Model: 6847449
Aircraft Gas Turbi Turbine RotorSpecial Features:
Cres, ems73634 fscm 73342, 44 blades, 7.170 in. Min, 7.172 in. Max o/a od, 1.319 in. Min, 1.321 in. Max o/a lg, 1st end hub, ext splines, 20 teeth, 30 degrees pressure angle, 1.938 in.-24 ext thd located 0.090 in. Nom distance from 1st end, 0.250 in. Nom thd lg, 10 holes 0.200 in. Nom diameter equally spaced on od hub, 0.520in. Nom c to c distance from 1st end to holes, 2nd end hub, ext splines, 20 teeth, 30 degrees pressure angle, stepped id, 1.1585 in. Min, 1.1590 in. Max smallest id.Flight safety critical aircraft part
Properties:
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.
Part 6847449 NSN 2840-00-940-8452
Material Classification
Hazardous material, precious metals, criticality, enviroment, and electrostatic discharge indicatorsPackaging & Shipping
Freight Classification
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Schedule B and Export
- Schedule B: 8411997050
- SITC: 71499
- End Use: Engines and turbines for military aircraft
- NAICS: 336412
- USDA: 1
Freight Class: Parts of gas turbine aircraft engines, other than for use in civil aircraft
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