P/N: FW-212-83-305.1A
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 | 26 Available |
The FW-212-83-305.1A is an L-section structural angle for aircraft airframe reinforcement. This aluminum extrusion stiffens fuselage frames, ribs, and brackets by providing localized reinforcement to primary and secondary structure. Manufactured to AMS/QQA material standards for aerospace applications.
Installation follows aircraft structural repair manual specifications or FAA AC 43.13-1B guidance when OEM data is unavailable. Commonly used in frame repair, rib reinforcement, and bracket stiffening 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 FW-212-83-305. 1A is an L-section structural angle for aircraft airframe reinforcement.
The ANGLE 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 ANGLE. 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 FW-212-83-305.1A.