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ASME Y14.5

ASME Y14.5 is a standard published by the American Society of Mechanical Engineers (ASME) that establishes symbols, rules, definitions, requirements, defaults, and practices for dimensioning and tolerancing, with a primary focus on geometric dimensioning and tolerancing (GD&T) for engineering drawings, digital models, and related documents. The standard defines principles and methods to control the form, orientation, location, and runout of part features using a datum reference frame, enabling precise specification of geometric tolerances such as positional tolerancing, profile, and runout. Its core purpose is to provide a uniform language for stating and interpreting dimensional and geometric tolerancing requirements, ensuring clear communication of engineering design intent, complete feature definition, and standardization for manufacturing, inspection, and assembly. By emphasizing functional relationships in datum selection and minimizing ambiguities, ASME Y14.5 supports interchangeability of parts, reduces manufacturing errors, and accommodates both traditional orthographic projections and model-based product definition. First issued in earlier forms dating back to the and evolving through revisions, the current edition—ASME Y14.5-2018—was approved on August 13, 2018, and issued on February 11, 2019, reaffirmed in 2024. Key features include the use of feature control frames to specify tolerances at maximum material condition () or least material condition (LMC), composite tolerancing for patterns and feature relationships, and rules for projecting tolerance zones to align with assembly needs. As the authoritative U.S. national standard for GD&T, it is integral to industries like , automotive, and , where it guides the creation and verification of compliant parts.

Introduction

Overview

ASME Y14.5-2018 (reaffirmed 2024) is the authoritative standard developed by the (ASME) that establishes symbols, rules, definitions, and requirements for dimensioning and tolerancing in engineering drawings, models defined in digital data files, and associated documents. It provides a comprehensive framework for communicating design intent precisely, ensuring consistency across manufacturing, inspection, and quality control processes in . At its core, ASME Y14.5 focuses on (GD&T), a symbolic language used to define the allowable variation in the form, size, orientation, and location of part features relative to datums. This approach goes beyond traditional coordinate dimensioning by emphasizing functional relationships between features, enabling tighter control over part assembly and performance while reducing manufacturing costs through optimized tolerances. The standard is structured into nine main sections, spanning from scope and general principles to specific tolerances for form, orientation, location, profile, and runout. In recognition of its importance, ASME Y14.5 was adopted by the U.S. Department of Defense on February 9, 2009, for mandatory use in contracts requiring engineering drawings.

Purpose and benefits

The ASME Y14.5 standard establishes uniform practices for defining and communicating engineering requirements in mechanical design through a symbolic language of geometric dimensioning and tolerancing (GD&T), ensuring that precision and functional requirements are clearly conveyed on drawings and models. This uniformity reduces ambiguity inherent in traditional coordinate tolerancing methods, such as plus/minus dimensions, by providing standardized rules, definitions, and symbols that minimize interpretation errors across design, manufacturing, and inspection teams. By promoting interchangeability of parts, the standard facilitates consistent fit and assembly, allowing components from different suppliers to meet functional objectives without excessive rework. Key benefits of ASME Y14.5 include significant cost reductions achieved through functional tolerancing, which allocates tolerances based on part performance rather than arbitrary limits, thereby decreasing material waste, scrap rates, and production delays. It enhances quality control by enabling precise geometric controls that ensure feature consistency and reliability, particularly in complex assemblies where traditional methods might overlook form variations. Improved communication between design and manufacturing teams is another advantage, as the standard's consistent language bridges gaps in interpretation, fostering collaboration and accelerating the product development cycle. Additionally, it supports advanced manufacturing processes by offering flexibility in tolerance application, streamlining production for techniques like additive manufacturing while maintaining design intent. A specific mechanism in GD&T under ASME Y14.5 is the use of maximum material condition (MMC) and least material condition (LMC), which optimize tolerances by incorporating bonus allowances based on feature size, allowing parts to function effectively without rigid dimensional constraints. This approach contrasts with coordinate tolerancing, where GD&T provides superior control over part geometry, reducing assembly issues and scrap by focusing on allowable variations relative to functional requirements rather than isolated measurements. Overall, these elements make ASME Y14.5 indispensable for achieving efficient, high-quality manufacturing outcomes.

History and development

Origins

The origins of ASME Y14.5 trace back to the post-World War II era, when the need for standardized manufacturing practices became critical for ensuring part interchangeability in military equipment. These military efforts were influenced by earlier work, such as Stanley Parker's development of positional tolerancing in the for parts. The U.S. Department of Defense introduced early concepts of geometric tolerancing through MIL-STD-8, published in 1949, which provided foundational guidelines for dimensioning and tolerancing in engineering drawings primarily for military applications. This standard was revised as MIL-STD-8A in 1953, incorporating initial (GD&T) principles, such as the envelope principle (later known as Rule #1), to control form and orientation more precisely than traditional coordinate tolerancing. Building on these military foundations, civilian standards evolved in the and to meet growing demands from the automotive and industries, where complex assemblies required unambiguous specifications to facilitate and reduce assembly errors. The American Standards Association (ASA) issued Y14.5-1957, marking the first national standard for dimensioning and tolerancing with basic GD&T elements, followed by the United States of America Standards (USASI) Y14.5-1966, which expanded geometric controls. These efforts addressed inconsistencies in traditional plus-and-minus tolerancing, which often led to over-specification or interpretation ambiguities in high-precision . The American National Standards (ANSI) then released Y14.5-1973, formalizing a comprehensive symbology-based system influenced by wartime standardization needs for reliable part functionality across sectors. The ASME Y14.5 standard emerged from these precedents through the work of the ASME Y14 Subcommittee on Dimensioning and Tolerancing, established under the broader Y14 and Related Documentation Practices Committee, to unify and refine practices for broader industrial adoption. The first edition fully under ASME, published in 1982 as ASME Y14.5M, consolidated prior ANSI developments into a cohesive framework, emphasizing geometric controls to enhance design intent communication and efficiency.

