P/N: 5475201-1
Category: Doors & Access Panels
This product requires a custom quote. Please contact our sales team for pricing information or submit an RFQ (Request for Quote).
| Condition | Stock |
|---|---|
| New Surplus | 2 Available |
The 5475201-1 is a structural safety plate assembly for the thrust reverser door on Hawker 850XP aircraft. This reinforcement plate maintains joint integrity at the nacelle door interface and provides critical attachment points under stow loads. Installed as part of the T/R door structure to support proper door operation and prevent structural movement during thrust reverser cycles.
Installation follows the Aircraft Maintenance Manual specifications. Verify compatibility with your 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 5475201-1 is a structural safety plate assembly for the thrust reverser door on Hawker 850XP aircraft. This reinforcement plate maintains joint integrity at the nacelle door interface and provides critical attachment points under stow loads.
The SAFTEY PLATE ASSEMBLY, T/R DOOR 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: New Surplus. 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 SAFTEY PLATE ASSEMBLY, T/R DOOR. 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 5475201-1.