Crane Steel Structure Fabrication & Inspection Acceptance Standard

GB/T 30027-2013 "Cranes — Steel Structure Fabrication and Inspection" is the acceptance and inspection standard governing the entire crane steel structure manufacturing process. The standard defines the inspection items, methods, acceptance criteria, and verification procedures for crane steel structures at every stage — from incoming raw materials and in-process fabrication through to finished product delivery. It is used in conjunction with GB/T 30025 (fabrication) and GB/T 30026 (welding) to form a complete quality assurance system for crane steel structure manufacturing.

GB/T 30027-2013 is the dedicated standard for crane steel structure fabrication, inspection, and acceptance. Together with GB/T 30025-2013 (steel structure fabrication) and GB/T 30026-2013 (steel structure welding), it forms the three-part manufacturing standard system for crane steel structures. This article provides a systematic interpretation of the fabrication requirements and inspection rules specified in the standard.

GB/T 30027-2013 Crane Steel Structure Fabrication and Inspection Standard


Standard Inspection Framework

GB/T 30027-2013 organizes crane steel structure inspection into four levels:

Level 1: Incoming Inspection (IQC) — Quality verification of incoming raw materials (steel plates, structural sections, welding consumables, bolts, etc.). Steel plates undergo visual inspection and thickness measurement on a plate-by-plate basis (thickness deviation within the allowable range per GB/T 709), with chemical composition and mechanical properties verified by batch (each batch not exceeding 60 t, with the same heat number, specification, and heat treatment condition forming one inspection lot). Welding consumables are checked against model, grade, and mill certificates; welding electrodes are dried as specified and tested for diffusible hydrogen content. High-strength bolts are tested for torque coefficient (8 sets per batch, mean torque coefficient ±0.110) and wedge load.

Level 2: In-Process Inspection (IPQC) — Inspection of each operation during fabrication. This includes: cutting dimensional inspection (CNC cutting accuracy ±1 mm), edge preparation inspection (bevel angle ±2.5°, root face ±1 mm), assembly dimensional inspection (joint gap, misalignment, straightness, etc.), and welding process inspection (welding parameters, preheating temperature, interpass temperature, welding sequence). In-process inspection follows a "First Article Inspection + patrol sampling" model — every component's first article must be confirmed by an inspector before batch production proceeds.

Level 3: Finished Product Inspection (FQC) — Comprehensive inspection of final dimensions, appearance, and performance after steel structure fabrication is complete. This includes camber and side bow measurement of the main girder, diagonal difference measurement of end carriages, weld seam visual and NDT inspection, final assembly dimensional inspection, and coating quality inspection. Finished product inspection must produce complete inspection records that serve as the product's quality certification documentation for delivery.

Level 4: Routine Test (OQC) — Functional testing of the complete crane or its components before delivery. This includes: no-load test (all mechanisms operate normally, limit switches actuate accurately, brakes operate reliably), rated load test (measuring main girder deflection, lifting and operating stability), static load test (1.25 times rated load, no permanent deformation after main girder deflection recovers), and dynamic load test (1.1 times rated load, all mechanisms operating in combination for 30 min).

Incoming Inspection
Material + Dimensions + Visual
Each lot ≤ 60 t
In-Process Inspection
Dimensions + Welding Parameters
First Article + Patrol
Finished Product Inspection
Camber + NDT + Coating
Full Records
Routine Test
No-Load + Rated + 1.25×
Static + Dynamic
Camber
L/1000–L/1400
Max at Mid-Span
Side Bow Limit
≤ L/2000
and ≤ 8 mm

Dimensional Accuracy and Geometrical Tolerances

The standard specifies detailed dimensional accuracy and geometrical tolerance requirements for crane steel structural components. Key dimensional requirements for major structural components are as follows:

Main Girder — Camber: L/1000 to L/1400 at mid-span, with a smooth parabolic camber curve and no abrupt changes or local depressions. Side bow: not greater than L/2000, with an absolute value not exceeding 8 mm. Web plate flatness: not greater than 0.7 times the web thickness in the compression zone, and not greater than 1.2 times the web thickness in the tension zone. Flange plate horizontal inclination (angular distortion): not greater than 1/100 of the flange plate width. Overall main girder length tolerance: ≤ ±5 mm (for lengths ≤ 15 m) or ≤ ±8 mm (for lengths > 15 m).

