P/N: 6511015-88
Category: General Aircraft Parts
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 | 2 Available |
The 6511015-88 is a structural stiffener that reinforces sheet-metal panels and assemblies in aircraft fuselage and wing structures. This aluminum component limits panel flexing under flight loads and maintains aerodynamic contour by managing load paths through the airframe. Commonly used in Cessna Citation 550/560 series aircraft where localized stiffening prevents buckling and fatigue cracking in high-stress areas.
Installation requires verification against the aircraft's Illustrated Parts Catalog and compliance with OEM Structural Repair Manual procedures and FAA AC 43.13-1B sheet-metal practices.
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 6511015-88 is a structural stiffener that reinforces sheet-metal panels and assemblies in aircraft fuselage and wing structures. This aluminum component limits panel flexing under flight loads and maintains aerodynamic contour by managing load paths through the airframe.
The 6511015-88 is currently available in the following conditions: New Surplus. Each condition reflects the part's maintenance history and certification status per FAA standards.
The 6511015-88 requires a custom quote. Submit a Request for Quote (RFQ) through our website or call our sales team at (904) 998-9101 for immediate pricing assistance.
Yes, we offer same-day processing on in-stock items and provide 24/7 AOG (Aircraft on Ground) support for urgent needs. Standard, expedited, and overnight shipping options are available.