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NSN 2840-01-033-9081, 2840010339081
HUB,COMPRESSOR,AIRCRAFT GAS TURB

Federal Supply Classification
FSC 2840 - Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
National Item Identification Number
NIIN 010339081
Codification Country
United States
Item Name Code
INC 50573
Criticality
(Y) This item does not have a nuclear hardened feature but does have other critical feature(s) 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.
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DLMS® Summary

National Stock Number 2840-01-033-9081

National Stock Number (NSN) 2840-01-033-9081, or NIIN 010339081, (hub,compressor,aircraft gas turb) was assigned January 14, 1977 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.

Based on a planned procurement review by the Primary Inventory Control Activity (PICA) on Sep 02, 2000, this NSN's acquisition method was noted as: Suitable for Competitive Acquisition. (Potential sources shall include dealers/distributors.) The Government physically does not have in its possession sufficient, accurate, or legible data to purchase this part from other than current source(s). (NOTE: This code is applicable only to parts under immediate buy requirements and only as long as the deficiency is under review for resolution and appropriate recoding.) Valid AMCs: 1, 2, 3, 4 and 5.

This NSN is assigned to Item Name Code (INC) 50573. [A COMPONENT OF A ROTOR, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE. IT IS DESIGNED TO ATTACH TO THE FRONT AND/OR REAR OF THE ROTOR PROVIDING SUPPORT, ALIGNMENT, AND A MEANS OF ATTACHMENT FOR A SHAFT, TURBINE, AIRCRAFT GAS TURBINE ENGINE. IT MAY HAVE PROVISIONS FOR INSTALLING BEARINGS, AND/OR OIL AND AIR SEALS. SEE ALSO DISK AND HUB, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE.]. This item does not have a nuclear hardened feature but does have other critical feature(s) 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 2840010339081 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

III MATERIAL
(MATT) NICKEL ALLOY HUB
END ITEM IDENTIFICATION
(AGAV) F100-PW-100 AIRCRAFT ENGINE
CRITICALITY CODE JUSTIFICATION
(CRTL) FEAT
DESIGN TYPE
(APGF) COMPRESSOR
DIAMETER
(ABMZ) 7.162 INCHES MINIMUM AND 7.166 INCHES MAXIMUM
ENGINE SECTION LOCATION
(CZBJ) COMPRESSOR
MATERIAL DOCUMENT AND CLASSIFICATION
(MDCL) PWA1022 MFR REF SINGLE MATERIAL RESPONSE HUB
MATERIAL
(MATT) NICKEL ALLOY HUB
PART NAME ASSIGNED BY CONTROLLING AGENCY
(CXCY) ORIG NAME NUT,PLAIN,ROUND
OVERALL LENGTH
(ABHP) 4.004 INCHES MINIMUM AND 4.014 INCHES MAXIMUM
SPECIAL FEATURES
(FEAT) INTL INVOLUTE SPLINE DATA: TEETH 140; PRESSURE ANGLE 30 DEG.; T.O. 2J-F100-4, FIGURE 115, INDEX 3; USED ON THE REAR COMPRESSOR DRIVE; SEE TCTO 2J-F100(II)-509 SUPERSEDES PN 4036639; F100 FRACTURE CRITICAL PART.
STAGE NUMBER
(CZCJ) 2

Manufacturer Part Numbers


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