LEVER (P/N 25-9cf227-33a) - New Surplus
P/N: 25-9cf227-33a
Category: Linkages, Rods & Bellcranks
This product requires a custom quote. Please contact our sales team for pricing information or submit an RFQ (Request for Quote).
Available Inventory
| Condition | Stock |
|---|---|
| New Surplus | 1 Available |
Product Description
The 25-9cf227-33a is a metal lever for aircraft mechanical control linkages. This component translates input motion into controlled actuation when paired with rods, bellcranks, or shaft assemblies. The lever interfaces with bearings or pivot points to actuate flight controls, landing gear, flap systems, or other mechanical functions.
Installation requires proper rigging per the aircraft maintenance manual to ensure correct throw, alignment, and friction characteristics. Aerospace-grade construction supports precise movement under flight loads and environmental conditions.
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.
Frequently Asked Questions
What is the LEVER (P/N 25-9cf227-33a)?
The 25-9cf227-33a is a metal lever for aircraft mechanical control linkages. This component translates input motion into controlled actuation when paired with rods, bellcranks, or shaft assemblies.
What conditions is the 25-9cf227-33a available in?
The 25-9cf227-33a is currently available in the following conditions: New Surplus. Each condition reflects the part's maintenance history and certification status per FAA standards.
How do I get pricing for the 25-9cf227-33a?
The 25-9cf227-33a requires a custom quote. Submit a Request for Quote (RFQ) through our website or call our sales team at (904) 998-9101 for immediate pricing assistance.
Do you offer expedited shipping for the 25-9cf227-33a?
Yes, we offer same-day processing on in-stock items and provide 24/7 AOG (Aircraft on Ground) support for urgent needs. Standard, expedited, and overnight shipping options are available.
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