P/N: 365a84-3235-27
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 |
|---|---|
| New Surplus | 4 Available |
The 365a84-3235-27 is a structural doubler used to reinforce aircraft sheet metal around cutouts, repairs, and high-stress areas. This aluminum reinforcement plate distributes loads across damaged or thinned skin, restoring stiffness and structural integrity per FAA AC 43.13-1B repair standards. Installed with MS20470 or MS20426 solid and countersunk rivets following OEM Structural Repair Manual (SRM) specifications.
Common in wing, fuselage, and tail repairs where local reinforcement prevents crack propagation and maintains airframe strength.
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 365a84-3235-27 is a structural doubler used to reinforce aircraft sheet metal around cutouts, repairs, and high-stress areas. This aluminum reinforcement plate distributes loads across damaged or thinned skin, restoring stiffness and structural integrity per FAA AC 43.
The DOUBLER 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 DOUBLER. 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 365a84-3235-27.