6.6 Cracks, Accumulation of Imperfections & Annex A (ECA)

Key Takeaways

  • Cracks (9.3.10): any crack of any size or location is a defect, with the sole exception of crater (star) cracks not exceeding 5/32 in. (4 mm).
  • Accumulation of Imperfections (9.3.12): excluding IPD and undercutting, the aggregate length of indications may not exceed 2 in. (50 mm) in any continuous 12 in. (300 mm) of weld, or 8% of the weld length.
  • Section 9.2 preserves the company's right to reject any weld even when indications appear to meet Section 9, if imperfection depth may be detrimental.
  • Annex A provides alternative (ECA) acceptance standards for girth welds based on fracture mechanics — CTOD toughness, applied stress, and AUT-measured flaw height and length — usable only when the company elects it and its prerequisites are met.
  • Under Annex A, acceptance turns on flaw HEIGHT (through-wall dimension) as much as length, which is why Annex A work requires AUT with demonstrated sizing accuracy (UT qualification, 3.1.60).
Last updated: August 2026

6.6 Cracks, Accumulation of Imperfections & Annex A (ECA)


1. Cracks (9.3.10) — Zero Tolerance, One Exception

Cracks are the most dangerous weld discontinuity: their sharp tips drive stress concentration toward theoretical infinity and provide fracture initiation points. API 1104:2021 Section 9.3.10 considers a crack a defect should either condition exist:

  • the crack, of any size or location in the weld, is not a crater crack or star crack; or
  • the crack is a crater or star crack with a length exceeding 5/32 in. (4 mm).

Classification reminders: longitudinal centerline cracks (solidification), transverse cracks (restraint + hardenability), HAZ hydrogen cracks (delayed, hours after welding), root cracks. All are rejectable. Section 10 adds that a weld containing a crack is repaired or cut out — and cut out when crack length exceeds 8% of weld length or after unsuccessful crack repair (see Section 7.1 of this guide).


2. Accumulation of Imperfections (9.3.12)

Individually acceptable imperfections can cluster into an unacceptable joint. The accumulation rule:

Excluding IPD and undercutting, any accumulation of imperfections is a defect when:

  • a) the aggregate length of indications in any continuous 12 in. (300 mm) of weld exceeds 2 in. (50 mm); or
  • b) the aggregate length of indications exceeds 8% of the weld length.

Only two categories are excluded: IPD (it already carries the generous 3 in. aggregate limit) and undercutting (governed by 9.3.11 / 9.7). Everything else — IP, ICP, IF, IFD, ESI, ISI, HB, porosity, BT — counts toward the 2 in. budget. (Cracks never reach the accumulation stage; they are defects on sight.)

Worked Example

A 12 in. segment contains: IP 0.35 in. + ESI 0.25 in. + HB 0.30 in. + IPD 1.50 in. + EU (Tier 2, 1.00 in.).

  1. Individual checks: IP ≤ 1.0 ✓; ESI ≤ 2.0 ✓; HB ≤ 1.0 ✓; IPD ≤ 2.0 ✓; EU within Table 8 ✓.
  2. AOI summation includes IP + ESI + HB only: 0.35 + 0.25 + 0.30 = 0.90 in.
  3. Compare: 0.90 ≤ 2.0 in.PASSES the accumulation rule (IPD and undercut are excluded by the rule itself).

3. Annex A — Alternative Acceptance Standards (ECA)

Section 9's workmanship limits are deliberately conservative. Annex A lets the company evaluate girth-weld imperfections by fitness for purpose instead: fracture mechanics using measured material toughness (CTOD per BS EN ISO 15653), applied stress, and flaw dimensions.

Key concepts:

  • Prerequisites: the company elects Annex A; the welding procedure and an AUT procedure with demonstrated detection and sizing accuracy (UT qualification per 3.1.60) are mandatory, because acceptance depends on flaw height as much as length.
  • Option 1: uses pre-computed allowable imperfection sizes keyed to measured CTOD toughness (e.g., the Figure A.7/A.8 limit curves for CTOD ≥ 0.010 in. and 0.004-0.010 in.).
  • Option 2: a project-specific fracture-mechanics analysis producing an acceptance table for the actual material, stress, and toughness.
  • Option 3: alternative acceptance criteria specified by the company (referenced also for repair acceptance in 10.6).
  • Cracks remain cracks: no ECA route legitimizes a crack — and U.S. regulation (49 CFR 192.241) expressly forbids using the alternative standards to accept a crack.
BasisSection 9Annex A
PhilosophyWorkmanship limitsFitness for purpose
Key measurementFlaw length per 12 in.Flaw height + length (AUT)
Toughness inputNoneCTOD / fracture analysis
CracksRejectedRejected

4. Related Structural-Integrity Rules

  • Crack disposition links to Section 10: a weld containing a crack is repaired (with authorization and a qualified crack-repair procedure) or cut out — cut-out being mandatory when a single crack or the aggregate of cracks exceeds 8% of weld length, and after any unsuccessful crack repair (no double repair of a crack).
  • Stacked defects (3.1.55): individual imperfections aligned in the radial (through-thickness) direction at the same circumferential location that exceed acceptance criteria are treated as a distinct condition — ultrasonically, 9.6.2.1 rejects multiple indications at the same location whose summed vertical height exceeds one-quarter of wall thickness.
  • UT height screen (9.6.2.1): ANY individual indication (not just cracks) with vertical through-wall height greater than one-quarter of wall thickness is a defect — the UT companion to the length-based rules.
  • Annex A toughness anchor: Option 1 publishes two limit-curve families — one for CTOD ≥ 0.010 in. (0.25 mm) and one for 0.004 in. (0.10 mm) ≤ CTOD < 0.010 in. — showing how measured toughness directly buys allowable imperfection size.
Test Your Knowledge

Under API 1104:2021 Section 9.3.10, what is the crack acceptance policy?

A
B
C
D
Test Your Knowledge

A 12-inch weld segment contains IP (0.40 in.), ESI (0.35 in.), and HB (0.35 in.), all passing their individual limits. What is the accumulation-of-imperfections (9.3.12) disposition?

A
B
C
D
Test Your Knowledge

In Annex A engineering critical assessment, which flaw dimension measured by AUT most governs fitness-for-purpose acceptance alongside CTOD toughness?

A
B
C
D