PLATE (P/N 755-888) - As Removed
P/N: 755-888
Category: Plates, Doublers & Reinforcements
This product requires a custom quote. Please contact our sales team for pricing information or submit an RFQ (Request for Quote).
Available Inventory
| Condition | Stock |
|---|---|
| As Removed | 6 Available |
Product Description
The 755-888 is a flat mounting plate that serves as a structural interface for securing aircraft components. It distributes loads between brackets and airframe structures, preventing stress concentration at attachment points. Constructed from aluminum or steel per aircraft-specific drawings, the plate's thickness and finish vary by application requirements.
Installation follows the applicable aircraft maintenance manual or structural repair manual, with part number verification against the Illustrated Parts Catalog. Common in general aviation and commercial aircraft structural assemblies.
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.
Frequently Asked Questions
What is the PLATE (P/N 755-888)?
The 755-888 is a flat mounting plate that serves as a structural interface for securing aircraft components. It distributes loads between brackets and airframe structures, preventing stress concentration at attachment points.
What conditions is the 755-888 available in?
The 755-888 is currently available in the following conditions: As Removed. Each condition reflects the part's maintenance history and certification status per FAA standards.
How do I get pricing for the 755-888?
The 755-888 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.
Do you offer expedited shipping for the 755-888?
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.
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