P/N: 25tf181
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 | 1 Available |
The 25tf181 is a structural reinforcement plate designed to distribute fastener loads at airframe joints. This aluminum or steel doubler installs at skin-to-frame connections to strengthen the joint and prevent stress concentration around fasteners. The plate conforms to applicable aerospace material specifications and airframe drawings.
Installation follows the aircraft structural repair manual, with proper fastener torque and spacing per manufacturer requirements. Verify part number in the 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 25tf181 is a structural reinforcement plate designed to distribute fastener loads at airframe joints. This aluminum or steel doubler installs at skin-to-frame connections to strengthen the joint and prevent stress concentration around fasteners.
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 25tf181.