RH MAIN GEAR STRUT(LEG) (P/N 1-4100-8) - As Removed

The 1-4100-8 is a right-hand main landing gear strut assembly designed to support aircraft weight during landing and taxi operations. This oleo-pneumatic shock absorber features a steel cylinder with internal piston rod and elastomeric seals that compress and extend to absorb touchdown impact and ground loads. The strut interfaces with the aircraft fuselage via upper attachment points and connects to the main wheel axle assembly below.

Installation requires verification against your aircraft's Illustrated Parts Catalog and compliance with manufacturer maintenance procedures. Proper strut function is critical for safe landing gear operation.

What is the RH MAIN GEAR STRUT(LEG) (P/N 1-4100-8)?

The 1-4100-8 is a right-hand main landing gear strut assembly designed to support aircraft weight during landing and taxi operations. This oleo-pneumatic shock absorber features a steel cylinder with internal piston rod and elastomeric seals that compress and extend to absorb touchdown impact and ground loads.

What aircraft models does the 1-4100-8 fit?

Part number 1-4100-8 is listed in multiple aircraft Illustrated Parts Catalogs. Always verify the RH MAIN GEAR STRUT(LEG) against your specific aircraft model's IPC and Type Certificate Data Sheet before ordering. Currently available in: As Removed.

Does the 1-4100-8 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 1-4100-8?

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 RH MAIN GEAR STRUT(LEG).