P/N: 20-1200-01-01
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 20-1200-01-01 jack point plate reinforces designated aircraft jacking stations on the fuselage and wings. This structural component creates a stable interface between the airframe and wing or tripod jacks during maintenance operations. Installed at factory-specified jack points, it distributes concentrated loads across a wider area, preventing airframe damage during tire changes, landing gear service, and other routine maintenance.
Follow aircraft Structural Repair Manual or Illustrated Parts Catalog procedures for correct installation location and fastening.
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 20-1200-01-01 jack point plate reinforces designated aircraft jacking stations on the fuselage and wings. This structural component creates a stable interface between the airframe and wing or tripod jacks during maintenance operations.
The JACK POINT PLATE 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 JACK POINT PLATE. 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 20-1200-01-01.