// Aerospace  ·  01

Limit Switch Bracket

Long-EZ Experimental Aircraft — Nose Gear Retraction System

Year 2024
Category Aerospace
Aircraft Long-EZ Experimental
Software SolidWorks
Material FormLabs Tough 2000 Resin
Status Prototype Complete  ·  Not Implemented
Limit Switch Bracket — Finished Prototype
// Finished Prototype FormLabs Tough 2000 Resin prototype — Long-EZ nose gear retraction system  ·  2024

Analyzed and resolved a critical landing gear malfunction on a Long-EZ experimental aircraft by diagnosing issues within the nose gear retraction system. The original bracket had sheared off due to incorrect positioning caused by malfunctioning limit switches — a damaged microswitch resulted in incorrect position indications, causing the actuator to over-travel. When the override was activated without accurate feedback, excessive force was applied to the bracket, ultimately shearing it off.

A replacement bracket was redesigned in SolidWorks and prototyped in FormLabs Tough 2000 Resin. The new design positions the sled close to the limit switches, ensuring the ramps on the top and bottom make contact to activate the up and down switches accurately — stopping rollers from falling into adjustment slots and restoring reliable nose gear position feedback.

The prototype was not ultimately implemented. During the process, it was determined that the limit switch the bracket was designed for was extremely cheap and prone to failure. Rather than continuing with a redesigned bracket around an unreliable component, the decision was made to invest in a full replacement of the original system — a more robust long-term solution.

// Key Specifications

Aircraft Long-EZ Experimental
System Nose Gear Retraction
Material FormLabs Tough 2000 Resin
Software SolidWorks
Microswitch Widely available replacement
Outcome Prototype complete — system fully replaced
Status Not Implemented

// NOTE — This prototype was not implemented.
Full system replacement was ultimately selected
over redesigning around an unreliable component.

What Went Wrong

01 — Root Cause

Root Cause

A damaged microswitch provided incorrect position indications to the nose gear retraction system, causing the actuator to over-travel beyond its intended range of motion.

02 — Failure Mode

Failure Mode

When the override was activated without accurate limit switch feedback, excessive force was applied to the bracket. The bracket sheared off due to the combined effect of incorrect positioning and actuator over-travel.

03 — Parts Scarcity

Parts Scarcity

The original limit switch components were obsolete and no longer available. The redesign adapted widely available microswitches as direct replacements, addressing both the mechanical failure and the parts scarcity problem.

Project Documentation

Original Bracket — Shear Failure

Original Bracket — Shear Failure

The original bracket sheared off due to incorrect positioning caused by malfunctioning limit switches. Actuator over-travel under override conditions applied excessive force to the bracket.

Nose Retraction System

Nose Retraction System

This bracket positions the sled (aluminum bar) close to the limit switches, ensuring the ramps on the top and bottom make contact to activate the up and down switches accurately.

Redesigned Bracket — Prototype

Redesigned Bracket — Prototype

The new bracket design stops rollers from falling into adjustment slots and ensures accurate gear position feedback. Easy to install and more durable than the original.

Build Log

Phase 01

Diagnose Malfunction

Performed hands-on inspection of the Long-EZ nose gear retraction system to identify the root cause of the landing gear malfunction. Traced the failure to a damaged microswitch providing incorrect position indications, causing actuator over-travel.

Inspected full nose gear retraction assembly
Identified damaged microswitch as root cause
Documented actuator over-travel failure mode
Confirmed bracket shear caused by excessive force
Phase 02

Inspect and Document Failed Bracket

Removed and documented the sheared bracket. Measured and recorded all critical dimensions, interface geometry, and mounting features to establish a baseline for the redesign.

Removed sheared bracket from aircraft
Measured all critical dimensions and geometry
Documented sled interface and switch positions
Photographed failure surfaces and context
Phase 03

Reverse Engineer Original Geometry

Reverse engineered the original bracket geometry from the failed part and surrounding system components to fully understand the design intent and identify improvements.

Reconstructed original geometry from measurements
Identified design weakness at shear point
Mapped sled ramp contact requirements
Defined improved geometry constraints
Phase 04

CAD Redesign — SolidWorks

Redesigned the bracket in SolidWorks with improved geometry to prevent roller fallout into adjustment slots and ensure accurate up/down switch activation. Adapted design to accommodate widely available replacement microswitches.

Modeled replacement bracket in SolidWorks
Designed ramp geometry for reliable switch activation
Prevented roller-slot interference in new design
Adapted mounting to accept replacement microswitches
Created engineering drawings for prototype
Phase 05

3D Print Prototype

Printed prototype in FormLabs Tough 2000 Resin — selected for its impact resistance and dimensional accuracy, appropriate for functional aerospace prototype validation.

Printed in FormLabs Tough 2000 Resin
Post-processed and cured per FormLabs spec
Inspected all critical dimensions post-print
Verified microswitch mounting interfaces
Phase 06

Test Fit and Iterate

Test fitted prototype in the nose gear retraction system. Verified sled positioning, ramp contact geometry, and switch activation timing. Iterated on geometry based on fitment findings.

Test fitted in Long-EZ nose gear system
Verified sled-to-switch clearances
Confirmed ramp contact activates both switches
Validated roller containment in new design
Phase 07Pivoted

Outcome and Decision

During the validation process, it was determined that the limit switch the bracket was designed for was extremely cheap and prone to premature failure. Continuing to design around an unreliable component was not an acceptable long-term solution. The decision was made to invest in a full replacement of the original system.

Evaluated long-term reliability of target microswitch
Determined component was unsuitable for aircraft use
Recommended full system replacement over patch repair
Prototype work concluded — system replacement selected

Skills Demonstrated

Engineering Analysis

Failure Mode Analysis Root Cause Diagnosis Actuator Over-Travel Analysis Reverse Engineering Engineering Judgment

CAD & Design

SolidWorks Modeling Design for Manufacturing Iterative Prototype Design Engineering Drawings Constraint-Based Design

Fabrication & Process

FormLabs Tough 2000 Resin SLA 3D Printing Post-Processing & Curing Test Fitting & Validation Hands-On Troubleshooting