Major revisions

The 1982 edition of ASME Y14.5M marked the first comprehensive standardization of geometric dimensioning and tolerancing (GD&T) under ASME, establishing a unified framework with symbols, rules, definitions, and practices for applying GD&T, including foundational datum concepts for reference and simulation. The 1994 edition, ASME Y14.5M, built on this by clarifying rules for composite tolerances, which allow separate control of form, orientation, location, and profile for patterns of features, and by adding appendices to document changes from prior versions and provide supplementary guidance. In the 2009 edition, ASME Y14.5, expansions to tolerances enabled non-uniform zones and controls without datums, while redundancies in terminology and practices were removed for clarity; this version became the most widely adopted, used by approximately half of surveyed companies in and . The 2018 edition introduced support for (MBD) through enhanced 3D annotations and figures, eliminated standalone concentricity and symmetry tolerances by subsuming them under for simpler inspection, added non-ambiguous datum stabilization protocols using for unstable features, and expanded to 326 pages to accommodate these updates. Each revision of ASME Y14.5 incorporates industry feedback through ASME's subcommittee review process, with the edition specifically addressing needs for sets and with standards like ASME Y14.41. The standard underwent reaffirmation in 2024 without major changes, confirming its ongoing validity for use in design and manufacturing.

Scope and definitions

Applicability

The ASME Y14.5 standard applies to the dimensioning and tolerancing of drawings, models, and associated for mechanical parts and assemblies, providing a system to define intent and control variation in physical products. It is primarily utilized in industries such as , automotive, , and general , where precise communication of geometric requirements is essential for , , and processes. The scope encompasses tolerancing for size, form (including straightness, flatness, circularity, and cylindricity), orientation (such as angularity, parallelism, and perpendicularity), location, profile, and runout, using geometric characteristic symbols and feature control frames to specify measurable requirements. However, it excludes topics like statistical tolerancing, which is addressed in Section 5.18 but not fully detailed, and surface texture or finish, which are covered by separate standards such as ASME Y14.36. The standard does not specify manufacturing methods or gaging practices, deferring those to other ASME Y14 series documents like Y14.43. Since its adoption by the U.S. Department of Defense on February 9, 2009, ASME Y14.5 has been mandatory for DoD contracts involving engineering drawings and related documentation, ensuring consistency in defense-related manufacturing. For international applications aligned with ISO standards, it serves as an optional but recommended framework, promoting interoperability while allowing adaptation to regional practices. As a communication standard rather than a comprehensive handbook, ASME Y14.5 focuses on the and rules for specifying tolerances, assuming users possess basic knowledge of principles and . It excludes non-engineering fields like architectural or symbology and does not address qualitative aspects beyond quantifiable geometric controls.

Key terminology

The ASME Y14.5 establishes a precise vocabulary for (GD&T) to ensure unambiguous communication in engineering design, manufacturing, and . Section 3 of the provides comprehensive definitions for numerous terms essential to GD&T, with approximately 70 entries that clarify concepts and promote consistency across applications. These definitions distinguish between functional features, which directly influence part performance or assembly, and geometric features, which are idealized representations used for tolerancing purposes. A feature is defined as a physical portion of a part, such as a surface, hole, pin, or pattern, that is recognized by its geometric shape and dimensions and serves as the basis for applying tolerances. This term encompasses both individual elements and assemblies of elements on a part, enabling precise control over form, size, orientation, location, and runout. The refers to the specific volume, area, or length within which the geometry of a feature must lie to conform to the specified tolerance; it is bounded by limiting surfaces or lines derived from the tolerance value and geometric characteristic. For example, a flatness tolerance zone is the space between two parallel planes separated by the tolerance amount, ensuring the feature remains within acceptable variation. A is a theoretically exact value used to describe the perfect geometry of a feature or datum target, indicated by enclosing the numeric value in a rectangular frame without any associated tolerance. Basic dimensions establish the foundation for tolerance zones but do not carry manufacturing limits themselves; deviations are controlled solely by geometric tolerances. A datum is a theoretically exact point, axis, line, or plane derived from a datum , serving as the origin for measurement and tolerancing of other features. Datums provide a reference framework to simulate functional conditions, with their exact nature simulated from the physical datum feature during . Detailed aspects of datum features are covered in the Datums section. Material condition modifiers adjust how tolerances apply based on the actual of a of size, allowing for tolerance in scenarios. MMC (Maximum Condition) denotes the state of a feature containing the maximum amount of material within its size limits, such as the largest or smallest , which typically represents the worst-case condition. LMC (Least Condition) is the opposite, where the feature has the minimum material, such as the smallest or largest , often used for clearance-critical applications. RFS (Regardless of Size) applies the tolerance without regard to the feature's actual , providing no tolerance and serving as the default unless MMC or LMC is . These modifiers, symbolized by Ⓜ, Ⓛ, and no symbol for RFS respectively, are crucial for functional gauging and calculations.

