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MS20392-1C41 - Textron Aviation OEM Straight Headed Pin

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MS20392-1C41 – Textron Aviation OEM Straight Headed Pin (Clevis Pin)

Available now on the Airparts.aero Marketplace.

Overview

The MS20392-1C41 is a mil-spec, straight-headed pin, commonly known in the industry as a clevis pin, which has been specified by Textron Aviation for a precise application within their aircraft. This is not a generic hardware store pin; it is a precision-manufactured fastener designed to act as a semi-permanent shear pin in control linkages, clevis fittings, and various mechanical assemblies. Its purpose is to create a pivoting joint that securely connects two or more components while allowing for angular motion. The pin is secured in place by a cotter pin (sold separately) installed through the cross-drilled hole in its shank.

This particular pin is defined by its material—corrosion-resistant steel—and its unique, high length-to-diameter ratio. It is engineered for very specific, low-load applications where it may function as a hinge, an alignment dowel, or a connector in a non-primary-structural linkage. The use of a fully certified, OEM-specified MS20392-1C41 is critical to ensure the correct material properties, dimensional tolerances, and integrity of the assembly as intended by the airframe manufacturer.

Key Features

  • Mil-Spec Certified: Manufactured in strict accordance with the MS20392 military standard, ensuring absolute conformity and quality.

  • Corrosion-Resistant Steel: Fabricated from Type 303 stainless steel ("C" code), providing excellent corrosion resistance for long service life.

  • Passivated Finish: Chemically passivated to remove surface contaminants and enhance the formation of a protective chromium-oxide layer, further inhibiting corrosion.

  • Precision Machining: Machined to extremely tight diametrical and length tolerances for a perfect, slop-free fit in close-tolerance holes.

  • OEM Specified: Selected by Textron Aviation for a specific application, guaranteeing it meets all engineering requirements for that joint.

Technical Specifications

  • Part Number: MS20392-1C41

  • AN Number: AN392-41

  • Component Type: Pin, Straight, Headed (Clevis Pin)

  • OEM Designator: Textron Aviation

  • Standard: MS20392

  • Diameter (-1): 1/16 inch (0.0625")

  • Material (C): Corrosion-Resistant Steel (CRES), Type 303 (UNS S30300)

  • Grip Length (-41): 41/16 inches (2-9/16" or 2.5625")

  • Finish: Passivated per AMS2700 or equivalent.

  • Securing Provision: Cross-drilled hole for a 1/32" cotter pin (e.g., MS24665 series).


Aircraft Compatibility

  • Textron Aviation: Used on various Cessna and Beechcraft models where specified by the engineering drawing, Illustrated Parts Catalog (IPC), or maintenance manual for a specific, low-load application.

Note: The application of a clevis pin is extremely specific. The correct diameter and grip length must be used as called out by the official documentation. Substitution with a non-certified part is strictly prohibited.

Applications

  • Control System Linkages: Connecting push-pull tubes to bellcranks or control horns in secondary flight control systems (e.g., trim tabs).

  • Mechanical Assemblies: Serving as a pivot or hinge pin in landing gear mechanisms, access panels, or other mechanical systems.

  • Low-Load Shear Joints: Designed to carry loads perpendicular to the shank (shear), not in tension (pulling).

Why Choose MS20392-1C41?

Even the smallest piece of hardware on an aircraft is flight-critical. The MS20392-1C41 is a certified component with guaranteed material composition (CRES 303), finish (passivation), and dimensional accuracy. Using a generic, non-certified pin from a hardware store introduces immense risk. Such a part would lack the required corrosion resistance, could have incorrect dimensions leading to a loose and vibrating joint ("control slop"), or could be made from an unknown material with insufficient shear strength. This could lead to a failure of a control linkage or mechanical assembly. Sourcing a fully traceable, OEM-specified pin is a fundamental requirement for airworthy maintenance.

The material science behind the MS20392-1C41's "C" designation is a deliberate engineering choice. It specifies Corrosion-Resistant Steel (CRES) Type 303, which is an austenitic stainless steel from the 300 series. While many 300-series alloys are known for their toughness, Type 303 is specifically formulated with added sulfur to make it a "free-machining" grade. This is critical for manufacturing small, high-precision components like this pin, as it allows for faster machining speeds and a better surface finish. However, the sulfide inclusions can be potential corrosion initiation sites. To counteract this, the pin undergoes a crucial chemical passivation process, typically in a nitric acid bath per AMS2700. This process removes free iron and sulfide particles from the surface and promotes the formation of a dense, inert, and self-healing chromium-oxide passive film, ensuring the pin's long-term corrosion resistance in the aerospace environment.

Note: The MS20392-1C41 is a shear fastener and must be installed in a properly sized, reamed hole. It must be secured with the correct diameter cotter pin, which should be installed and bent in accordance with standard practices (e.g., AC 43.13-1B). Never use this pin in an application where it will be subjected to significant tensile (pulling) or bending loads.

Documentation

  • MS20392 Standard: The military standard sheet (e.g., NASM20392) defines all dimensional, material, and finish requirements for this series of pins and is publicly available through various online mil-spec libraries.

MS20392-1C41 Part Specifications: 

Head Style :Pan No. 2 (r1 Not Required In Item Description)
Chamfer Length :0.062" Inches Maximum
Diameter :0.122" Inches Minimum And 0.124" Inches Maximum
Under Head Length
:1.397" Inches Minimum And 1.417" Inches Maximum
Hole Arrangement Style
:One End Drilled
First Hole Diameter
:0.060" Inches Minimum And 0.080" Inches Maximum
Distance From Centerline Of Hole To End Of Pin
:
0.091" Inches Nominal
Hardness Rating
:26.5 Rockwell C Minimum Overall And 32.0 Rockwell C Maximum Overall
Pin Chamfer Angle
:14.5 Degrees Minimum And 15.5 Degrees Maximum
Shear Strength
:1840 Double Pound
Pin Head Diameter
:0.234" Inches Minimum And 0.266" Inches Maximum
Special Features
:The Shank End May Have Either A Chamfer Or Radius At The Option Of The Vendor
Height
:0.030 Inches Minimum And 0.062 Inches Maximum
Material
:Steel Comp 4037 Overall Or Steel Comp 4130 Overall Or Steel Comp 8630 Overall
Material Document And Classification


:

Ams 6300 Assn Std 1st Material Response Overall Or Mil-s-6758
Mil Spec 2nd Material Response Overall Or Mil-s-6050 Mil Spec 3rd Material Response Overall
Surface Treatment
:Cadmium Overall And Chromate Overall
Surface Treatment Document And Classification
:
Qq-p-416,ty 2 Cl 2 Fed Spec Single Treatment Response Overall
Style Designator
:Straight 



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