11.1 Circular Runout vs. Total Runout Interpretation & Dial Indicator Verification

Key Takeaways

  • Runout per ASME Y14.5-2009 Section 9.2 is a composite tolerance controlling the functional relationship of one or more part surfaces to a datum axis established at Regardless of Material Boundary (RMB).
  • Circular runout (single arrow ↗) controls circularity and coaxiality (or axial wobble) at each individual cross-section independently as the part rotates 360° about the datum axis with the dial indicator held at a fixed station.
  • Total runout (double arrow ⌰) controls circularity, straightness, taper, and coaxiality (or perpendicularity and flatness) simultaneously across the entire surface as the part rotates while the indicator traverses axially or radially.
  • Full Indicator Movement (FIM), formerly Total Indicator Reading (TIR), represents the full peak-to-valley swing of the dial indicator needle and must never exceed the specified feature control frame tolerance.
  • Material condition modifiers (Ⓜ or Ⓛ) are strictly prohibited on all runout callouts; runout tolerances always apply Regardless of Feature Size (RFS) to toleranced surfaces, and datum references always apply at RMB.
Last updated: September 2026

11.1 Circular Runout vs. Total Runout Interpretation & Dial Indicator Verification

Quick Answer: Under ASME Y14.5-2009 Section 9, runout is a composite tolerance used to control the functional relationship of one or more part surfaces to a datum axis. Circular Runout (single slant arrow , Section 9.4.1) controls circularity and coaxiality at each individual circular cross-section independently as the part rotates 360° with the dial indicator held at a fixed station. Total Runout (double slant arrow , Section 9.4.2) controls circularity, straightness, taper, and coaxiality simultaneously across the entire surface as the part rotates while the indicator traverses axially or radially. In runout inspection, tolerance compliance is verified by measuring Full Indicator Movement (FIM). Under ASME rules, material condition modifiers (Ⓜ or Ⓛ) are strictly prohibited in runout feature control frames; runout always applies Regardless of Feature Size (RFS) and datums always apply at Regardless of Material Boundary (RMB).


Foundations of Runout Tolerancing (ASME Y14.5-2009 Section 9.2)

In mechanical power transmission systems, high-speed rotating shafts, precision spindles, and turbine rotors, dynamic stability and balance depend heavily on how accurately cylindrical journals, conical tapers, and shoulder faces are aligned with the operational axis of rotation. Traditional size limits alone cannot prevent eccentric mounting, angular wobble, or surface lobing from causing catastrophic vibration, bearing destruction, and fatigue failure.

                    RUNOUT FEATURE CONTROL FRAME ANATOMY

        CIRCULAR RUNOUT (Section 9.4.1)        TOTAL RUNOUT (Section 9.4.2)
        ┌───┬──────┬───┬───┐                   ┌───┬──────┬─────┐
        │ ↗ │ 0.05 │ A │ B │                   │ ⌰ │ 0.02 │ A-B │
        └───┴──────┴───┴───┘                   └───┴──────┴─────┘
          ▲   ▲      ▲   ▲                       ▲   ▲       ▲
          │   │      └───┴─ Datum References    │   │       └─ Compound Datum Axis
          │   │             (RMB Only)           │   └─ Tolerance (RFS Only)
          │   └─ Tolerance Value (RFS Only)      └─ Double Arrow Symbol
          └─ Single Arrow Symbol

Definition of Runout

Per ASME Y14.5-2009 Section 9.2, runout is defined as a composite tolerance used to control the functional relationship of one or more features of a part to a datum axis established from a datum feature specified at RMB.

Runout is a direct surface control. Unlike position or concentricity, which govern theoretical centerlines or derived median points, runout directly monitors the physical variations of the part surface during dynamic rotation.

