P/N: 755-818
Category: Structural Components
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 755-818 is a torque plate for Piper PA-28 series aircraft main wheel brake assemblies. This steel component transfers braking loads from the Cleveland wheel and brake system to the landing gear structure, ensuring safe load distribution during landing and taxi operations. Installation requires manufacturer-specified torque values and new lockwire per FAA AC 43.13-1B standards.
Verify applicability in the 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 755-818 is a torque plate for Piper PA-28 series aircraft main wheel brake assemblies. This steel component transfers braking loads from the Cleveland wheel and brake system to the landing gear structure, ensuring safe load distribution during landing and taxi operations.
The PLATE: may be available as an OEM (Original Equipment Manufacturer) or PMA (Parts Manufacturer Approval) part depending on condition and source. Both carry FAA certification for airworthiness. Currently available in: As Removed. Contact us for sourcing details.
Installation hardware requirements vary by application. Check your aircraft's Structural Repair Manual (SRM) or Illustrated Parts Catalog (IPC) for the complete installation kit requirements for the PLATE:. We stock related hardware and can help identify companion parts.
Yes, we ship airframe components worldwide. International orders typically arrive within 3-14 business days depending on destination. Export documentation and customs forms are included. Contact us for international shipping quotes on the 755-818.