General rules

Fundamental assumptions

The ASME Y14.5 standard is built upon several core assumptions that establish the foundational principles for (GD&T), ensuring consistent interpretation and application across , , and processes. These assumptions address how features are controlled by size tolerances in the absence of explicit geometric tolerances, the default state of parts, and the independence of tolerances unless modified. One of the primary assumptions is the Envelope Principle, also known as Rule #1, which states that the form of an individual regular of is controlled by its limits of , such that the feature cannot extend beyond a boundary (envelope) of perfect form at its maximum material condition (). Under this principle, a feature is assumed to have perfect geometric form when at ; as the actual departs from toward least material condition (LMC), form imperfections are permitted within the specified zone, but the surface must remain within the size limits at every point. This applies to individual features of , distinguishing them from related features in assemblies where additional controls may be needed. Complementing the Envelope Principle is the Independence Principle, or Rule #2, which assumes that each tolerance applies independently to its associated feature unless explicitly modified by a geometric tolerance or symbol, such as the independency symbol that removes form control from size limits. Consequently, size tolerances control only the size of a feature, while geometric tolerances control form, orientation, location, or runout independently, with no automatic bonus tolerance unless MMC or LMC is invoked. This principle ensures that variations in size do not inherently affect geometric tolerances, promoting flexibility in manufacturing unless tighter controls are specified. Early editions of the standard, such as ASME Y14.5M-1994, outlined 14 fundamental rules for ing in section 1.4 that underpin these principles, including: (1) each feature shall be dimensioned and toleranced; (2) dimensions and tolerances shall fully define the part without reliance on scaling or assumptions; (3) dimensions shall suit the and mating relationships; (4) each dimension shall define a single feature without locating one from another unless necessary; (5) dimensioning and tolerancing shall be consistent and non-duplicative; (6) all dimensions and tolerances apply at 20°C (68°F) unless otherwise noted; and additional rules on implied angles, zero dimensions, and application. In the edition, these rules have been revised, with many relocated to section 4 and expanded, including new rule 4.1(q) stating that as-designed dimensions do not establish functional or manufacturing targets unless specified. Additionally, parts are assumed to exist —free from external forces other than —unless restrained conditions are specified, with the implying rigidity and for application unless non-rigid features are denoted. This free-state allows for natural deformation in flexible parts, while geometric tolerances may be applied under restrained conditions to simulate functional .

General tolerancing practices

In ASME Y14.5, general tolerancing practices establish the framework for specifying allowable variations in part features to ensure interchangeability and functionality during manufacturing and inspection. Limits of size define the maximum and minimum boundaries for features such as holes, shafts, or external dimensions, ensuring that parts conform to design intent while accommodating production variations. These limits are typically expressed as a nominal dimension with a tolerance range, adhering to principles that control both size and inherent form at the maximum material condition unless otherwise specified. Unilateral tolerances permit variation in only one direction from the nominal size, often with a zero value on one side (e.g., +0.1/-0.0), which is useful for features where material addition or removal must be strictly controlled, such as in assemblies requiring clearance. Bilateral tolerances, in contrast, allow variation equally or unequally on both sides of the nominal (e.g., ±0.05), providing balanced flexibility and are the default for symmetric features. The standard mandates that tolerance values use consistent places, with plus values placed above minus values for clarity in documentation. Accumulation of tolerances refers to the buildup of permissible variations across multiple features or dimensions in a , which can compound errors and affect overall part accuracy; this is mitigated through strategic dimensioning methods like or approaches rather than chain dimensioning. For instance, in a linear stack-up, chain tolerancing might yield a total variation of ±0.15, while methods reduce it to ±0.10 by referencing all features to a common datum. These practices build on fundamental assumptions of the standard to minimize such accumulations without invoking specific geometric controls. Basic dimensions in geometric dimensioning and tolerancing (GD&T) serve as theoretically exact values that establish the perfect geometry or location of features, denoted by rectangular borders or notes, and require associated tolerances to be applied exclusively through feature control frames rather than direct limits. This approach decouples size from geometric tolerances, allowing precise control over form, orientation, and location while avoiding ambiguity in interpretation. The standard includes rules for projection and extension lines in section 1.7, which govern orthographic representations to ensure accurate depiction of tolerances in multiview drawings, alongside guidelines for sectional views that reveal internal features without distorting tolerance zones and tabulation methods for presenting tolerance data in tables to streamline complex assemblies. These elements facilitate clear communication of tolerancing intent across engineering drawings. For threaded features and , tolerances are applied to the to control alignment and functionality, with exceptions for diameters that may use limits; these are handled via tables in the appendices or referenced standards like ASME B1.1 for unified inch screw threads, incorporating positional tolerances and projected tolerance zones where necessary to ensure proper mating.

