HUB (P/N apc23032-1900) - New Surplus
P/N: apc23032-1900
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 |
|---|---|
| New Surplus | 5 Available |
Product Description
The apc23032-1900 is a wheel hub assembly for aircraft landing gear systems. This component supports tapered roller bearings and transmits braking loads to the axle during wheel rotation and braking events. Typically fabricated from aluminum or steel, the hub provides the mounting interface for wheel assemblies on fixed-wing aircraft.
Installation requires torque specifications per the aircraft Maintenance Manual and verification against the Illustrated Parts Catalog to confirm applicability. Proper hub assembly ensures safe wheel operation and brake system functionality.
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 HUB (P/N apc23032-1900)?
The apc23032-1900 is a wheel hub assembly for aircraft landing gear systems. This component supports tapered roller bearings and transmits braking loads to the axle during wheel rotation and braking events.
What conditions is the apc23032-1900 available in?
The apc23032-1900 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 apc23032-1900?
The apc23032-1900 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 apc23032-1900?
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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