End Carriage — Diagonal difference (difference between the two diagonal lengths of the end carriage): not exceeding 5 mm. Alignment difference after wheel installation (deviation between the vertical centerlines of two wheels on the same end carriage projected onto the horizontal plane): not exceeding 2 mm. Perpendicularity of the end carriage-to-main girder connection surface: not exceeding 1 mm per 500 mm.

Tower Mast Standard Section — Diagonal difference of the standard section: not exceeding 2 mm (difference in diagonal lengths of the connection faces). Parallelism between the top and bottom end faces: not exceeding 1/1000, with an absolute value ≤ 2 mm. Straightness of the main chord member axis: not exceeding 1/1000 of the full length. Hole pitch deviation for connection holes in the standard section: not exceeding ±0.3 mm.

Boom — Overall boom length tolerance: 0 to +5 mm (positive tolerance applied to nominal dimensions to account for welding shrinkage). Lateral bow of the boom: not exceeding L/2000. Upward bow: not exceeding L/1500. Coaxiality of the boom joint pin holes: Φ1.0 mm.

Non-Destructive Testing Requirements

Non-destructive testing (NDT) is one of the most critical aspects of steel structure fabrication inspection. The standard specifies clear requirements for NDT methods, sampling ratios, and acceptance grades for various weld seam categories:

Ultrasonic Testing (UT) — applicable to internal flaw detection of butt welds and T-joint welds. Grade 1 welds require 100% UT, evaluated per GB/T 11345, with Grade Ⅱ acceptance criteria (no cracks, incomplete fusion, or other linear defects permitted). Grade 2 welds also require 100% UT with Grade Ⅱ acceptance. Grade 3 welds do not require UT. Timing: testing is performed 24 hours after weld completion (allowing sufficient time for hydrogen diffusion).

Radiographic Testing (RT) — applicable as a supplementary inspection for butt welds. Grade 1 welds undergo an additional 10% RT verification on top of UT (evaluated per GB/T 3323, Grade Ⅱ acceptance). RT provides direct visual indication of internal porosity, slag inclusions, and incomplete penetration, complementing UT. When UT reveals suspected indications, expanded RT verification should be performed.

Magnetic Particle Inspection (MPI) — applicable to surface and near-surface flaw detection on ferromagnetic steel weld seams. Grade 1 and Grade 2 fillet welds require 100% MPI; butt welds are inspected once on the groove face and once on the finished weld surface. MPI acceptance criteria: no cracks or linear indications of any kind are permitted.

Penetrant Testing (PT) — applicable to surface inspection of welds on non-ferromagnetic materials (stainless steel, aluminum alloys), with technical requirements similar to MPI.

inspection items inspection method Acceptance Criteria Sampling Rate
camber Level Instrument/Pull Steel wire L/1000~L/1400 100%
Main Girder Side bow / lateral bow Pull Steel wire ≤L/2000 And≤8mm 100%
Web plate Flatness 1mStraightedge+feeler gauge Compression Zone≤0.7t / Tension Zone≤1.2t 100%
End Carriagediagonal difference Steel Ruler ≤5mm 100%
Crane wheelalignment difference Taut Wire/theodolite ≤2mm 100%
Grade IWeld Seam UT Ultrasonic Testing (UT) ⅡGrade Acceptance(GB/T 11345) 100%
Grade IWeld Seam RT Radiographic testing (RT) ⅡGrade Acceptance(GB/T 3323) ≥10%Re-inspection
Coating / painting Thickness Coating Thickness Gauge ≥80μm(Indoor)/≥120μm(Outdoor) Per10m²Measure5Point

Coating Quality Inspection

Coating is the last line of defense against corrosion for steel structures. The standard specifies the inspection items and requirements for coating quality: Coating appearance — must be uniform and consistent, free from sagging, pinholes, blistering, or exposed substrate. Coating thickness — measured with a film thickness gauge; total thickness must be ≥80 μm for indoor steel structures and ≥120 μm for outdoor use. Measurement points: 5 points per 10 m², with the arithmetic mean taken as the result. Faying surfaces of friction-type high-strength bolted connections must not be painted (protected with masking tape before delivery). Coating adhesion — tested by the cross-cut method per ISO 2409 (equivalent to GB/T 9286); a peeled area not exceeding 15% is considered acceptable. Coating inspection is performed after the coating has fully cured (typically 24–48 hours at ambient temperature).