Surfaces Controlled by Runout

Runout tolerances are applicable exclusively to two specific geometric categories of surfaces:

  1. Surfaces constructed around a datum axis: These include external and internal cylindrical features, truncated cones, and spherical or contoured surfaces of revolution.
  2. Surfaces constructed at right angles to a datum axis: These include flat planar shoulder faces, flange mounting faces, and shaft end faces perpendicular to the axis of rotation.

Metrological Basis: Full Indicator Movement (FIM)

The fundamental metrological measurement unit in runout verification is Full Indicator Movement (FIM), formerly referred to in earlier standards and shop floor terminology as Total Indicator Reading (TIR) or Full Indicator Reading (FIR).

  • Definition of FIM: FIM is the total algebraic difference between the maximum positive deflection and the minimum negative deflection recorded by a dial or electronic indicator during rotation: $\text{FIM} = \text{Reading}{\max} - \text{Reading}{\min}$.
  • Rotation Requirement: The part must be rotated a full 360° about its established datum axis.
  • Acceptance Rule: At no point during inspection may the observed FIM exceed the tolerance value stated in the feature control frame.

Establishing the Datum Reference Axis (ASME Y14.5-2009 Section 9.3)

Every runout tolerance requires an established datum axis of rotation. Because runout controls rotational dynamic relationships, an improper datum setup invalidates the entire inspection. ASME Y14.5-2009 para. 9.3.1 states that the datum axis for a runout tolerance may be established by a cylindrical datum feature of sufficient length, by two or more cylindrical datum features having sufficient axial separation, or by a cylindrical datum feature and a face at right angles to it. It adds that features used as datum features for establishing axes should be functional, such as mounting features that establish an axis of rotation:

                     DATUM AXIS ESTABLISHMENT METHODS

     1. COMPOUND DATUM AXIS (A-B)          2. PRIMARY CYLINDER (A)
     ┌───────┐             ┌───────┐       ┌────────────────────────┐
     │Datum A│═════════════│Datum B│       │     Datum Feature A    │
     └───────┘             └───────┘       └────────────────────────┘
     ═══════════════════════════════       ══════════════════════════
             Common Axis A-B                               Axis A

     3. PLANAR FACE & PERPENDICULAR CYLINDER (A | B)
             ┌──┐
             │  │◄── Primary Planar Datum A (Controls pitch, yaw, Z)
             └──┴────────────────────────┐
                │   Datum Cylinder B     │
                └────────────────────────┘
             ═════════════════════════════◄── Axis established by B normal to A

1. Compound Coaxial Datum Axis (e.g., Datum A-B)

In multi-bearing power transmission shafts, the operational axis is rarely established by a single journal; rather, it is established by two separated cylindrical bearing journals acting simultaneously.

  • Callout Syntax: Specified as [ A-B ] in the datum reference compartment.
  • Physical Simulator: Two precision chucks, expanding collets, or pairs of V-blocks that clamp both datum features simultaneously at Regardless of Material Boundary (RMB).
  • Mathematical Axis: A single, uninterrupted datum centerline connecting the centers of the two simulated datum features.

2. Single Cylindrical Datum Feature (e.g., Datum A)

Para. 9.3.1 permits the datum axis to be established by a single cylindrical datum feature of sufficient length. The standard does not publish a numeric length-to-diameter ratio for what counts as sufficient; the judgement is functional — the feature must be long enough that its simulator repeatably constrains the four degrees of freedom a cylinder can constrain (two translations and two rotations) rather than allowing the part to rock. A short pilot diameter is the case that drives designers to method 3 below.

  • Callout Syntax: Specified as [ A ].
  • Physical Simulator: A high-precision expanding arbor, precision centering chuck, or precision inspection spindle that engages the datum cylinder across its entire operational length at RMB.

3. Planar Surface & Perpendicular Cylinder (e.g., Datum A | Datum B)

When a part has a wide locating face and a short pilot diameter (such as a flywheel, disc rotor, or bolt-on flange):

  • Primary Datum A (Planar Surface): Clamps against a precision surface plate, establishing three degrees of freedom (axial translation $Z$, and pitch/yaw rotations $u, v$).
  • Secondary Datum B (Cylinder): Establishes the datum axis perpendicular to Datum Plane A, constraining the remaining two translational degrees of freedom ($X, Y$).

