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Overview
Damper is designed for use in compressor vane applications and is identified by 4318313. This component serves to minimize vibrations in aircraft gas turbines, specifically for the F119-PW-100 engine utilized in the F-22 aircraft. The damper features a nickel alloy construction, ensuring durability and performance in high-stress environments. Its criticality code justification is AGAV, indicating its importance in operational readiness and safety. This damper is essential for maintaining the integrity of the aircraft's systems.
Features & Benefits
Minimizes vibrations in aircraft gas turbines
Enhances operational readiness and safety
Constructed from durable nickel alloy
Technical Information
NIIN
014848072
NSN
2840-01-484-8072
FSCG
2840
FSCG Category
Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
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