P/N: 756-818
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 | 4 Available |
The 756-818 is a torque plate assembly for aircraft wheel and brake systems. This component reacts braking torque and maintains caliper alignment during landing and taxi operations. Mounted on the fixed axle side, the plate anchors the brake assembly while allowing controlled force distribution through standard AN/MS/NAS fasteners.
Steel construction provides the rigidity needed to withstand repeated braking cycles. Installation requires qualified personnel following the wheel-and-brake Component Maintenance Manual (CMM) and aircraft Illustrated Parts Catalog specifications.
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 756-818 is a torque plate assembly for aircraft wheel and brake systems. This component reacts braking torque and maintains caliper alignment during landing and taxi operations.
The TORQUE PLATE ASSEMBLY - (75-16) 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 TORQUE PLATE ASSEMBLY - (75-16). 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 756-818.