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G.E. 1639M70P20 TRIO II Stage 1 High Temperature Turbine Blade
  • G.E. 1639M70P20 TRIO II Stage 1 High Temperature Turbine Blade
  • G.E. 1639M70P20 TRIO II Stage 1 High Temperature Turbine Blade
  • G.E. 1639M70P20 TRIO II Stage 1 High Temperature Turbine Blade
  • G.E. 1639M70P20 TRIO II Stage 1 High Temperature Turbine Blade
  • G.E. 1639M70P20 TRIO II Stage 1 High Temperature Turbine Blade
  • G.E. 1639M70P20 TRIO II Stage 1 High Temperature Turbine Blade

G.E. 1639M70P20 TRIO II Stage 1 High Temperature Turbine Blade

GE Engines TRIO II

Part # 1639M70P20=CK

8130-3 Eligible
8130-3 Eligible
The G. E. TRIO II Stage 1 High Temperature Turbine Blade is crafted for gas turbine engines, capable of enduring high temperatures and pressures. Its advanced material design promotes durability and efficiency, making it suitable for challenging aerospace applications where reliable performance is essential.
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Boeing Distribution (formerly Aviall)
InfoAllocation Control: Allocation control is a process used to ensure fair allocation of assets. It is applied to parts with limited availability and high customer demand. Due to the nature of allocation control items, there is the possibility that stock shown as available may already be allocated based on previously received customer order(s). Specific questions related to allocation control, please contact Boeing Customer Support.

Overview

1639M70P20 G.E. TRIO II Stage 1 High Temperature Turbine Blade is engineered for advanced performance in gas turbine engines. This component is designed to withstand extreme temperatures and pressures, ensuring reliable operation in demanding environments. Its innovative design incorporates advanced materials that enhance durability and efficiency, making it an ideal choice for modern aerospace applications.

Features & Benefits

  • Constructed from advanced materials for enhanced thermal resistance.
  • Optimized aerodynamic profile to improve engine efficiency.
  • Precision manufacturing techniques ensure consistent performance and reliability.
  • Increased engine performance and fuel efficiency through reduced drag.
  • Extended service life due to superior material properties, reducing maintenance costs.
  • Enhanced operational reliability in high-stress conditions, contributing to overall system performance.

Technical Information

FAA Approval Code

PC

Condition

New

Country of Origin

United States

Harmonized Tariff Schedule Code

8411917010

Lead Time (Days)

270

Shelf Life

No

Forecasted

Yes

Dimensions (L x W x H)

5.75 x 4.25 x 4.50

Package Weight

0.74 LB

Aircraft Makes

Boeing

Aircraft Models

747-400PC
747-400ERF
767-400
767-200SF
767-200
767-200ERSF
8 more

Engine Makes

GE

Engine Models

CF6-80C2B1

Shipping Details

Hazmat Code

ZND

ECCN

9A991.c

Schedule B

8411917010

8130-3 Eligible

Yes

Hazmat

No

Part Explosive

No

Item Replacement History

Buy now from
Boeing Distribution (formerly Aviall)
DISCLAIMER: Product information provided “as is.” Boeing may add, change, discontinue or remove this information at any time. Product photos may not be exact match to product delivered. See terms & conditions.