Symbology

Geometric characteristic symbols

In ASME Y14.5-2018, Section 3 establishes a standardized set of symbols to denote geometric characteristics for dimensioning and tolerancing, enabling precise communication of tolerances on drawings. These symbols are categorized into form, , , , and tolerances, totaling 12 primary geometric characteristic symbols following revisions that streamlined the . Form tolerances control the shape of individual features without reference to datums. Straightness (↗) specifies the allowable deviation of a line or element from a straight line, applied to surfaces, axes, or medians. Flatness (⏤) defines the tolerance between two parallel planes within which the entire surface must lie. Circularity (○) ensures a feature's cross-section remains within two concentric circles. Cylindricity (⌭) combines straightness and circularity to control a surface within a cylindrical . Orientation tolerances regulate the direction of features relative to frames. Parallelism (∥) requires a surface or to lie within a tolerance zone parallel to a datum. Perpendicularity (⊥) mandates a 90-degree to a datum plane or . Angularity (∠) controls a specified angle between a feature and a datum. Location tolerances define the position of features. Position (⌖) governs the exact location of a feature of size or pattern relative to datums, often using a true position framework. Profile tolerances manage the outline of lines or surfaces. Profile of a line (⏫) controls the form and location of a line element within a uniform bilateral tolerance zone. Profile of a surface (⌒) extends this to the entire surface, ensuring uniformity and orientation. Runout tolerances assess variation during rotation around a datum axis. Circular runout (↻) measures the runout of a surface or feature at any single circular measurement. Total runout (⟲) controls the cumulative runout across the entire feature surface. The 2018 revision removed the symbols for concentricity (⊙) and symmetry (⌯), which previously controlled median point or plane alignment, due to their frequent misapplication and measurement challenges; these concepts are now addressed using position or profile tolerances for more effective control. Additional modifiers include the diameter symbol (⌀), which precedes values for cylindrical features, and the radius symbol (⌽) for radial dimensions. These geometric characteristic symbols are placed within feature control frames or general notes on drawings to specify tolerances clearly.

Feature control frames

In ASME Y14.5, a feature control frame serves as the primary mechanism for specifying geometric tolerances on engineering drawings, encapsulating the geometric characteristic symbol, tolerance value, any applicable modifiers, and datum references in a rectangular format. This frame ensures precise control over feature geometry relative to datums, promoting interchangeability in manufacturing. The composition of a feature control frame begins with the geometric characteristic symbol (e.g., the position symbol ⌖), followed by the tolerance value (e.g., 0.1), which defines the allowable variation. Modifiers such as maximum material condition (MMC) or least material condition (LMC) may appear after the tolerance value to adjust the tolerance based on feature size, enabling bonus tolerances for assembly clearance. Datum references, denoted by letters like A, B, C, are listed in subsequent compartments, establishing the reference frame for measurement. Feature control frames are read from left to right, with the geometric symbol and tolerance value first, followed by modifiers, and then datum references stacked top to bottom to indicate primary (top), secondary, and tertiary datums in . This hierarchical reading ensures consistent interpretation during . Frames can be single-segmented for individual requirements or composite, consisting of two vertically stacked segments sharing the same geometric symbol to address multiple related tolerances, such as pattern location in the upper segment and feature-to-feature relationships in the lower. The 2018 revision of ASME Y14.5 introduced the "SIM REQT" notation for composite frames, placed adjacent to applicable lower segments to clarify simultaneous requirements across multiple patterns, resolving ambiguities in prior editions. For example, a single-segmented position tolerance might appear as ⌖0.1|A|B|C (), controlling hole positions at relative to datums A, B, and C. A composite could stack two such segments, with the upper specifying broader datum controls (e.g., ⌖0.5|A|B|C) and the lower tighter feature relations (e.g., ⌖0.1|B|C), optionally annotated with SIM REQT for pattern simultaneity.

Datums

Datum features

In ASME Y14.5, a datum feature is defined as the actual physical feature on a part—such as a surface, , slot, or other feature of size—from which a datum is derived during and processes. This feature serves as the tangible reference point for establishing the location, orientation, and form of other features on the part, ensuring consistent interpretation across design, production, and verification. Unlike theoretical datums, which are idealized exact planes, lines, or points, datum features account for real-world imperfections like surface variations. The datum feature is identified on engineering drawings using the datum feature symbol, a rectangular containing a capital letter (e.g., A, B, or C) placed adjacent to the feature's edge view or dimension line. This symbol, often described as a "" or "suction cup" due to its appearance, directly references the physical feature and prevents ambiguity in datum selection. For features of size, such as holes or pins, the symbol applies to the entire feature unless modified by datum targets. Datum targets are used to refine or limit the datum feature to specific points, lines, or areas on the part, particularly when the full feature is irregular, oversized, or unsuitable for complete contact. These targets, denoted by symbols like circles for points or lines for areas, ensure precise simulation during by constraining the datum to high points or designated zones, avoiding over-constraint from irregular surfaces. For example, on a machined face with minor burrs, datum targets might specify three points to define a , promoting . ASME Y14.5, in Section 4, outlines the hierarchy of datum features as primary, secondary, and , based on their in the datum reference frame. The primary datum feature constrains three (typically two and one ), providing the foundational plane or axis for the part. Secondary datum features then constrain two additional (one and one ) relative to the primary, refining , while tertiary features constrain the final degree of freedom (one ) to fully locate the part. This sequential establishment ensures stability and minimizes , with higher-precedence datums controlling lower ones to maintain functional relationships. The 2018 revision of ASME Y14.5 introduced provisions for datum feature simulated datums, particularly for irregular or unstable surfaces like convex radii that might "rock" during simulation. These simulated datums allow for idealized representations derived from the physical feature using minimum material or maximum material boundaries, improving applicability to complex geometries without requiring full contact. This update enhances clarity for features previously difficult to datum, such as splines or undulating surfaces, by permitting partial or tangential simulation methods.

