G.E. 4124T31P14 Stage 1 High Pressure Turbine Blade
  • G.E. 4124T31P14 Stage 1 High Pressure Turbine Blade
  • G.E. 4124T31P14 Stage 1 High Pressure Turbine Blade

G.E. 4124T31P14 Stage 1 High Pressure Turbine Blade

GE Engine Services

Part # 4124T31P14=CZ

8130-3 Eligible
8130-3 Eligible

The G.E. 4124T31P14 Stage 1 High Pressure Turbine Blade is a precision turbine component manufactured from advanced nickel-based superalloys for high-temperature strength, creep resistance, and oxidation resistance. It is used in General Electric turbine engine platforms configured with Stage 1 HPT assemblies. Exact engine compatibility should be verified by part number.

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Features & Benefits

  • Resistant to oxidation and corrosion at high temperatures
  • Reduces gas turbine engine downtime for improved operational efficiency
  • Coated with thermal barrier coating for enhanced performance
  • Increased efficiency, thus lowering fuel consumption
  • Highly reliable in harsh environmental conditions

Technical Information

FAA Approval Code

PC

Condition

New

CAGE Code

99207

Country of Origin

United States

Harmonized Tariff Schedule Code

8411917010

Storage Required

No

Lead Time (Days)

60

Shelf Life

No

Forecasted

Yes

Dimensions (L x W x H)

4.63 x 2.25 x 1.25 Inch

Package Weight

0.09 LB

Shipping Details

Hazmat Code

ZND

ECCN

9A991.d

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.