212-011-704-107 (P/N TRUNNION ASSY) - As Removed
P/N: TRUNNION ASSY
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 | 1 Available |
Product Description
The 212-011-704-107 trunnion assembly is a structural pivot component in helicopter main rotor hub systems. It provides the bearing interface between the rotor yoke and hub, enabling controlled flapping motion of rotor blades during flight. This assembly is installed during rotor hub maintenance and overhaul procedures.
Installation requires torque specifications and lubrication per the applicable helicopter maintenance manual. Verify part compatibility in your aircraft's 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 212-011-704-107 (P/N TRUNNION ASSY)?
The 212-011-704-107 trunnion assembly is a structural pivot component in helicopter main rotor hub systems. It provides the bearing interface between the rotor yoke and hub, enabling controlled flapping motion of rotor blades during flight.
What conditions is the TRUNNION ASSY available in?
The TRUNNION ASSY 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 TRUNNION ASSY?
The TRUNNION ASSY 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 TRUNNION ASSY?
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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