P/N: 5511152-200
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 5511152-200 is a structural frame component for Cessna Citation 550/560 series aircraft. This aluminum load-distribution member mounts within fuselage bays to support and position critical airframe components. The frame interfaces with surrounding structure through multiple fastener points, maintaining fuselage integrity and component alignment during flight operations.
Installation requires torque verification per Cessna Aircraft Maintenance Manual specifications and confirmation against the aircraft Illustrated Parts Catalog. OEM Cessna part (CAGE 71379).
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 5511152-200 is a structural frame component for Cessna Citation 550/560 series aircraft. This aluminum load-distribution member mounts within fuselage bays to support and position critical airframe components.
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 5511152-200.