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NSN 2840-00-828-5212, 2840008285212
CHAMBER,COMBUSTION,AIRCRAFT GAS

Federal Supply Classification
FSC 2840 - Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
National Item Identification Number
NIIN 008285212
Codification Country
United States
Item Name Code
INC 50337
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: Readily Available Qualified Suppliers: Currently qualifying suppliers

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DLMS® Summary

National Stock Number 2840-00-828-5212

National Stock Number (NSN) 2840-00-828-5212, or NIIN 008285212, (chamber,combustion,aircraft gas) was assigned August 28, 1967 in the Federal Logistics Information System (FLIS). This NIIN is Available for Manual Assignment. This NSN does not replace any other NSNs.

There are 3 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, 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.

There has been very little 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 Jun 10, 2020, this NSN's acquisition method was noted as: Acquire, for the first time, directly from the actual manufacturer rather than the prime contractor who is not the actual manufacturer. The rights to use the data needed to purchase this part from additional sources are not owned by the Government and cannot be purchased. Valid AMCs: 1, 2, 3, 4 and 5.

This NSN is assigned to Item Name Code (INC) 50337. [THE PORTION OF AN ENGINE, GAS TURBINE, AIRCRAFT IN WHICH FUEL IS BURNED. IT MAY BE AN ANNULAR TYPE IN WHICH THE SPACE BETWEEN THE CIRCULAR INNER AND OUTER CYLINDERS FORM THE BURNING CHAMBER OR IT MAY BE THE MULTI-ARRANGEMENT CAN TYPE IN WHICH SEPARATE CAN LIKE BURN CYLINDERS ARE POSITIONED IN A CIRCULAR ARRANGEMENT WITHIN AN INNER AND OUTER CASE.]. 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 2840008285212 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

END ITEM IDENTIFICATION
(AGAV) ACFT ENG TF33
ENGINE SECTION LOCATION
(CZBJ) COMBUSTION CHAMBER
OVERALL LENGTH
(ABHP) 17.260 INCHES MINIMUM AND 17.320 INCHES MAXIMUM
MATERIAL
(MATT) UNABLE TO DECODE
SPECIAL FEATURES
(FEAT) T.O. 2J-TF33-14, FIG 25, IND 9; USED ON THE TF33-P-7A ENGINE ONLY; T.O. 2J-TF33-4, FIG 27, IND 8; TO BE USED ON THE P-5 AND P-9 ENGINE ONLY; COMBUSTION CAN USED ON THE CASE OUTER FRONT AND OUTER REAR CHAMBER
CRITICALITY CODE JUSTIFICATION
(CRTL) AGAV
MATERIAL
(MATT) STEEL OVERALL

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