P/N: 3102102-3
Category: Hoses & Tubing
This product requires a custom quote. Please contact our sales team for pricing information or submit an RFQ (Request for Quote).
| Condition | Stock |
|---|---|
| Serviceable | 1 Available |
| Overhauled | 1 Available |
The 3102102-3 is a nickel alloy transition liner assembly for Honeywell T76-G-420/421 turbine engines. This component channels hot combustor gases into the turbine section, managing thermal flow between engine stages. Fabricated from AMS5536 nickel alloy to withstand extreme combustor temperatures and pressure differentials.
Installation follows the applicable Honeywell engine maintenance manual with applicability verification through the engine illustrated parts catalog. NSN 2840-01-245-8118.
Please note: Product descriptions are provided for informational purposes. Always refer to your aircraft's Illustrated Parts Catalog (IPC) to verify part compatibility and specifications.
The 3102102-3 is a nickel alloy transition liner assembly for Honeywell T76-G-420/421 turbine engines. This component channels hot combustor gases into the turbine section, managing thermal flow between engine stages.
Hydraulic component compatibility depends on the aircraft system design. Common aviation hydraulic fluids include MIL-PRF-5606 (mineral-based), MIL-PRF-83282 (synthetic), and Skydrol (phosphate ester). Verify the LINER ASSY against your aircraft maintenance manual for fluid compatibility.
Overhauled and repaired hydraulic components are pressure-tested per manufacturer specifications and include 8130-3 documentation. The LINER ASSY is available in: Serviceable, Overhauled. Contact us for test documentation on your selected condition.
In-stock hydraulic components ship same business day before 3 PM EST. We provide 24/7 AOG support at (904) 998-9101 for urgent hydraulic system needs. RFQ submissions are typically quoted within 24 hours.