P/N: 25um821a
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 | 2 Available |
The 25um821a is an oleo-pneumatic landing gear strut designed to support aircraft weight during ground operations and absorb landing impacts. This shock absorber assembly combines hydraulic fluid and nitrogen gas to dampen vertical loads during taxi, takeoff, and landing cycles. The strut maintains structural integrity under repeated compression and extension cycles common in general aviation and commercial aircraft landing gear systems.
Service and maintenance follow SAE ARP5908 guidelines and aircraft-specific AMM procedures. Verify compatibility with 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.
The 25um821a is an oleo-pneumatic landing gear strut designed to support aircraft weight during ground operations and absorb landing impacts. This shock absorber assembly combines hydraulic fluid and nitrogen gas to dampen vertical loads during taxi, takeoff, and landing cycles.
Part number 25um821a 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.