Traditional coordinate dimensioning uses basic dimensions with plus/minus tolerances to define part features. This approach works for simple geometries but falls short for complex aerospace components where form, orientation, location, and runout matter as much as size.
GD&T provides a standardized method to communicate exact part requirements using symbols, feature control frames, and datums. Instead of saying "this hole should be between 0.500" and 0.502" in diameter," GD&T specifies the hole's size, location relative to datums, perpendicularity to a surface, and allowable positional variation—all in a compact, unambiguous format.
For aerospace manufacturing, GD&T delivers critical advantages:
When completing FAIRs, GD&T knowledge directly impacts inspection correctness. Measuring a basic dimension without applying the associated geometric tolerance leads to incorrect pass/fail decisions and potential part rejection.
The feature control frame is GD&T's core element—a rectangular box containing all information needed to evaluate a geometric tolerance. Reading these frames correctly is essential for AS9102 inspection.
A feature control frame consists of compartments reading left to right:
Geometric Characteristic Symbol: The first compartment shows which geometric control applies—position, flatness, perpendicularity, profile, etc. Each symbol has a specific meaning defined by ASME Y14.5.
Tolerance Zone: The second compartment specifies the allowable variation, often preceded by a diameter symbol (Ø) when the tolerance zone is cylindrical. This might be followed by modifiers like "M" (Maximum Material Condition) or "L" (Least Material Condition) that affect how tolerance applies.
Datum References: Subsequent compartments identify the datum features used as references for measurement. Primary, secondary, and tertiary datums establish a coordinate system for evaluating the characteristic. These might also include material condition modifiers.
For example, a position callout might read: Ø 0.010 M | A | B M | C
This means: positional tolerance of 0.010" diameter at Maximum Material Condition, referenced to datum A (primary), datum B at MMC (secondary), and datum C (tertiary).
While ASME Y14.5 defines fourteen geometric characteristics, several appear frequently on aerospace drawings:
Position: Controls location of features like holes or slots relative to datums. Inspectors typically measure actual hole locations and calculate positional deviation using coordinate or CMM data.
Profile of a Surface/Line: Controls the shape of complex contours, ensuring surfaces stay within tolerance boundaries. Common on airfoil sections, organic shapes, and composite parts.
Perpendicularity/Parallelism/Angularity: Orientation controls ensuring features maintain specific angular relationships to datums. Critical for mating surfaces and assembly interfaces.
Flatness: Controls how much a surface can deviate from a perfect plane, independent of any datums. Important for sealing surfaces and mounting interfaces.
Concentricity/Runout: Controls how well cylindrical features share a common axis, critical for rotating components and bearing surfaces.
True Position: Often associated with hole patterns, this uses basic dimensions (shown in boxes on drawings) combined with position tolerance to define exact feature location.
When completing Form 3, each geometric tolerance requires appropriate measurement methods. Visual inspection doesn't suffice—you need CMM data, height gauge measurements, or specialized fixtures to generate valid results.
Understanding GD&T theory is one thing; applying it during inspection is another. Quality inspectors should remember:
Modern CMM software handles much of the geometric evaluation automatically, but quality engineers must still understand the requirements to program inspections correctly and validate results.
GD&T knowledge separates competent quality inspectors from exceptional ones. When you understand not just what to measure but why the engineer specified that particular geometric control, you can make better decisions about inspection methods, fixture design, and measurement uncertainty.
For AS9102 FAIRs, GD&T comprehension ensures Form 3 accurately reflects part conformance to design intent. This protects your shop from shipping nonconforming parts and demonstrates inspection competency to aerospace customers who expect GD&T fluency throughout their supply chain.
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