P/N: n35-22740-0301-a01
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 | 5 Available |
The n35-22740-0301-a01 is a structural fitting designed to join airframe members in primary load paths. This component transfers shear and tension forces at spar, strut, and bracket junctions using standard AN or NAS fasteners for bolted connections. Installation requires torquing per aircraft SRM/AMM specifications, following FAA AC 43.13 methods when manufacturer data is unavailable.
Commonly used in wing and fuselage structural assemblies on general and commercial aircraft.
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 n35-22740-0301-a01 is a structural fitting designed to join airframe members in primary load paths. This component transfers shear and tension forces at spar, strut, and bracket junctions using standard AN or NAS fasteners for bolted connections.
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 n35-22740-0301-a01.