The 0310196-13 is a Piper/Cessna aircraft-grade spring part number used in light aircraft airframe and control system applications. Based on aviation parts cross-references, this component is generally categorized as a general-purpose airframe spring manufactured under Cessna aircraft part numbering conventions, and supplied through OEM or aftermarket aviation parts channels.

In practice, springs in the 0310196-series are typically used in mechanical linkage systems such as control surface return mechanisms, flap or trim system assist components, or other aircraft cabin/airframe mechanical assemblies where consistent tension, preload, or return force is required. The exact installation location can vary depending on aircraft model and configuration, as this part number family is used across multiple light aircraft applications.

These springs are designed for repeated cyclic loading under vibration, temperature variation, and continuous mechanical stress typical of general aviation operations. They are manufactured from high-carbon spring steel or corrosion-resistant alloy steel, selected to maintain elastic properties over long service life while resisting permanent deformation.

Because aircraft springs are safety-critical mechanical components, correct replacement requires matching both the part number and physical characteristics (length, hook geometry, wire diameter, and spring rate). Substitution with visually similar springs is not acceptable in certified maintenance without approved cross-reference documentation.

Key features include:

Piper / Cessna 0310196-13 aircraft spring (airframe/control system use)
Used in general aircraft mechanical linkage or return force systems
Designed for cyclic loading in vibration-prone aviation environments
Material: high-strength spring steel or corrosion-resistant alloy steel
Maintains consistent tension and elastic performance over time
May be used in control, flap, trim, or cabin mechanism assemblies (model-dependent)
Critical requirement: exact part number matching for airworthiness compliance
Subject to fatigue inspection and replacement during scheduled maintenance
Engineered for stable force output across repeated compression/extension cycles