Model: 68B37671CL10
Turbine Engi Turbine Nozzle VaneSpecial Features:
Nickle alloy, pwa 651, fscm 77445, coated per sanep 68-248, fscm98750, 3.479-3.489 in. Lg, 2.000 in. W, 91.700-92.400 sq in. Area. Used on aircraft jet engine, j57
Properties:
Inc 61701 cancelled/replaced by ,inc 50614, fiig a10700, app-key a ,inc 50613, fiig a10700, app-key a ,inc 50612, fiig a10700, app-key a ,inc 50611, fiig a10700, app-key a ,on 100112 ~(all except usa) for usa inc 61701 canceled replaced by vane, turbine engine: inc 40963, fiig a107, appl key a. An item spaced radially in a nozzle, turbine, turbine engine, located between the inner and outer shroud of the nozzle unit, designed for the function of directing hot gases to the turbine at a proper velocity and angle.
Part 68B37671CL10 NSN 2840-00-943-2359
Material Classification
Hazardous material, precious metals, criticality, enviroment, and electrostatic discharge indicatorsFreight 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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