P/N: 22-3220-05-03
Category: Struts & Shock Absorbers
This product requires a custom quote. Please contact our sales team for pricing information or submit an RFQ (Request for Quote).
| Condition | Stock |
|---|---|
| New Surplus | 1 Available |
The 22-3220-05-03 is a threaded stud for shock absorber assemblies on aircraft landing gear. This fastener provides a secure attachment point for damper components and linkage connections within strut assemblies. Typically manufactured from steel with corrosion-resistant plating, the stud maintains alignment and load transfer during landing and taxi operations.
Installation requires proper torque specification and locking device per the Aircraft Maintenance Manual. Verify fitment against the Illustrated Parts Catalog before installation on your specific aircraft platform.
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.
The 22-3220-05-03 is a threaded stud for shock absorber assemblies on aircraft landing gear. This fastener provides a secure attachment point for damper components and linkage connections within strut assemblies.
Part number 22-3220-05-03 is listed in multiple aircraft Illustrated Parts Catalogs. Always verify the STUD, SHOCK ABSORBER against your specific aircraft model's IPC and Type Certificate Data Sheet before ordering. Currently available in: New Surplus.
Documentation varies by condition. Overhauled and repaired landing gear components include 8130-3 airworthiness tags. New surplus includes manufacturer documentation. Contact us for trace documentation on the specific condition you need.
Yes, we offer quantity discounts for fleet maintenance orders. Submit a Request for Quote (RFQ) specifying your required quantity, or call (904) 998-9101 to discuss fleet pricing for the STUD, SHOCK ABSORBER.