P/N: 1234666-2
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 | 1 Available |
The 1234666-2 is a structural doubler for aircraft airframe reinforcement. This component distributes concentrated loads around fastener holes and skin discontinuities to prevent crack propagation in high-stress areas. Installed around fuselage cutouts, window frames, and attachment points using approved fasteners or adhesive bonding per maintenance manual specifications.
Commonly aluminum construction matching airframe skin gauge. Installation follows FAA AC 43.13-1B acceptable repair practices. Verify part applicability in 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 1234666-2 is a structural doubler for aircraft airframe reinforcement. This component distributes concentrated loads around fastener holes and skin discontinuities to prevent crack propagation in high-stress areas.
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 1234666-2.