Quality Record Management — The standard requires manufacturers to establish a complete quality record system. The full manufacturing process records for each crane's steel structure must include: raw material certificates of quality and retest reports, welding procedure qualification records (PQR), welder qualification certificates, non-destructive testing reports, key dimension measurement records, camber records, coating inspection records, Non-Conforming Product disposition records (including rework records), and factory test reports. All records must be retained at least until the crane is scrapped.


Crane Steel Structure Fabrication & Inspection Reference

The comparison table below outlines the core parameters for crane steel structure fabrication and inspection, serving as a reference for selection and operational personnel.

← Scroll left / right to view full table →
Machining Processtechnical requirementsInspection StandardSampling Rate
CuttingDimension Deviation±1mmGB/T 30027100%
groove MachiningAngle Deviation±2.5°GB/T 30027Spot Check20%
tack-up AssemblyGap≤2mm/Misalignment≤1mmGB/T 30027100%
StraighteningFlame straightening Temperature≤900°CGB/T 30027Piece-by-Pieceinspection

Frequently Asked Questions

Q: Under what conditions should camber measurement of the main girder be performed?
A: The standard specifies that camber measurement must be carried out after the main girder has been fully manufactured, with all welding and straightening work completed, and before coating or painting begins. During measurement, the girder should be placed horizontally, supported at both ends at the same elevation, with no added counterweight or external force applied. Measurement points should be set at intervals of 1–2 m from both ends toward the mid-span. Common measurement methods include: direct reading with a 2 m level and feeler gauge; the steel wire method, where a 150 N tension is applied with a spring scale and the vertical distance from the wire to the top surface of the girder is measured, then corrected for wire sag due to dead weight; and the level instrument method, which offers the highest accuracy. For acceptance, the camber of the main girder may be re-verified under no-load conditions.
Q: How should defects found during UT inspection of weld seams be handled?
A: When UT inspection reveals non-conforming defects (such as cracks, lack of fusion, or oversized point-like and elongated indications), the following procedure applies: 1) Mark the defect location and extent, and record the findings in the NDT Report; 2) Have a welding technician analyze the root cause (improper welding parameters, welder technique issues, base metal defects, etc.); 3) Remove the defect using carbon arc gouging or grinding until sound base metal is exposed, and confirm complete removal by Magnetic Particle Inspection (MPI); 4) Have a certified welder perform repair welding in accordance with the approved rework procedure; 5) Re-inspect the repaired area after 24 hours using UT and MT to verify the defect has been fully eliminated; 6) Rework at the same location is limited to two attempts—the second repair requires approval from the technical manager.
Q: How is the Static Load Test performed during the routine test?
A: The Static Load Test is a critical procedure for verifying the load-bearing capacity of the crane steel structure. Operating procedures: 1) Lift a load equal to 1.25 times the rated load (composed of test weights or standard test blocks) to a height of approximately 200 mm above the ground; 2) Maintain the suspended position for at least 10 minutes; 3) Observe and measure the main girder deflection (the maximum value must not exceed 1/700 of the span); 4) After unloading, check the main girder for permanent deformation (determined by comparing the camber difference before and after loading; permanent deformation must not exceed the smaller of 1/2000 of the span or 2 mm); 5) The test is considered satisfactory if all connections remain tight, no weld seam cracking is found, and no abnormal deformation of the structure is observed. The Static Load Test must be completed before the Dynamic Load Test.
Q: What marking requirements does the standard impose on steel structural components before delivery?
A: The standard requires that each steel structural component carry clear, permanent markings before leaving the factory. At a minimum, these markings must include: 1) the manufacturer's name or trademark; 2) the product model and serial number; 3) the component number (matching the assembly drawing); 4) the date of manufacture (month and year); and 5) a quality inspection approval mark (inspector's stamp or steel seal). For primary load-bearing members such as main girders, the weight (kg) and center of gravity position must also be indicated to facilitate proper lifting point placement during hoisting. Markings should be located in a visible area that is not prone to wear. The component numbering system is especially critical during installation and final assembly, and must correspond exactly to the numbering used on the General Assembly Drawing.

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