Datum reference frames

A datum reference frame (DRF) in ASME Y14.5 is a theoretical established from simulated datum features to define the exact orientation and location of tolerance zones relative to the part's geometry. It constrains the —three translational (along X, Y, Z axes) and three rotational (about those axes)—to create a stable basis for applying geometric tolerances. Derived from physical datum features, the DRF simulates idealized planes, axes, or points that the actual part aligns with during or . The construction of a full DRF follows a sequential of primary, secondary, and datums to progressively immobilize the part. The primary datum constrains three : two and one , typically by establishing a through at least three points of contact. The secondary datum then constrains two additional : one and one , often to the primary for . Finally, the datum constrains the remaining one translational degree of freedom, completing the six constraints without over-constraining the system. This sequential approach ensures a unique, repeatable reference frame for tolerancing. Partial DRFs are employed when a tolerance control does not require full constraint of all six degrees of freedom, allowing fewer datums to suffice for specific geometric requirements such as orientation or partial location. These are particularly useful in feature control frames where only relevant freedoms need restriction, promoting efficiency without ambiguity in application. The 2018 revision of ASME Y14.5 introduced the stability method to address ambiguities in datum simulation for unstable features, such as those prone to rocking or shifting. This non-ambiguous protocol uses simultaneous requirements—evaluating multiple constraint conditions concurrently—to determine allowable datum shifts, ensuring consistent interpretation across manufacturing and inspection processes. Mathematically, DRF constraints are modeled using transformation matrices for alignment, where R and vector \mathbf{t} adjust the part's to the theoretical frame: \mathbf{x}' = R \mathbf{x} + \mathbf{t} Here, \mathbf{x} represents points in the part's , and \mathbf{x}' are the aligned points satisfying the datum constraints. This formulation, detailed in ASME Y14.5.1, supports precise simulation without deriving full optimization here.

Form tolerances

Straightness and flatness

In ASME Y14.5-2018, Section 5 addresses form tolerances, which control the intrinsic shape of individual features without reference to datums, including straightness and flatness as fundamental controls for linear and planar elements. Straightness specifies the condition where an element of a surface, derived median line, or axis of a feature of size conforms to a straight line, ensuring uniformity along specified directions. For straightness applied to surface elements, the tolerance zone consists of two parallel lines separated by the specified tolerance value, within which all points on the surface must lie; this is a two-dimensional control suitable for features like edges or slots. When applied to a derived median line or axis of a feature of size, such as a shaft or hole, the tolerance zone is cylindrical with a diameter equal to the tolerance value, controlling the straightness of the theoretical axis derived from the feature's boundaries. The tolerance is denoted in a feature control frame using the straightness symbol—a horizontal line—and the value directly defines the zone width, for example, a straightness tolerance of 0.05 mm establishes a zone 0.05 mm wide (or ⌀0.05 mm for the cylindrical case). No datum reference is permitted in the feature control frame for straightness, as it is a self-referenced form control. Applications include ensuring the linearity of machined rods, guide rails, or hole axes to prevent functional deviations in assembly or motion. Flatness, also covered in Section 5, defines the condition where all points on a surface or derived median plane lie within a single plane, controlling deviations that could affect or sealing. The tolerance zone for flatness is bounded by two parallel planes separated by the specified value, encompassing the entire surface or the median plane derived from a feature of size. Similar to straightness, the value sets the uniform zone width—for instance, a flatness of 0.02 mm means the surface must fit between planes 0.02 mm apart—and is indicated via the flatness (a ) in a feature control frame without any datum references. This applies to planar features such as mounting faces, gaskets, or derived planes of width features, where planarity directly impacts load distribution or alignment. Both straightness and flatness may incorporate material condition modifiers like maximum material condition () for features of size, adjusting the effective zone based on size variations, but regardless, they prioritize form control independent of orientation or location.

Circularity and cylindricity

Circularity, also known as roundness, is a two-dimensional form in ASME Y14.5 that controls the of a cylindrical or conical feature's cross-section to ensure it approximates a perfect circle. The zone for circularity is defined as the annular space between two concentric circles in any to the feature's , within which the entire surface must lie. This zone applies independently at every cross-section along the feature's length, controlling local deviations from roundness without regard to orientation or location. The width of this zone is specified by the value t, such that the radial difference between the outer and inner circles satisfies r_{\text{outer}} - r_{\text{inner}} = t. As a form tolerance, circularity is independent of the feature's size, meaning it must be met at any actual size within the basic dimension limits, and it requires no datum references since it evaluates the intrinsic shape of the feature alone. It primarily addresses rotational form errors, such as lobing or ovality, complementing linear controls like straightness in maintaining overall feature integrity. Cylindricity extends circularity to a three-dimensional form tolerance, controlling the overall cylindrical shape of a feature by ensuring all points on its surface conform to a perfect cylinder. The tolerance zone for cylindricity is the space between two coaxial cylinders along the entire length of the feature, within which the surface must lie, thereby regulating both local circularity at each cross-section and axial straightness or taper. Like circularity, the zone's radial width equals the specified tolerance value t, applied uniformly without datum references or size dependency. This tolerance ensures comprehensive control of the feature's form, preventing deviations that could affect assembly or function in applications such as shafts and bores.

