Welcome to Boeing distribution, formerly Aviall

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

GE Engines - TRIO II
Part # 1639M70P20=CK
Log Into view price
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
•Constructed from advanced materials for enhanced thermal resistance.
•Optimized aerodynamic profile to improve engine efficiency.
•Precision manufacturing techniques ensure consistent performance and reliability.

Benefits

•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.
Log in to view availability
NSN
 
Cage Code
 
Country of origin
United States 
ECCN / USML
9A991.c 
Schedule B
8411917010 
Dimensions (L x W x H)
5.75 x 4.25 x 4.5 IN
Total Shelf Life (days)
No Information
Hazmat Code
Package Weight
.738 LB
FAA Approval Code
PC
ISBN
 
Condition
Color
 
Brand
 
Hazmat(Y/N)
N 
LTL(Y/N)
N 
8130-3 Eligible
Yes 
Item Replacement History
  • 1639M70P17

Save to a new or existing list
New list name
Saved list
Save
     
Cancel