Product Details | AIRCRAFT GAS TURBINE ENGIN TURBINE NOZZLE ASSEMBLY

2840-00-054-1355 A stationary item designed for the purpose of directing air at the proper angle and velocity to a ROTOR, TURBINE, AIRCRAFT GAS TURBINE ENGINE. It has provisions for attaching to a CASE (3), TURBINE, AIRCRAFT GAS TURBINE ENGINE. It may have an inner support shroud. The assembled item forms a complete circle.

Part Alternates: 617295, 704575, 730825, 2840-00-054-1355, 00-054-1355, 2840000541355, 000541355

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

Supply Group (FSG) NSN Assign. NIIN
28 00-054-1355

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Technical Data | NSN 2840-00-054-1355

Characteristic Specifications
ENGINE SECTION LOCATION TURBINE
OVERALL LENGTH 1.272 INCHES NOMINAL
DIAMETER 27.680 INCHES NOMINAL
SPECIAL FEATURES 19.330 IN. ID.; 174 VANES
CRITICALITY CODE JUSTIFICATION AGAV
III END ITEM IDENTIFICATION TF-30 AIRCRAFT ENGINE
MANUFACTURERS CODE 77445
DESIGN CONTROL REFERENCE 730825

Restrictions/Controls & Freight Information | NSN 2840-00-054-1355

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
Category Code Description
No Freight Information