Orientation tolerances

Perpendicularity

Perpendicularity is an tolerance in ASME Y14.5 that controls the condition where a surface, axis, or center plane of a is oriented at 90 degrees to a specified datum . This tolerance ensures that the referenced maintains a relative to the datum, which is essential for functional assembly and performance in mechanical designs. The tolerance zone for perpendicularity varies depending on the feature type. For a surface, it consists of two parallel planes separated by the tolerance value, both oriented perpendicular to the datum plane or axis, within which the entire surface must lie. For an axis or center plane derived from a feature of size, the zone is a cylinder (for axes) or a pair of parallel planes (for center planes) perpendicular to the datum, with the derived axis or plane required to remain inside the zone. As defined in Section 6 of ASME Y14.5-2018, perpendicularity requires at least one to establish the orientation basis, typically a primary datum or . When applied to a of , the maximum material condition () modifier may be specified, which permits a as the actual of the departs from toward least material condition (LMC). The effective is calculated as the stated value plus the , where equals the difference between the actual and its (bonus = actual - ). This adjustment provides additional allowable deviation when the is undersized relative to , enhancing manufacturability without compromising function.

Angularity and parallelism

Angularity and parallelism s in ASME Y14.5 the of s relative to a frame (DRF) at specified angles, ensuring precise angular relationships beyond perpendicularity. These s define s that limit allowable deviation in , promoting functional interchangeability in manufactured parts. Angularity establishes an exact angle, other than 90°, between a and a datum using a with no on the angle itself. The for a surface consists of two parallel planes spaced apart by the value, oriented at the basic angle to the DRF; all points on the must lie between these planes. For s of size, such as axes, the zone may form a of diameter equal to the value, though this application is less common due to measurement challenges. The uniform boundary width equals the specified value, providing a consistent linear regardless of the angle. This structure is analogous to that of perpendicularity but rotated to the designated basic angle. In the 2018 revision of ASME Y14.5, angularity tolerances were clarified for application in compound angular relationships, particularly when multiple datums define the DRF, ensuring the zone aligns properly with the composite orientation. Additionally, the standard permits the angularity symbol as an alternative to specify parallelism or perpendicularity controls, offering flexibility in documentation while maintaining equivalent functional requirements. Parallelism, a specific , requires a feature to maintain a 0° or 180° relationship to a datum, effectively controlling or coaxiality without angular deviation. The zone comprises two planes (or lines for 2D features) oriented to the datum, with spacing equal to the value; the entire feature must reside within this zone. For surfaces, this refines control beyond basic dimensions under Rule #1, acting similarly to flatness but relative to the datum . When applied to features of , such as axes, the zone becomes a to the datum , with the not exceeding the feature's at maximum material condition. Like angularity, the zone's uniform width matches the value, emphasizing over . These tolerances are typically specified in a feature control frame referencing the applicable datums, with the basic angle (for angularity) or implied 0°/180° (for parallelism) ensuring the DRF establishes the reference . often involves aligning the part to the datum and verifying deviation using indicators or coordinate measuring machines oriented to the specified angle.

Location tolerances

Position

In ASME Y14.5-2018, the position tolerance, detailed in Section 7, controls the of a by defining the permissible variation from its true , which is the theoretically exact location of the feature's axis or center plane as established by basic dimensions relative to the frame (DRF). This tolerance applies to individual features or patterns of features, ensuring functional assembly and interchangeability in . Unlike coordinate tolerancing, position tolerance uses a uniform zone shape for more efficient control, prioritizing the functional relationship to datums over Cartesian deviations. The for varies by type: for axes of features (such as or pins), it forms a of equal to the specified value, centered on the true and extending the full length of the ; for planes of slot-like features, it consists of a strip between two parallel planes separated by the distance. When applied to patterns of features, such as arrays, composite tolerances may be used, with the upper controlling the of the entire relative to the DRF and the lower governing the orientation and spacing within the itself. The is typically circular and denoted by the (⌀) preceding the value; omitting this results in a non-circular , such as , which is less common and provides non-uniform control—allowing greater variation in diagonal directions (up to approximately 41% more maximum radial deviation)—making the circular preferable for round features as it offers more efficient, uniform tolerancing equivalent to about 57% more usable when matched for worst-case conditions. A key update in the 2018 edition of ASME Y14.5 removed the symbols and concepts for concentricity and tolerances, subsuming their functions under tolerance for more precise and versatile control of or coplanar features. can now be specified at maximum material condition () or least material condition (LMC) with modifiers, allowing bonus tolerance as the feature departs from to accommodate clearances without overconstraining size. For applications in , such as threaded fasteners or projected pins, the projected tolerance zone extends the cylindrical zone outward from the part surface by a specified height, ensuring sufficient engagement length despite positional variation. The deviation from true position is calculated using the in the plane perpendicular to the DRF, ensuring the feature axis lies within the zone. For a circular zone in two dimensions, the position deviation d must satisfy: d = \sqrt{(X - X_b)^2 + (Y - Y_b)^2} \leq \frac{T}{2} where (X, Y) are the actual coordinates of the feature axis, (X_b, Y_b) are the basic (true) coordinates, and T is the specified position diameter. This yields the radial deviation, which is doubled to obtain the full diametric for verification, emphasizing the zone's cylindrical nature over linear measurements.