Mandatory RMB Application

On the ASME GDTP examination, remember this inviolable rule: All datum features referenced in a runout feature control frame apply strictly at Regardless of Material Boundary (RMB). Material boundary modifiers (such as Maximum Material Boundary Ⓜ) are strictly illegal. The physical datum simulator must contract or expand to achieve intimate, zero-play contact with the datum feature, precluding any datum shift.


Circular Runout Interpretation & Metrology (ASME Y14.5-2009 Section 9.4.1)

Circular Runout is designated by a single slant arrow (). It provides two-dimensional composite control over individual circular elements of a surface.

                     CIRCULAR RUNOUT INSPECTION SETUP

                     Fixed Indicator Station 1    Fixed Indicator Station 2
                             ┌───┐                        ┌───┐
                             │(D)│                        │(D)│
                             └───┘                        └───┘
                               │ (Indicator fixed in Z)     │
                               ▼                            ▼
     ╔══════════╗      ┌────────────────────────────────────────┐      ╔══════════╗
     ║ Center A ║──────┤ Workpiece rotated 360° on datum axis   ├──────║ Center B ║
     ╚══════════╝      └────────────────────────────────────────┘      ╚══════════╝
     ══════════════════════════════════════════════════════════════════════════════
                                   Datum Axis A-B

     • Indicator held stationary at Station 1; part rotated 360°; FIM recorded.
     • Indicator moved to Station 2; re-zeroing allowed; part rotated 360°; FIM recorded.
     • FIM readings are independent (NOT cumulative between stations).

Tolerance Zone & Kinematic Inspection

Under Section 9.4.1, circular runout applies independently to each circular cross-section as the part is rotated 360° about its datum axis:

  1. Surfaces of Revolution (Cylinders and Cones):
    • Tolerance Zone: At each cross-section perpendicular to the datum axis, the tolerance zone is bounded by two concentric circles whose radii differ by the specified runout tolerance value $t$, generated about the datum axis.
    • Inspection Action: The dial indicator tip is placed normal to the feature surface at a fixed axial station. The workpiece is rotated 360° about the datum axis. The observed FIM represents the error at that station.
    • Non-Cumulative Rule: The indicator is then lifted, moved axially to a new station, and placed down. The inspector is permitted to re-zero the indicator at each station. The readings are independent and are never added together across stations.
  2. Surfaces at Right Angles to the Datum Axis (Perpendicular Flat Faces):
    • Tolerance Zone: At each radial distance from the datum axis, the tolerance zone is bounded by two parallel circles spaced apart axially by the tolerance value $t$.
    • Inspection Action: The dial indicator is placed parallel to the datum axis against the flat face at a fixed radial height. The part is rotated 360°. The indicator measures local circular wobble at that fixed radius.

Geometric Characteristics Controlled by Circular Runout

  • On Cylinders: Circular runout simultaneously controls circularity (roundness) and coaxiality (eccentricity) at each cross-section.
  • What It Does NOT Control: Circular runout does not control straightness of surface elements, taper, or overall diameter variation along the length of the cylinder. A shaft could be barrel-shaped, hourglass-shaped, or heavily tapered from end to end, yet exhibit zero circular runout at every individual cross-section if each slice is round and concentric to the datum axis!
  • On Flat Faces: Circular runout controls circular wobble (local perpendicularity) at each independent radial track. It does not control overall surface flatness.

Total Runout Interpretation & Metrology (ASME Y14.5-2009 Section 9.4.2)

Total Runout is designated by a double slant arrow (). It provides comprehensive three-dimensional composite control over an entire physical surface simultaneously.

