P/N: 4040t29g03
Category: Controls & Cables
This product requires a custom quote. Please contact our sales team for pricing information or submit an RFQ (Request for Quote).
| Condition | Stock |
|---|---|
| Serviceable | 24 Available |
The 4040t29g03 is a vane actuator lever for aircraft gas turbine compressor variable stator vane control systems. This steel linkage component transmits actuator displacement directly to the vane sector, controlling blade angle during engine operation. NSN 2840-01-087-1687.
Installed within the variable vane control linkage on General Electric engines, the lever responds to actuator motion and schedules stator vane pitch for optimal compressor efficiency across flight regimes. Installation follows engine maintenance manual specifications and 14 CFR Part 43 standards.
Please note: Product descriptions are provided for informational purposes. Always refer to your aircraft's Illustrated Parts Catalog (IPC) to verify part compatibility and specifications.
The 4040t29g03 is a vane actuator lever for aircraft gas turbine compressor variable stator vane control systems. This steel linkage component transmits actuator displacement directly to the vane sector, controlling blade angle during engine operation.
The LEVER may be available as an OEM (Original Equipment Manufacturer) or PMA (Parts Manufacturer Approval) part depending on condition and source. Both carry FAA certification for airworthiness. Currently available in: Serviceable. Contact us for sourcing details.
Installation hardware requirements vary by application. Check your aircraft's Structural Repair Manual (SRM) or Illustrated Parts Catalog (IPC) for the complete installation kit requirements for the LEVER. We stock related hardware and can help identify companion parts.
Yes, we ship airframe components worldwide. International orders typically arrive within 3-14 business days depending on destination. Export documentation and customs forms are included. Contact us for international shipping quotes on the 4040t29g03.