Concentricity and symmetry

In ASME Y14.5, concentricity and were legacy location tolerances used to control the alignment of features relative to datums, but they were removed from the standard in the 2018 edition due to frequent misinterpretation and ambiguity in application. These tolerances are now retained solely for reference to interpret drawings and are no longer permitted as standalone symbols; instead, their intent is achieved through the position tolerance applied at regardless of feature size (RFS). Concentricity controlled the condition where the axis of a cylindrical feature of size must coincide with the axis of a specified datum feature within a cylindrical tolerance zone of diameter equal to the specified tolerance value. For legacy applications, this meant that the derived median points along the feature's axis had to lie entirely within the zone, ensuring central alignment without regard to feature size variations or form errors. The maximum allowable deviation of the feature axis from the datum axis was thus limited to half the tolerance value, expressed as: \text{Deviation from common axis} \leq \frac{\text{Tolerance value}}{2} This equation reflects the radial offset constraint within the cylindrical zone for pre-2018 usage. Symmetry, similarly deprecated, controlled the median plane of a slot or other bilateral feature of size to lie within two parallel planes equidistant from and parallel to a specified datum plane, with the total width of the zone equal to the tolerance value. In practice, this ensured that the feature's center plane bisected the tolerance zone symmetrically relative to the datum, focusing solely on locational uniformity across the plane without addressing orientation or size. Like concentricity, symmetry was eliminated in 2018 because it provided incomplete control—overlooking functional aspects like tilt or taper—that could be more precisely managed via position tolerance at RFS.

Profile tolerances

Profile of a line

of a line is a geometric that defines allowable variation for a or a cross-section of a surface, ensuring it conforms to a specified theoretical . This applies to two-dimensional features, such as curves or straight lines in a , and is particularly suited for controlling irregular or contours that cannot be adequately managed by basic form tolerances like straightness or circularity. In ASME Y14.5-2018, of a line is addressed in section 11, where it serves as a versatile control for features derived from basic dimensions on drawings. The zone for of a line consists of two parallel boundary lines (or curves) separated by the specified value, within which all points of the considered line must lie; for uneven , the zone may vary in width along the if explicitly defined using unequal distribution or other modifiers. This zone is established relative to the true , which is defined by dimensions, and can be bilateral (equal distribution on both sides) or unilateral (all allowance on one side) to accommodate design intent, such as clearance or fit requirements. The zone width is equal to the value provided in the feature control frame, with the boundaries tangent to the curve, ensuring precise conformance without excessive implications unless is separately controlled. Depending on datum references, profile of a line controls the form, orientation, and location of the line element: without datums, it primarily governs form; one or two datums add orientation control; and two or three datums enable full location control relative to the established datum reference frame. It is especially useful for complex curves, such as those on turbine blades or aerodynamic surfaces, where cross-sectional variations must be tightly regulated to maintain functional performance. For instance, in an extruded feature with varying profiles, multiple profile of a line callouts can refine control at specific slices, preventing deviations that might affect assembly or aerodynamics.

Profile of a surface

The of a surface in ASME Y14.5 controls the form, orientation, location, and size of a surface relative to specified datums or a , ensuring that all points on the actual surface conform to the intended three-dimensional . This is particularly versatile for defining complex, irregular shapes such as aerodynamic contours or molded components, where traditional form tolerances like flatness or cylindricity may be insufficient. Unlike simpler controls, it applies to the entire surface, providing comprehensive geometric constraint without relying on size dimensions alone. The tolerance for of a surface is a three-dimensional volume bounded by two offset surfaces parallel to the true , typically bilateral and at half the tolerance value (t/2) on either side, though unilateral or unequal distributions are possible with modifiers. The all-around symbol (∘) may be used to indicate full circumferential around the , extending the zone uniformly without datum references. This zone ensures that the surface maintains uniformity relative to the idealized shape defined by basic dimensions in the drawing or model. Mathematically, the tolerance zone is defined such that for any point P_S on the actual surface, there exists a point P_N on the nominal (true) profile surface and a scalar u satisfying -t^- \leq u \leq t^+, where P_S = P_N + \mathbf{n} u, \mathbf{n} is the unit vector to the nominal surface at P_N, and t^+ + t^- = t (the total value). For bilateral cases, t^+ = t^- = t/2, meaning all surface points must lie within this boundary to conform. In the 2018 revision of ASME Y14.5, profile of a surface tolerances were expanded to better support model-based definition (MBD), integrating with Y14.41 for 3D annotations and introducing the dynamic profile modifier (a triangular symbol) to control form, orientation, and location independently of size for non-cylindrical features. This update also standardized the circle U modifier as the sole method for specifying unequal bilateral tolerances, enhancing readability and inspection in digital environments. Building briefly on profile of a line, which controls two-dimensional cross-sections, profile of a surface extends this to full 3D coverage for broader applications.

Runout tolerances

Circular runout

Circular runout is a geometric tolerance in ASME Y14.5 that controls the functional variation of a surface of revolution, specifically the radial deviation of circular elements relative to a specified datum axis when the part is rotated 360 degrees. It applies to individual cross-sections perpendicular to the datum axis, capturing combined effects of form (such as circularity) and orientation (such as coaxiality) within a single plane, ensuring the surface remains within limits for rotational accuracy. This tolerance is particularly useful for features like shafts, bores, and gears where precise radial positioning is critical to prevent vibration or misalignment during operation. The tolerance zone for circular runout on cylindrical or conical features consists of two coaxial circles in each cross-section, separated radially by the tolerance value and aligned with the datum axis; all points on the controlled surface in that plane must lie between these boundaries. For planar features perpendicular to the datum axis, the zone consists of two concentric circles in the plane of the feature, centered on the datum axis, with the radial separation equal to the tolerance value, controlling wobble of the surface elements. A datum reference is always required, typically established by a cylindrical feature or pattern to define the axis of rotation, and the tolerance is specified at regardless of feature size (RFS) without material condition modifiers. Circular runout is detailed in Section 12 of ASME Y14.5-2018, where it is measured using a dial indicator or similar device mounted perpendicular to the surface; the value is the maximum total indicator reading (TIR) obtained during one full , which must not exceed the specified (e.g., Runout = max TIR ≤ tolerance value). This measurement method verifies by simulating the part's operational , with the datum serving as the for all readings. For example, on a with a 0.010-inch circular runout tolerance relative to datum A, the indicator variation at any cross-section must stay within ±0.005 inches radially from the true .

