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CLIP, RETAINING,

General Electric Aircraft Engines
Part # 9523M21P01=CW
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SPECIFICATIONS
• Material: Nickel Alloy Outer Case
• Material Thickness: 0.077 Inches Minimum and 0.085 Inches Maximum
• Stage Number: 1
• Overall Length: 0.254 Inches Minimum and 0.375 Inches Maximum
• Engine Section Location: High Pressure Turbine
• End Item Identification: B1B Aircraft/F108 Aircraft Engineine
• Design Type: Compressor
• Overall Length: 0.254 Inches Minimum and 0.375 Inches Maximum
• Engine Section Location: High Pressure Turbine
• End Item Identification: B1B Aircraft/F108 Aircraft Engineine
• Material Thickness: 0.077 Inches Minimum and 0.085 Inches Maximum
• Stage Number: 1
• Design Type: Compressor
• Material: Nickel Alloy Outer Case
Material is non forecasted. Orders can not be canceled or returned. Please see our returnspolicy for more information.
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NSN
 
Cage Code
07482 
Country of origin
China 
ECCN / USML
EAR99 
Schedule B
7318240000 
Dimensions (L x W x H)
4 x .5 x .25 IN
Total Shelf Life (days)
No Information
Hazmat Code
Package Weight
.066 LB
FAA Approval Code
PC
ISBN
 
Condition
Color
 
Brand
 
Hazmat(Y/N)
N 
LTL(Y/N)
N 
8130-3 Eligible
Yes 
Forecasted
No

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