P/N: 204-040-236-1
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 | 3 Available |
The 204-040-236-1 is a structural plate designed for aircraft airframe assemblies. This component provides load distribution and reinforcement at mounting points and equipment interfaces. Installed in structural bays using MS or NAS fasteners, the plate aligns adjacent components and ensures reliable attachment under flight loads.
Verify fit against the aircraft's Illustrated Parts Catalog and follow torque specifications per the maintenance manual during installation. Common in general aviation and commercial aircraft structural repairs and assembly work.
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 204-040-236-1 is a structural plate designed for aircraft airframe assemblies. This component provides load distribution and reinforcement at mounting points and equipment interfaces.
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 204-040-236-1.