Total runout

Total runout is a composite geometric tolerance in ASME Y14.5 that controls the form, orientation, location, and circular runout of all points on a surface relative to a specified datum axis, ensuring the entire feature maintains uniformity during rotation. It applies simultaneously to both circular elements (perpendicular to the datum axis) and longitudinal elements (parallel to the datum axis), addressing variations such as circularity, cylindricity, straightness, and coaxiality for the controlled surface. Unlike circular runout, which evaluates individual cross-sections, total runout encompasses the full length of the feature for comprehensive control. The tolerance zone for total runout on cylindrical features consists of two coaxial cylinders separated radially by the specified tolerance value, with the zone centered on the datum axis and extending along the entire feature length. All surface points must lie within this cylindrical zone when the part rotates 360 degrees about the datum, limiting both radial and axial deviations across the feature. For conical features, the zone adapts similarly, maintaining coaxiality with the datum while accommodating the taper. Total runout represents the strictest form of control, as it imposes a single value on the cumulative effects over the whole surface without allowances for or least material condition (LMC); it applies exclusively at regardless of size (RFS). It is typically specified for cylindrical or conical surfaces, such as shafts or rotating components, where precise alignment and minimal wobble are critical. The variation is assessed using full indicator movement (FIM) with a dial indicator along the length, where the total runout is the maximum difference in indicator readings during at multiple axial positions. The condition for compliance is given by: \text{FIM} \leq t where t is the specified total runout tolerance value, ensuring the cumulative radial and axial variation does not exceed t across the feature. This measurement captures the overall geometric integrity without isolating form errors from positional ones.

Applications

In engineering drawings

In engineering drawings, ASME Y14.5 specifies that (GD&T) elements, such as feature control frames, must be placed directly adjacent to the features they control to ensure clear association and readability. These frames, which contain the geometric tolerance symbol, tolerance value, any modifiers, and datum references, are connected via leader lines to the specific feature, such as a or surface, preventing in interpretation. Datum feature symbols, denoted by capital letters in triangular frames, are similarly applied to edges, surfaces, or axes on the drawing, often using extension lines or direct placement to identify the physical features used for establishing datums. The standard outlines rules for applying GD&T across various drawing views to maintain consistency in orthographic projections. In multi-view orthographic drawings, tolerances like of a line or surface require the true profile to be shown in an appropriate view, ensuring that all necessary geometric controls are visible without distortion. For al views, datum references can be applied to cut surfaces or implied features, with the section lines clearly indicating the datum plane's location to avoid misaligning the reference frame. Broken-out sections follow similar principles, where partial views expose internal features for tolerancing, and datum labels must align with the visible geometry to preserve the intended precedence. ASME Y14.5 integrates with ASME Y14.1, which governs drawing sheet sizes and formats, to provide a uniform layout for annotating GD&T on engineering drawings. For instance, annotated drawings typically feature GD&T symbols and frames aligned with standard line weights and lettering per Y14.1, as seen in examples where position tolerances are applied to hole patterns relative to datum edges on A-series sheets. This coordination ensures that tolerances are presented clearly within the constrained space of 2D sheets. Common pitfalls in applying ASME Y14.5 to engineering drawings include over-specifying datums by referencing unnecessary features, which complicates inspection and increases costs without adding functional value. Another frequent error is ignoring datum precedence, such as applying redundant orientation tolerances (e.g., perpendicularity alongside ) that conflict with the hierarchical frame, leading to ambiguous instructions. To mitigate these, designers should limit s to those essential for and verify controls against the standard's rules for non-redundancy.

In model-based definition

In (MBD), ASME Y14.5 principles are adapted to embed (GD&T) directly into 3D CAD models as product manufacturing information (PMI), serving as the authoritative source for product specifications without relying on separate 2D drawings. This integration allows GD&T symbols, datums, and tolerance specifications to be annotated semantically within the digital model, enabling downstream processes like manufacturing and to access a unified, unambiguous . The 2018 edition of ASME Y14.5 introduces enhancements for environments, including semantic definitions for datums that emphasize non-ambiguous stabilization protocols, where a datum is derived from the feature's true geometric counterpart—a perfect form that minimizes separation from the actual surface using methods like (CMM) simulation. zones are explicitly defined within the model's coordinate space, supporting dynamic tolerances that apply independently of constraints and clarifying modifiers like "all over" for uniform application across entire surfaces. These updates incorporate more visualizations and absorb elements from ASME Y14.41, which standardizes the presentation of in digital product definition data practices. ASME Y14.5 aligns with ASME Y14.41 to facilitate MBD workflows, where GD&T annotations in models support automated by providing machine-readable semantics for tools. This compatibility ensures that tolerance zones and datum references are interpretable in model space, streamlining validation in computer-aided systems. Key advantages of applying ASME Y14.5 in MBD include reduced errors from discrepancies between drawings and models, as all specifications reside in a single , and enhanced simulation capabilities for stack-up analysis directly in the environment. General rules from the standard, such as feature control frames, are adapted to 3D by leveraging semantics for precise geometric control.

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