G.E. 4128T10P02 Stage 6-10 Compressor Rotor Blade Lock

GE Engine Services

Part # 4128T10P02=CZ

8130-3 Eligible
8130-3 Eligible
G.E. 4128T10P02 Stage 6-10 Compressor Rotor Blade Lock is critical flight hardware designed to secure compressor blades within stages 6 through 10 of the high-pressure compressor assembly, enhancing the operational efficiency of gas turbine engines.
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Overview

G.E. 4128T10P02 Blade Lock ensures the secure retention of rotor blades during high-speed operations, contributing to the overall reliability and performance of the engine. Engineered with precision, this blade lock features high-quality materials that withstand extreme temperatures and pressures, making it an suitable choice for demanding aerospace applications. Its robust design prevents blade movement during operation, ensuring optimal performance and safety in gas turbine engines.

Features & Benefits

  • Designed for secure retention of rotor blades in gas turbine engines
  • Manufactured from high-quality materials for durability and performance
  • Enhances engine reliability by preventing blade movement during operation
  • Contributes to improved engine performance and efficiency
  • Reduces maintenance needs through robust design and material selection

Technical Information

FAA Approval Code

PC

Condition

New

CAGE Code

99207

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)

8.25 x 6 x 0.32 Inch

Package Weight

0.01 LB

Shipping Details

Hazmat Code

ZND

ECCN

9A991.d

Schedule B

8411917010

8130-3 Eligible

Yes

Hazmat

No

Part Explosive

No

Item Replacement History

  • 4128T10P02=CILOCK: BLADE,COMPRESSOR ROTOR,STG 6-10, ONLY SOH AVAILABLE
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.