CONNECTING LINK (P/N 206-010-710-3) - As Removed
P/N: 206-010-710-3
Category: General Aircraft Parts
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 |
|---|---|
| As Removed | 4 Available |
Product Description
The 206-010-710-3 is an aluminum alloy connecting link manufactured by Bell Helicopter Textron for aircraft mechanical linkages. This rigid coupling component transmits motion between bellcranks and control rods in flight-control systems. The link maintains precise alignment and load transfer in control linkage assemblies, ensuring smooth actuation of flight surfaces.
Installation requires AN/MS/NAS hardware per the aircraft maintenance manual. Verify compatibility with the Illustrated Parts Catalog before installation.
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 CONNECTING LINK (P/N 206-010-710-3)?
The 206-010-710-3 is an aluminum alloy connecting link manufactured by Bell Helicopter Textron for aircraft mechanical linkages. This rigid coupling component transmits motion between bellcranks and control rods in flight-control systems.
What conditions is the 206-010-710-3 available in?
The 206-010-710-3 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 206-010-710-3?
The 206-010-710-3 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 206-010-710-3?
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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