Product Details | AIRCRAFT GAS TURBINE ENGINE COMBUSTION CHAMBER

2840-01-110-8104 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.

Part Alternates: 729195, 2840-01-110-8104, 01-110-8104, 2840011108104, 011108104

Engines, Turbines, and Components | Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components

Supply Group (FSG) NSN Assign. NIIN
28 06 APR 1981 01-110-8104

Cross Reference | NSN 2840-01-110-8104

Part Number Cage Code Manufacturer
729195 77445 UNITED TECHNOLOGIES CORPORATION DBA PRATT WHITNEY-SPARE PARTS

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Technical Data | NSN 2840-01-110-8104

Characteristic Specifications
ENGINE SECTION LOCATION COMBUSTION CHAMBER
OVERALL LENGTH 12.178 INCHES MINIMUM AND 12.238 INCHES MAXIMUM
CRITICALITY CODE JUSTIFICATION AGAV
END ITEM IDENTIFICATION ACFT ENG TF 30

Restrictions/Controls & Freight Information | NSN 2840-01-110-8104

Category Code Description
Hazardous Material Indicator CodeNThere is no data in the HMIS and the NSN is in an FSC not generally suspected of containing hazardous materials
Demilitarization Code:BMunitions List Item - Mutilation (MUT) to the point of scrap required. (Formerly: Demilitarization not required. Trade Security Controls (TSCs) required at disposition.)
Precious Metals Indicator Code:AItem does not contain precious metal
Criticality Code:YThe item does not have a nuclear hardened feature but does have other critical feature(s) such as tolerance, fit restriction or application.
Category Code Description
No Freight Information