P/N: 25ct477ac
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 |
|---|---|
| As Removed | 1 Available |
The 25ct477ac is a landing gear shock strut assembly component designed for oleo‑pneumatic damping systems. It absorbs touchdown and taxi loads through a combination of compressed nitrogen gas and hydraulic fluid (MIL‑PRF‑5606/83282), reducing impact forces on the airframe. Installed within the main or nose gear shock strut, this component provides structural support while maintaining ride quality during ground operations.
Service and installation follow the aircraft maintenance manual and FAA AC 43.13‑1B guidance, with proper nitrogen charging and hydraulic fluid specifications critical to performance.
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 25ct477ac is a landing gear shock strut assembly component designed for oleo‑pneumatic damping systems. It absorbs touchdown and taxi loads through a combination of compressed nitrogen gas and hydraulic fluid (MIL‑PRF‑5606/83282), reducing impact forces on the airframe.
Part number 25ct477ac is listed in multiple aircraft Illustrated Parts Catalogs. Always verify the STRUT against your specific aircraft model's IPC and Type Certificate Data Sheet before ordering. Currently available in: As Removed.
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 STRUT.