CONROD (P/N 25-8cw335-1a) - As Removed
P/N: 25-8cw335-1a
Category: General Aircraft Parts
Shipping for this part is quoted to your address. We email you the total to approve before anything is charged.
Available Inventory
| Condition | Price | Stock |
|---|---|---|
| As Removed | $1850.00 | 4 Available |
Product Description
The 25-8cw335-1a is a control rod for aircraft flight-control linkages. This conrod transmits push-pull motion between control levers and bellcranks in mechanical flight-control systems. Designed for Hawker Beechcraft airframes, the rod features precision rod-end hardware and connects to control surfaces through rigging assemblies.
Installation requires matching the rod length and end-fitting style to aircraft specifications per the maintenance manual. Secure all connections with AN/MS standard fasteners and torque per OEM requirements to ensure proper control authority and system integrity.
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 CONROD (P/N 25-8cw335-1a)?
The 25-8cw335-1a is a control rod for aircraft flight-control linkages. This conrod transmits push-pull motion between control levers and bellcranks in mechanical flight-control systems.
What conditions is the 25-8cw335-1a available in?
The 25-8cw335-1a is currently available in the following conditions: As Removed. Each condition reflects the part's maintenance history and certification status per FAA standards.
How do I get pricing for the 25-8cw335-1a?
The 25-8cw335-1a 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 25-8cw335-1a?
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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