P/N: 2700-45
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 2700-45 is a structural fitting designed to join and reinforce airframe members at critical load-transfer points. This component handles shear and tension forces at wing-to-fuselage attach joints and similar structural interfaces. Typically manufactured from aluminum alloy or steel per AN/MS/NAS aerospace standards.
Installation requires proper alignment, hardware torque specifications, and adherence to the aircraft's structural repair manual. Used across general aviation and commercial aircraft where reliable load distribution and structural integrity are essential.
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 2700-45 is a structural fitting designed to join and reinforce airframe members at critical load-transfer points. This component handles shear and tension forces at wing-to-fuselage attach joints and similar structural interfaces.
The FITTING 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 FITTING. 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 2700-45.