LINK (P/N din71802a10) - As Removed
P/N: din71802a10
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 DIN 71802A10 is an angled ball joint link combining a ball socket and ball stud for articulating push-pull rod connections. This steel component enables controlled movement in aircraft control-rod linkages and actuator mechanisms. Installation involves threading the link onto mating rods or studs and securing per aircraft maintenance manual requirements.
Safety-catch provisions must be observed where specified. The angled design accommodates directional changes in confined spaces while maintaining mechanical articulation.
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 LINK (P/N din71802a10)?
The DIN 71802A10 is an angled ball joint link combining a ball socket and ball stud for articulating push-pull rod connections. This steel component enables controlled movement in aircraft control-rod linkages and actuator mechanisms.
What conditions is the din71802a10 available in?
The din71802a10 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 din71802a10?
The din71802a10 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 din71802a10?
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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