P/N: 3101688-1
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).
| Condition | Stock |
|---|---|
| As Removed | 1 Available |
The 3101688-1 is a lock plate for aircraft structural fasteners, designed to prevent bolt and nut rotation under vibration and flight loads. After torquing a fastener to specification, the plate's tabs are bent against the bolt head or nut flats to create positive mechanical locking. Commonly installed at critical structural bolted joints on fuselage, wing, and empennage assemblies.
Installation follows FAA AC 43.13 guidance and your aircraft's approved maintenance manual or engineering authorization. Steel construction provides durability in high-vibration environments.
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 3101688-1 is a lock plate for aircraft structural fasteners, designed to prevent bolt and nut rotation under vibration and flight loads. After torquing a fastener to specification, the plate's tabs are bent against the bolt head or nut flats to create positive mechanical locking.
The 3101688-1 is currently available in the following conditions: As Removed. Each condition reflects the part's maintenance history and certification status per FAA standards.
The 3101688-1 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.