P/N: FW-212-83-305.2A
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 | 10 Available |
The FW-212-83-305.2A is an aerospace aluminum structural angle for airframe framing and load transfer. Extruded to AMS-QQ-A-200 or ASTM B221 specifications, this angle component provides rigidity and reinforcement in aircraft substructure assemblies. Installed as a stiffener in fuselage, wing, or empennage frameworks, it transfers loads between primary structure members.
Installation requires fastening per approved structural data and verification against the aircraft's Illustrated Parts Catalog. Consult the Structural Repair Manual for specific torque, spacing, and material compatibility requirements.
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. 2A is an aerospace aluminum structural angle for airframe framing and load transfer.
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-212-83-305.2A.