                      TOTAL RUNOUT INSPECTION SETUP

                                  Traversing Dial Indicator
                                      ┌───┐   ◄── Indicator translates
                                      │(D)│       continuously along Z
                                      └───┘
                                        │
                                        ▼
     ╔══════════╗      ┌────────────────────────────────────────┐      ╔══════════╗
     ║ Center A ║──────┤ Workpiece rotated 360° on datum axis   ├──────║ Center B ║
     ╚══════════╝      └────────────────────────────────────────┘      ╚══════════╝
     ══════════════════════════════════════════════════════════════════════════════
                                   Datum Axis A-B

     • Workpiece rotates 360° while indicator translates along full cylinder length.
     • ZERO re-zeroing permitted; single cumulative FIM = (Highest Peak - Lowest Valley).

Tolerance Zone & Kinematic Inspection

Under Section 9.4.2, total runout applies to the entire feature surface simultaneously:

  1. Surfaces Constructed Around a Datum Axis (Cylinders):
    • Tolerance Zone: The tolerance zone is a three-dimensional annular space bounded by two coaxial cylinders spaced radially by the specified tolerance value $t$, concentric with the datum axis across the entire length of the feature.
    • Inspection Action: As the workpiece rotates continuously about the datum axis, the dial indicator is traversed longitudinally along the entire axial length of the cylinder (generating a continuous helical scanning path). Alternatively, a dense grid of synchronized measurements is recorded.
    • Cumulative FIM Rule: The dial indicator CANNOT be re-zeroed! The inspector must record the single absolute highest reading and the single absolute lowest reading across the entire cylinder surface. $\text{FIM}_{\text{total}} = \text{Maximum Peak} - \text{Minimum Valley}$.
  2. Surfaces Constructed at Right Angles to the Datum Axis (Flat Faces):
    • Tolerance Zone: Bounded by two parallel planes spaced apart axially by the tolerance value $t$, oriented perfectly perpendicular to the datum axis across the entire surface area.
    • Inspection Action: As the part rotates 360°, the indicator is traversed radially from the inner diameter to the outer edge of the face without re-zeroing.

Geometric Characteristics Controlled by Total Runout

  • On Cylinders: Total runout controls circularity, straightness of surface elements, taper (diameter variation), and coaxiality / angularity simultaneously relative to the datum axis. If a cylinder passes total runout of $0.02\text{ mm}$, its circularity, straightness, taper, and coaxiality are each guaranteed to be within $0.02\text{ mm}$.
  • On Flat Faces: Total runout controls perpendicularity and flatness simultaneously across the entire face.

Master Comparison: Circular Runout vs. Total Runout

Metrological ParameterCircular Runout (Section 9.4.1)Total Runout (Section 9.4.2)
SymbolSingle slant arrow ()Double slant arrow ()
Dimensionality2D control (individual cross-sections)3D control (entire surface simultaneously)
Tolerance Zone (Cylinder)Two concentric circles per cross-sectionTwo coaxial cylinders spanning full length
Tolerance Zone (Face)Two parallel circles per radial trackTwo parallel planes perpendicular to datum axis
Indicator MotionFixed station during 360° rotationTraverses continuously (axial or radial)
Dial Indicator Re-ZeroingPermitted at each station (independent)Strictly prohibited (single cumulative FIM)
Controls Circularity?Yes (within each slice)Yes (across all slices)
Controls Coaxiality?Yes (radial center offset)Yes (radial offset plus angular tilt)
Controls Straightness?No (blind to axial bow between slices)Yes (surface element straightness included)
Controls Taper / Cone?No (each slice can have different radius)Yes (taper causes indicator to sweep beyond FIM)
Controls Face Flatness?No (only local circular wobble)Yes (full face flatness included)
Inspection ComplexityModerate (sample discrete cross-sections)High (helical sweep or automated multi-channel)

The Strict Prohibition of Material Condition Modifiers

One of the most frequently tested principles on the ASME GDTP Technologist exam is the absolute prohibition of material condition modifiers in runout tolerancing:

Prohibited in Runout: Maximum Material Condition (Ⓜ) and Least Material Condition (Ⓛ)

Why Are Modifiers Prohibited?

