P/N: 207-8032-1101
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 |
|---|---|
| Serviceable | 1 Available |
The 207-8032-1101 is a machined structural fitting for load transfer between airframe members in fuselage frame joints. This aircraft-grade metal component aligns and secures mating brackets or frames, providing rigid connection points where fuselage sections meet. Installation requires specified torque values and fastener callouts per the aircraft maintenance manual.
Verify applicability in the Illustrated Parts Catalog before use on certificated 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 207-8032-1101 is a machined structural fitting for load transfer between airframe members in fuselage frame joints. This aircraft-grade metal component aligns and secures mating brackets or frames, providing rigid connection points where fuselage sections meet.
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: Serviceable. 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 207-8032-1101.