204-011-179-001 – CLEVIS, ROD END, AVIATION

Description

204-011-179-001 – CLEVIS, ROD END, AVIATION

Specifications

Style/Shape: Clevis
Surface Treatment: Cadmium
Material: Steel
Distance From Pivot Pinhole Center To Rod Connection End: 4.990″ Min – 5.010″ Max
End Radius: 0.970″ Min – 1.000″ Max
Fork Arm Thickness: 0.490Mm Nom And 0.510Cm Nom
Fork Depth: 3.490″ Min – 3.510″ Max
Fork Span Width: 1.950″ Min – 1.960″ Max
Hole Diameter: 0.8744″ Min – 0.8748″ Max
Overall Width: 2.950″ Min – 2.960″ Max
Shank Diameter: 1.940″ Min – 2.000″ Max
Thread Class: 3B Rod Connection
Thread Direction: Right-Hand Rod Connection
Thread Length: 1.500″ Nom Rod Connection
Thread Series Designator: Unf Rod Connection
Thread Size: 1.500″ Rod Connection
Manufacturer: Bell
Aircraft Model Compatibility: Bell 204

Part Number: 204-011-179-001
Unpunctuated: 204011179001

The specifications above are for reference only. Verify tolerances and details in the official spec sheets before use.

AVBOX US Certificate of Conformance: This product comes with an AVBOX US Certificate of Conformance (CoC), assuring that the part(s) meet specified design, quality, and regulatory standards at the time of manufacture, providing confirmation of compliance and adherence to applicable aviation requirements.

Part Numbers, Alternates & Reference Info: We ship the exact part number shown in the product title/description when in stock. Any NSNs or alternate part numbers listed are for traceability/reference only. If a compatible alternate is the only option available, we will contact you before shipping to confirm acceptance. Specifications are compiled from multiple sources and provided for convenience; always verify fit, tolerances, and requirements in the official spec sheets and applicable repair manuals/IPCs before purchase. If specific documentation (e.g., 8130 or company CoC/trace) is required, please contact us before ordering. We do not provide usage/support guidance, please refer to the manuals. Ordering the wrong part can extend lead times and result in aircraft downtime.