  1. Surface Control vs. Size Control: Runout is an inspection of a physical surface boundary, not a feature of size axis or derived median line. An indicator probe contacts surface peaks and valleys directly; there is no mathematical "feature axis" or "virtual condition envelope" to which bonus tolerance could apply.
  2. RFS Default and Mandatory: Under ASME Y14.5-2009 Section 9.2, runout tolerances always apply Regardless of Feature Size (RFS). The stated tolerance value represents the absolute maximum allowable indicator needle swing regardless of whether the cylinder is produced at minimum, nominal, or maximum material size.
  3. RMB Datum Requirement: All datum references in a runout feature control frame must apply at Regardless of Material Boundary (RMB). Permitting datum shift (MMB Ⓜ) would cause an indicator needle to fluctuate unpredictably during rotation due to fixture slop, completely invalidating the runout measurement.
  4. Drafting Syntax Error: Placing Ⓜ or Ⓛ in either the tolerance compartment or datum compartment of a runout callout (e.g., [ ↗ | 0.05 Ⓜ | A Ⓜ ]) is an illegal drafting syntax error under ASME Y14.5-2009.

Common Exam Traps: Circular & Total Runout

  • Trap 1: Believing Circular Runout Controls Taper or Straightness: Candidates often assume that if a cylinder meets a circular runout callout of $0.04\text{ mm}$, its taper must be within $0.04\text{ mm}$. False. A shaft whose diameter changes from $\varnothing 20.00\text{ mm}$ at one end to $\varnothing 20.20\text{ mm}$ at the other end has $0.10\text{ mm}$ of radial taper, yet if each cross-section is round and concentric with the datum axis, circular runout at every slice is $0.00\text{ mm}$!
  • Trap 2: Re-Zeroing the Indicator During Total Runout Inspection: On total runout, if an inspector re-zeros the indicator between axial stations, they have converted a total runout check into an invalid circular runout check. Total runout requires measuring the peak-to-valley spread across the entire surface without resetting the gage.
  • Trap 3: Applying Runout to Non-Rotational Features: Runout cannot be applied to flat surfaces parallel to a datum axis (such as a keyway wall or hex flat) or to features that do not rotate about the datum axis.
  • Trap 4: Missing the Flat Face Perpendicularity Relationship: When circular runout is applied to a face perpendicular to a datum axis, it controls wobble (perpendicularity) at each individual radius, whereas total runout controls perpendicularity and flatness simultaneously across the whole face.
  • Trap 5: Assuming Bonus Tolerance Exists for Runout: Never add bonus tolerance from feature size departure to a runout tolerance. Runout is strictly RFS.
Test Your Knowledge

An inspector mounts a cylindrical transmission shaft on precision centers to inspect a bearing journal controlled by circular runout: '[ ↗ | 0.05 | A-B ]'. Datum A-B is a compound datum axis established by two chucked bearing surfaces. How must the dial indicator be operated during inspection per ASME Y14.5-2009?

A
B
C
D
Test Your Knowledge

A stepped turbine rotor shaft drawing specifies a total runout tolerance of '[ ⌰ | 0.03 | A ]' on an annular shoulder face constructed perpendicular to cylindrical datum feature A. Which statement correctly describes the tolerance zone and dial indicator verification for this planar surface under ASME Y14.5-2009?

A
B
C
D
Test Your Knowledge

During a drawing review for an aerospace rotating component, a quality engineer notices a feature control frame applied to a high-speed journal reading '[ ↗ | 0.08 Ⓜ | A Ⓜ ]'. How should this callout be evaluated according to the rules of ASME Y14.5-2009?

A
B
C
D