P/N: 5511132-32
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 5511132-32 is a structural frame component for the Cessna 560 Citation V upper fuselage. This aluminum bulkhead assembly maintains fuselage load paths and provides structural alignment at a critical station. Installed using AN/NAS fasteners per the aircraft's maintenance documentation, this frame integrates with surrounding fuselage sections to support pressurization loads and flight stresses.
Verify part compatibility with 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 5511132-32 is a structural frame component for the Cessna 560 Citation V upper fuselage. This aluminum bulkhead assembly maintains fuselage load paths and provides structural alignment at a critical station.
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: 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 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 5511132-32.