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BL,FAN RTR-STG1,

General Electric Aircraft Engines
Part # 9531M21P19=CW
The 9531M21P19 compressor blade from G.E. is constructed from high-strength titanium alloy, specifically designed to perform efficiently in compressor applications. This blade optimizes airflow and enhances the overall performance of the compressor system. Its lightweight yet durable design ensures reliability under demanding conditions, contributing to effective operation in various environments.

Features:
• Constructed from durable titanium alloy for excellent quality

Benefits:
• Ensures reliable performance in high-stress environments
• Enhances overall efficiency and durability of the compressor system

SPECIFICATIONS
• Engine Section Location: Fan
• End Item Identification: F110-100Engine
• Material: Titanium Alloy Blade
• Stage Number: 1
• Reference Data and Literature: 2J-F110-4
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NSN
 
Cage Code
07482 
Country of origin
Israel 
ECCN / USML
9A619.x 
Schedule B
8411917050 
Dimensions (L x W x H)
11.75 x 5 x 3.75 IN
Total Shelf Life (days)
No Information
Hazmat Code
Package Weight
1.592 LB
FAA Approval Code
NO
ISBN
 
Condition
Color
 
Brand
 
Hazmat(Y/N)
N 
LTL(Y/N)
N 
8130-3 Eligible
No 

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