P/N: 65249-000
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 | 2 Available |
The 65249-000 is a structural backing plate for the stabilator trim rib assembly on Piper PA-28-180 aircraft. This aluminum plate distributes loads at riveted joint locations, reinforcing the trim mechanism structure. Installed perpendicular to the stabilator surface, it supports the trim actuator interface and maintains structural integrity during flight loads and control inputs.
Installation follows the aircraft maintenance manual with standard riveted fastening per FAA AC 43.13-1B guidance.
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 65249-000 is a structural backing plate for the stabilator trim rib assembly on Piper PA-28-180 aircraft. This aluminum plate distributes loads at riveted joint locations, reinforcing the trim mechanism structure.
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 65249-000.