Model: 2-121-054-11
A Inner Augmentor Nozzle SectionProperties:
A rigid item designed to help direct the flow of hot gases from an afterburner,turbine engine. it is an integral part of a nozzle,augmentor exhaust, aircraft gas turbine engine. the item is to the rear of and hinged to an augmentor nozzle section,convergent, aircraft gas turbine engine.
Part 2-121-054-11 NSN 2840-01-475-9246
Material Classification
Hazardous material, precious metals, criticality, enviroment, and electrostatic discharge indicatorsPackaging & Shipping
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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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