P/N: 19c02-12a
Category: Lighting
This product requires a custom quote. Please contact our sales team for pricing information or submit an RFQ (Request for Quote).
| Condition | Stock |
|---|---|
| New | 2 Available |
The 19c02-12a is a loop-type cushioned clamp designed to secure aircraft lighting wire bundles and conduit to structural members. Manufactured with elastomeric cushioning, it provides strain relief and chafe protection during vibration and thermal cycling. The clamp features an eyelet for fastener attachment and follows AS21919/MS21919 standards for aviation applications.
Installation requires appropriate fasteners torqued per aircraft maintenance manual specifications. Commonly used in lighting harness routing throughout cockpit, cabin, and exterior lighting systems on general and commercial aircraft.
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 19c02-12a is a loop-type cushioned clamp designed to secure aircraft lighting wire bundles and conduit to structural members. Manufactured with elastomeric cushioning, it provides strain relief and chafe protection during vibration and thermal cycling.
The CLAMP 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. 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 CLAMP. 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 19c02-12a.