX IN. LG 2ND STEP 1ST END; 1.11 MIN 1.13 MAX OD 3RD STEP 1ST END; 0.07 MIN 0.08 MAX IN. LG 3RD STEP 1ST END; 1.3 MIN 1.3007 MAX IN. OD 4TH STEP 1ST END; 0.155 MIN 0.16 MAX IN. LG 4TH STEP 1ST END; 1.82 MIN 1.83 MAX IN. OD 5TH STEP 1ST END; 6TH STEP 1ST END TAPERED:1.675 MIN 1. 685 MAX SMALLEST OD; 0.635 MIN 0.705 MAX IN. LG 6TH STEP 1ST END; 1.77 MIN 1.825 MAX LG FROM 1ST END TO DISK; 2ND END PLAIN HUB; 1.408 MIN. 1.412 MAX IN. OD HUB 2ND END ; 0.495 MIN 0.515 MAX IN. LG FROM 2ND END TO DISK; 4 HOLES 0.208 MIN 0.212 MAX IN. DIA; 0.125 MIN 0.145 MAX IN. LG 5TH STEP 1ST END
III MATERIAL
(MATT) NICKEL ALLOY OVERALL

Manufacturer Part Numbers


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