SHOCK STRUTH (P/N ca-251-1b) - Serviceable

The ca-251-1b is an oleo-pneumatic shock strut for aircraft main landing gear. This component absorbs touchdown and taxi loads while damping rebound motion through a sealed air-oil design. Hydraulic fluid and nitrogen work together to provide progressive resistance during compression and extension cycles.

Mounted between the gear trunnion and axle, the strut maintains proper extension and inflation settings critical for safe landing operations. Service and installation follow aircraft maintenance manual specifications and 14 CFR Part 43 requirements.

What is the SHOCK STRUTH (P/N ca-251-1b)?

The ca-251-1b is an oleo-pneumatic shock strut for aircraft main landing gear. This component absorbs touchdown and taxi loads while damping rebound motion through a sealed air-oil design.

What aircraft models does the ca-251-1b fit?

Part number ca-251-1b is listed in multiple aircraft Illustrated Parts Catalogs. Always verify the SHOCK STRUTH against your specific aircraft model's IPC and Type Certificate Data Sheet before ordering. Currently available in: Serviceable.

Does the ca-251-1b include an 8130-3 tag and maintenance records?

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.

Do you offer volume pricing for fleet orders of the ca-251-1b?

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 SHOCK STRUTH.