P/N: 204-011-180-003
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 204-011-180-003 is a machined steel structural fitting for Bell helicopter drag brace assemblies. This component provides the load-transfer interface where the rotor-system drag brace attaches to the airframe structure. Manufactured from aerospace-grade steel per NAS/MS standards, the fitting ensures secure alignment and load distribution during flight operations.
Installation follows the aircraft maintenance manual specifications for your specific Bell model. Verify compatibility in the Illustrated Parts Catalog before ordering.
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 204-011-180-003 is a machined steel structural fitting for Bell helicopter drag brace assemblies. This component provides the load-transfer interface where the rotor-system drag brace attaches to the airframe structure.
The FITTING 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 FITTING. 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 204-011-180-003.