P/N: 105-530011-4
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 105-530011-4 is a structural frame component for aircraft fuselage assemblies, manufactured from aerospace aluminum or steel per Hawker Beechcraft specifications. This frame distributes loads and maintains alignment where skins, ribs, and longerons interface within the fuselage structure. Installation requires fastener torquing per the aircraft maintenance manual and FAA AC 43.13-1B guidance.
Used in general aviation and business aircraft fuselage substructures where primary structural integrity is critical.
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 105-530011-4 is a structural frame component for aircraft fuselage assemblies, manufactured from aerospace aluminum or steel per Hawker Beechcraft specifications. This frame distributes loads and maintains alignment where skins, ribs, and longerons interface within the fuselage structure.
The FRAME 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 FRAME. 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 105-530011-4.